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turbojet

Course: AME 436, Fall 2008
School: USC
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M_1_default Parameter gamma_default MW_default T_1_default P_1_default n_diffuser_default gamma_d Pi_c_default n_comp gamma_c Pi_fan_default n_fan_default gamma_f alpha_fan_default Afterburner_default Tau_lamda_default Pi_burner_default n_burner gamma_b nturb_default gamma_t Tau_lam_ab Pi_ab_default n_ab gamma_ab P_9_default n_nozzle_default gamma_n Values in use Ideal cycle "Real" cycle 0.8000...

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Coursehero >> California >> USC >> AME 436

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Course Hero has millions of student submitted documents similar to the one below including study guides, practice problems, reference materials, practice exams, textbook help and tutor support.
M_1_default Parameter gamma_default MW_default T_1_default P_1_default n_diffuser_default gamma_d Pi_c_default n_comp gamma_c Pi_fan_default n_fan_default gamma_f alpha_fan_default Afterburner_default Tau_lamda_default Pi_burner_default n_burner gamma_b nturb_default gamma_t Tau_lam_ab Pi_ab_default n_ab gamma_ab P_9_default n_nozzle_default gamma_n Values in use Ideal cycle "Real" cycle 0.8000 0.8000 0.8000 1.4000 1.4000 1.4000 0.0290 0.0290 0.0290 250.0000 250.0000 250.0000 0.2500 0.2500 0.2500 1.0000 1.0000 0.9500 1.4000 1.4000 1.4000 20.0000 30.0000 20.0000 0.9000 1.0000 0.9000 1.3800 1.4000 1.3800 1.1000 2.0000 2.0000 1.0000 1.0000 0.9500 1.4000 1.4000 1.4000 0.0000 0.0000 0.0000 FALSE FALSE FALSE 5.0000 5.0000 5.0000 1.0000 1.0000 0.9500 1.0000 1.0000 0.9900 1.3000 1.4000 1.3000 1.0000 1.0000 0.9200 1.2900 1.4000 1.2900 7.0000 7.0000 7.0000 0.9500 1.0000 0.9500 1.0000 1.0000 0.9900 1.3000 1.4000 1.3000 0.2500 0.2500 0.2500 1.0000 1.0000 0.9500 1.3200 1.4000 1.3200 Description Description Default flight Mach number Default specific heat ratio (same throughout cycle unless overridden) Default gas molecular weight (assumed constant throughout cycle) Default ambient temperature Default ambient pressure Default inlet diffuser efficiency Specific heat ratio for diffuser (default value = gamma_default) Default compressor pressure ratio Default compressor efficiency Specific heat ratio for compressor (default value = gamma_default) Default fan pressure ratio Default fan efficiency Specific heat ratio for fan (default value = gamma_default) Default bypass ratio (mass flow through fan / mass flow through core stream) Default afterburner on/off (false = no afterburner) Default value of (turbine inlet temperature limit /ambient temperature) Default burner pressure ratio Default burner efficiency (actual fuel input / ideal fuel input if no heat losses) Specific heat ratio for diffuser (default value = gamma_default) Default turbine efficiency Specific heat ratio for diffuser (default value = gamma_default) Default value of (afterburner temperature limit /ambient temperature) Default afterburner pressure ratio Default afterburner efficiency (actual fuel input / ideal fuel input if no heat losses) Specific heat ratio for diffuser (default value = gamma_default) Exit pressure (default = ambient pressure) Default nozzle efficiency Specific heat ratio for diffuser (default value = gamma_default) M_1 0.0001 MW 0.0290 T_1 250.0000 P_1 0.2500 Rgas 286.9865 a_1 316.9310 u_1 0.0317 S_1 0.0000 T_2 250.0000 n_diffuser 1.0000 P_2 0.2500 S_2 0.0000 Pi_c 20.0000 n_comp 0.9000 Tau_comp 2.4241 T_3 606.0221 P_3 5.0000 S_3 0.2199 Pi_fan 1.1000 P_3_fan 0.2750 n_fan 1.0000 Tau_fan 1.0276 T_3_fan 256.9014 Tau_lamda 5.0000 T_4 1250.0000 q_in 8.009E+05 Pi_burner 1.0000 P_4 5.0000 S_4 3.3571 n_turb 1.0000 alpha 0.0000 T_5 893.9779 Tau_turb 0.7152 Pi_turb 0.2251 P_5 1.1256 S_5 3.3571 Afterburn 0.0000 Tau_lam_ab 7.0000 T_7 893.9779 q_in_ab 0.000E+00 q_ab/q_b 0.0000 Pi_ab 0.9500 P_7 1.0693 S_7 3.4084 P_9 0.2500 Pe/Pa 1.0000 n_nozzle 1.0000 M_9 1.6247 T_9 628.5191 S_9 3.4084 u_9 792.7866 P_9_fan 0.2500 T_9_fan 250.0000 M_9_fan 0.3715 u_9_fan 117.7467 Specific_thrust 2.5013 Thermal_eff 0.3924 Ideal thermal eff 0.5751 Propulsive_eff 0.0001 Overall_eff 0.0000 TSFC 3.1875 0.1001 0.0290 250.0000 0.2500 286.9865 316.9310 31.7248 0.0000 250.5010 1.0000 0.2518 0.0000 20.0000 0.9000 2.4241 607.2365 5.0352 0.2199 1.1000 0.2769 1.0000 1.0276 257.4162 5.0000 1250.0000 7.993E+05 1.0000 5.0352 3.3485 1.0000 0.0000 893.2645 0.7146 0.2243 1.1295 3.3485 0.0000 7.0000 893.2645 0.000E+00 0.0000 0.9500 1.0730 3.3997 0.2500 1.0000 1.0000 1.6270 627.4916 3.3997 793.2554 0.2500 250.0000 0.3851 122.0595 2.4028 0.3930 0.5760 0.0769 0.0302 3.3119 0.2001 0.0290 250.0000 0.2500 286.9865 316.9310 63.4179 0.0000 252.0020 1.0000 0.2571 0.0000 20.0000 0.9000 2.4241 610.8751 5.1415 0.2199 1.1000 0.2828 1.0000 1.0276 258.9587 5.0000 1250.0000 7.948E+05 1.0000 5.1415 3.3226 1.0000 0.0000 891.1269 0.7129 0.2219 1.1411 3.3226 0.0000 7.0000 891.1269 0.000E+00 0.0000 0.9500 1.0841 3.3739 0.2500 1.0000 1.0000 1.6338 624.4362 3.3739 794.6240 0.2500 250.0000 0.4233 134.1534 2.3071 0.3947 0.5785 0.1478 0.0583 3.4298 0.3001 0.0290 250.0000 0.2500 286.9865 316.9310 95.1110 0.0000 254.5030 1.0000 0.2661 0.0000 20.0000 0.9000 2.4241 616.9377 5.3224 0.2199 1.1000 0.2927 1.0000 1.0276 261.5287 5.0000 1250.0000 7.873E+05 1.0000 5.3224 3.2798 1.0000 0.0000 887.5653 0.7101 0.2180 1.1604 3.2798 0.0000 7.0000 887.5653 0.000E+00 0.0000 0.9500 1.1024 3.3311 0.2500 1.0000 1.0000 1.6449 619.4201 3.3311 796.7879 0.2500 250.0000 0.4802 152.1845 2.2140 0.3975 0.5826 0.2133 0.0848 3.5402 0.4001 0.0290 250.0000 0.2500 286.9865 316.9310 126.8041 0.0000 258.0040 1.0000 0.2792 0.0000 20.0000 0.9000 2.4241 625.4245 5.5831 0.2199 1.1000 0.3071 1.0000 1.0276 265.1264 5.0000 1250.0000 7.767E+05 1.0000 5.5831 3.2206 1.0000 0.0000 882.5795 0.7061 0.2126 1.1871 3.2206 0.0000 7.0000 882.5795 0.000E+00 0.0000 0.9500 1.1277 3.2719 0.2500 1.0000 1.0000 1.6599 612.5514 3.2719 799.5806 0.2500 250.0000 0.5500 174.3200 2.1228 0.4012 0.5883 0.2738 0.1098 3.6428 0.5001 0.0290 250.0000 0.2500 286.9865 316.9310 158.4972 0.0000 262.5050 1.0000 0.2966 0.0000 20.0000 0.9000 2.4241 636.3353 5.9315 0.2199 1.1000 0.3262 1.0000 1.0276 269.7516 5.0000 1250.0000 7.632E+05 1.0000 5.9315 3.1456 1.0000 0.0000 876.1697 0.7009 0.2058 1.2209 3.1456 0.0000 7.0000 876.1697 0.000E+00 0.0000 0.9500 1.1599 3.1969 0.2500 1.0000 1.0000 1.6783 603.9730 3.1969 802.7849 0.2500 250.0000 0.6285 199.1962 2.0329 0.4058 0.5953 0.3298 0.1338 3.7374 Thrust & fuel consumption 7 Specific thrust & TSFC 6 5 4 3 2 1 0 0.0 0.3 0.5 0.8 1.0 1.3 1.5 1.8 2.0 2.3 2.5 Mach number Specific_thrust TSFC T-s diagram 2000 Temperature (K) 1600 1200 800 400 0 Co lu m n Row 3 Co lu m n Co lu m n Co lu m n Co Co Co Co Co Co Co Co Co Co Co Co lu lu lu lu lu lu lu lu lu lu lu lu mmmmmmmmmmmm n n n nI nJ n n n n n n n Dimensionless entropy (S-S1)/R Row 16 Row 25 Row 32 Row 39 Co lu m n Co lu m n Co lu m n Co lu m n Row 9 Row 49 Effect of flight Mach number (ideal turbojet) 0.6001 0.0290 250.0000 0.2500 286.9865 316.9310 190.1903 0.0000 268.0060 1.0000 0.3189 0.0000 20.0000 0.9000 2.4241 649.6702 6.3780 0.2199 1.1000 0.3508 1.0000 1.0276 275.4045 5.0000 1250.0000 7.466E+05 1.0000 6.3780 3.0557 1.0000 0.0000 868.3358 0.6947 0.1978 1.2614 3.0557 0.0000 7.0000 868.3358 0.000E+00 0.0000 0.9500 1.1984 3.1070 0.2500 1.0000 1.0000 1.6996 593.8557 3.1070 806.1450 0.2500 250.0000 0.7128 225.9097 1.9435 0.4110 0.6037 0.3818 0.1569 3.8244 0.7001 0.0290 250.0000 0.2500 286.9865 316.9310 221.8834 0.0000 274.5070 1.0000 0.3468 0.0000 20.0000 0.9000 2.4241 665.4292 6.9361 0.2199 1.1000 0.3815 1.0000 1.0276 282.0849 5.0000 1250.0000 7.270E+05 1.0000 6.9361 2.9519 1.0000 0.0000 859.0778 0.6873 0.1886 1.3080 2.9519 0.0000 7.0000 859.0778 0.000E+00 0.0000 0.9500 1.2426 3.0032 0.2500 1.0000 1.0000 1.7232 582.3901 3.0032 809.3804 0.2500 250.0000 0.8011 253.8811 1.8537 0.4167 0.6130 0.4303 0.1793 3.9044 0.8001 0.0290 250.0000 0.2500 286.9865 316.9310 253.5765 0.0000 282.0080 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.6123 7.6225 0.2199 1.1000 0.4192 1.0000 1.0276 289.7930 5.0000 1250.0000 7.044E+05 1.0000 7.6225 2.8351 1.0000 0.0000 848.3957 0.6787 0.1784 1.3596 2.8351 0.0000 7.0000 848.3957 0.000E+00 0.0000 0.9500 1.2916 2.8864 0.2500 1.0000 1.0000 1.7482 569.7781 2.8864 812.1982 0.2500 250.0000 0.8921 282.7374 1.7626 0.4226 0.6233 0.4759 0.2011 3.9785 0.9001 0.0290 250.0000 0.2500 286.9865 316.9310 285.2696 0.0000 290.5090 1.0000 0.4229 0.0000 20.0000 0.9000 2.4241 704.2195 8.4574 0.2199 1.1000 0.4652 1.0000 1.0276 298.5287 5.0000 1250.0000 6.787E+05 1.0000 8.4574 2.7064 1.0000 0.0000 836.2895 0.6690 0.1673 1.4151 2.7064 0.0000 7.0000 836.2895 0.000E+00 0.0000 0.9500 1.3443 2.7577 0.2500 1.0000 1.0000 1.7740 556.2257 2.7577 814.3034 0.2500 250.0000 0.9852 312.2332 1.6692 0.4285 0.6344 0.5189 0.2224 4.0481 1.0001 0.0290 250.0000 0.2500 286.9865 316.9310 316.9627 0.0000 300.0100 1.0000 0.4733 0.0000 20.0000 0.9000 2.4241 727.2507 9.4658 0.2199 1.1000 0.5206 1.0000 1.0276 308.2920 5.0000 1250.0000 6.501E+05 1.0000 9.4658 2.5669 1.0000 0.0000 822.7593 0.6582 0.1556 1.4729 2.5669 0.0000 7.0000 822.7593 0.000E+00 0.0000 0.9500 1.3993 2.6182 0.2500 1.0000 1.0000 1.7996 541.9356 2.6182 815.4073 0.2500 250.0000 1.0797 342.2033 1.5727 0.4341 0.6459 0.5598 0.2430 4.1152 1.1001 0.0290 250.0000 0.2500 286.9865 316.9310 348.6558 0.0000 310.5110 1.0000 0.5339 0.0000 20.0000 0.9000 2.4241 752.7061 10.6770 0.2199 1.1000 0.5872 1.0000 1.0276 319.0829 5.0000 1250.0000 6.184E+05 1.0000 10.6770 2.4178 1.0000 0.0000 807.8049 0.6462 0.1434 1.5312 2.4178 0.0000 7.0000 807.8049 0.000E+00 0.0000 0.9500 1.4547 2.4691 0.2500 1.0000 1.0000 1.8244 527.1019 2.4691 815.2322 0.2500 250.0000 1.1754 372.5332 1.4722 0.4390 0.6579 0.5991 0.2630 4.1822 1.2001 0.0290 250.0000 0.2500 286.9865 316.9310 380.3489 0.0000 322.0120 1.0000 0.6063 0.0000 20.0000 0.9000 2.4241 780.5855 12.1264 0.2199 1.1000 0.6670 1.0000 1.0276 330.9013 5.0000 1250.0000 5.838E+05 1.0000 12.1264 2.2602 1.0000 0.0000 791.4265 0.6331 0.1309 1.5876 2.2602 0.0000 7.0000 791.4265 0.000E+00 0.0000 0.9500 1.5083 2.3115 0.2500 1.0000 1.0000 1.8474 511.9056 2.3115 813.5137 0.2500 250.0000 1.2720 403.1416 1.3667 0.4429 0.6701 0.6372 0.2822 4.2523 1.3001 0.0290 250.0000 0.2500 286.9865 316.9310 412.0421 0.0000 334.5130 1.0000 0.6928 0.0000 20.0000 0.9000 2.4241 810.8891 13.8556 0.2199 1.1000 0.7621 1.0000 1.0276 343.7474 5.0000 1250.0000 5.461E+05 1.0000 13.8556 2.0952 1.0000 0.0000 773.6239 0.6189 0.1183 1.6394 2.0952 0.0000 7.0000 773.6239 0.000E+00 0.0000 0.9500 1.5575 2.1465 0.2500 1.0000 1.0000 1.8677 496.5117 2.1465 810.0011 0.2500 250.0000 1.3693 433.9698 1.2557 0.4453 0.6825 0.6743 0.3003 4.3297 1.4001 0.0290 250.0000 0.2500 286.9865 316.9310 443.7352 0.0000 348.0140 1.0000 0.7957 0.0000 20.0000 0.9000 2.4241 843.6167 15.9136 0.2199 1.1000 0.8752 1.0000 1.0276 357.6212 5.0000 1250.0000 5.054E+05 1.0000 15.9136 1.9237 1.0000 0.0000 754.3973 0.6035 0.1058 1.6835 1.9237 0.0000 7.0000 754.3973 0.000E+00 0.0000 0.9500 1.5993 1.9750 0.2500 1.0000 1.0000 1.8844 481.0674 1.9750 804.4543 0.2500 250.0000 1.4671 464.9739 1.1382 0.4455 0.6948 0.7110 0.3167 4.4206 1.5001 0.0290 250.0000 0.2500 286.9865 316.9310 475.4283 0.0000 362.5150 1.0000 0.9179 0.0000 20.0000 0.9000 2.4241 878.7684 18.3578 0.2199 1.1000 1.0097 1.0000 1.0276 372.5225 5.0000 1250.0000 4.617E+05 1.0000 18.3578 1.7468 1.0000 0.0000 733.7466 0.5870 0.0935 1.7165 1.7468 0.0000 7.0000 733.7466 0.000E+00 0.0000 0.9500 1.6307 1.7981 0.2500 1.0000 1.0000 1.8967 465.7014 1.7981 796.6394 0.2500 250.0000 1.5654 496.1210 1.0135 0.4425 0.7070 0.7475 0.3308 4.5350 1.6001 0.0290 250.0000 0.2500 286.9865 316.9310 507.1214 0.0000 378.0160 1.0000 1.0628 0.0000 20.0000 0.9000 2.4241 916.3442 21.2552 0.2199 1.1000 1.1690 1.0000 1.0276 388.4514 5.0000 1250.0000 4.149E+05 1.0000 21.2552 1.5654 1.0000 0.0000 711.6718 0.5693 0.0816 1.7349 1.5654 0.0000 7.0000 711.6718 0.000E+00 0.0000 0.9500 1.6482 1.6167 0.2500 1.0000 1.0000 1.9034 450.5243 1.6167 786.3225 0.2500 250.0000 1.6640 527.3858 0.8810 0.4352 0.7190 0.7841 0.3412 4.6892 1.7001 0.0290 250.0000 0.2500 286.9865 316.9310 538.8145 0.0000 394.5170 1.0000 1.2342 0.0000 20.0000 0.9000 2.4241 956.3440 24.6837 0.2199 1.1000 1.3576 1.0000 1.0276 405.4079 5.0000 1250.0000 3.652E+05 1.0000 24.6837 1.3803 1.0000 0.0000 688.1730 0.5505 0.0703 1.7352 1.3803 0.0000 7.0000 688.1730 0.000E+00 0.0000 0.9500 1.6485 1.4315 0.2500 1.0000 1.0000 1.9035 435.6291 1.4315 773.2610 0.2500 250.0000 1.7630 558.7484 0.7397 0.4212 0.7308 0.8213 0.3459 4.9149 1.8001 0.0290 250.0000 0.2500 286.9865 316.9310 570.5076 0.0000 412.0180 1.0000 1.4367 0.0000 20.0000 0.9000 2.4241 998.7680 28.7334 0.2199 1.1000 1.5803 1.0000 1.0276 423.3920 5.0000 1250.0000 3.124E+05 1.0000 28.7334 1.1922 1.0000 0.0000 663.2500 0.5306 0.0597 1.7143 1.1922 0.0000 7.0000 663.2500 0.000E+00 0.0000 0.9500 1.6285 1.2435 0.2500 1.0000 1.0000 1.8958 421.0931 1.2435 757.1923 0.2500 250.0000 1.8622 590.1934 0.5890 0.3967 0.7422 0.8594 0.3409 5.2806 1.9001 0.0290 250.0000 0.2500 286.9865 316.9310 602.2007 0.0000 430.5190 1.0000 1.6754 0.0000 20.0000 0.9000 2.4241 1043.6161 33.5084 0.2199 1.1000 1.8430 1.0000 1.0276 442.4038 5.0000 1250.0000 2.567E+05 1.0000 33.5084 1.0018 1.0000 0.0000 636.9029 0.5095 0.0498 1.6693 1.0018 0.0000 7.0000 636.9029 0.000E+00 0.0000 0.9500 1.5858 1.0531 0.2500 1.0000 1.0000 1.8791 406.9789 1.0531 737.8191 0.2500 250.0000 1.9617 621.7081 0.4279 0.3540 0.7533 0.8988 0.3182 5.9714 M_1 0.8000 MW 0.0290 T_1 250.0000 P_1 0.2500 Rgas 286.9865 a_1 316.9310 u_1 253.5448 S_1 0.0000 T_2 282.0000 n_diffuser 1.0000 P_2 0.3811 S_2 0.0000 Pi_c 1.0000 n_comp 0.9000 Tau_comp 1.0000 T_3 282.0000 P_3 0.3811 S_3 0.0000 Pi_fan 1.1000 P_3_fan 0.4192 n_fan 1.0000 Tau_fan 1.0276 T_3_fan 289.7848 Tau_lamda 5.0000 T_4 1250.0000 q_in 1.204E+06 Pi_burner 1.0000 P_4 0.3811 S_4 6.4523 n_turb 1.0000 alpha 0.0000 T_5 1250.0000 Tau_turb 1.0000 Pi_turb 1.0000 P_5 0.3811 S_5 6.4523 Afterburn 0.0000 Tau_lam_ab 7.0000 T_7 1250.0000 q_in_ab 0.000E+00 q_ab/q_b 0.0000 Pi_ab 0.9500 P_7 0.3620 S_7 6.5036 P_9 0.2500 Pe/Pa 1.0000 n_nozzle 1.0000 M_9 0.7661 T_9 1142.6859 S_9 6.5036 u_9 504.0645 P_9_fan 0.2500 T_9_fan 250.0000 M_9_fan 0.8920 u_9_fan 282.7081 Specific_thrust 0.7905 Thermal_eff 0.0788 Ideal thermal eff 0.1135 Propulsive_eff 0.6693 Overall_eff 0.0528 TSFC 15.1619 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 1.3500 0.9000 1.0957 308.9930 0.5145 0.0319 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 1.170E+06 1.0000 0.5145 6.0880 1.0000 0.0000 1223.0070 0.9784 0.9075 0.4669 6.0880 0.0000 7.0000 1223.0070 0.000E+00 0.0000 0.9500 0.4435 6.1393 0.2500 1.0000 1.0000 0.9653 1064.3240 6.1393 612.9470 0.2500 250.0000 0.8920 282.7081 1.1340 0.1331 0.1863 0.5852 0.0779 10.2738 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 1.8225 0.9000 1.1997 338.3115 0.6945 0.0610 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 1.134E+06 1.0000 0.6945 5.7243 1.0000 0.0000 1193.6885 0.9550 0.8146 0.5658 5.7243 0.0000 7.0000 1193.6885 0.000E+00 0.0000 0.9500 0.5375 5.7756 0.2500 1.0000 1.0000 1.1289 991.5249 5.7756 691.8457 0.2500 250.0000 0.8920 282.7081 1.3830 0.1827 0.2532 0.5364 0.0980 8.1619 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 2.4604 0.9000 1.3126 370.1556 0.9376 0.0875 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 1.094E+06 1.0000 0.9376 5.3611 1.0000 0.0000 1161.8444 0.9295 0.7223 0.6772 5.3611 0.0000 7.0000 1161.8444 0.000E+00 0.0000 0.9500 0.6434 5.4124 0.2500 1.0000 1.0000 1.2687 923.9062 5.4124 750.5676 0.2500 250.0000 0.8920 282.7081 1.5682 0.2281 0.3145 0.5050 0.1152 6.9462 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 3.3215 0.9000 1.4353 404.7431 1.2658 0.1118 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 1.051E+06 1.0000 1.2658 4.9983 1.0000 0.0000 1127.2569 0.9018 0.6314 0.7993 4.9983 0.0000 7.0000 1127.2569 0.000E+00 0.0000 0.9500 0.7593 5.0496 0.2500 1.0000 1.0000 1.3898 861.1135 5.0496 793.8081 0.2500 250.0000 0.8920 282.7081 1.7047 0.2692 0.3709 0.4842 0.1303 6.1391 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 4.4840 0.9000 1.5685 442.3102 1.7088 0.1341 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 1.004E+06 1.0000 1.7088 4.6359 1.0000 0.0000 1089.6898 0.8718 0.5431 0.9280 4.6359 0.0000 7.0000 1089.6898 0.000E+00 0.0000 0.9500 0.8816 4.6872 0.2500 1.0000 1.0000 1.4944 802.8196 4.6872 824.1390 0.2500 250.0000 0.8920 282.7081 1.8004 0.3061 0.4226 0.4705 0.1440 5.5544 Thrust & fuel consumption 7 Specific thrust & TSFC 6 5 4 3 2 1 0 0.0 10.0 20.0 30.0 40.0 50.0 Specific_thrust TSFC Compressor pressure ratio T-s diagram 2000 Temperature (K) 1600 1200 800 400 0 Co lu m n Row 3 Co lu m n Co lu m n Co lu m n Co Co Co Co Co Co Co Co Co Co Co Co lu lu lu lu lu lu lu lu lu lu lu lu mmmmmmmmmmmm n n n nI nJ n n n n n n n Dimensionless entropy (S-S1)/R Row 16 Row 25 Row 32 Row 39 Co lu m n Co lu m n Co lu m n Co lu m n Row 9 Row 49 Effect of compressor pressure ratio (ideal turbojet) 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 6.0534 0.9000 1.7132 483.1137 2.3069 0.1544 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 9.537E+05 1.0000 2.3069 4.2739 1.0000 0.0000 1048.8863 0.8391 0.4583 1.0572 4.2739 0.0000 7.0000 1048.8863 0.000E+00 0.0000 0.9500 1.0043 4.3252 0.2500 1.0000 1.0000 1.5829 748.7224 4.3252 843.0183 0.2500 250.0000 0.8920 282.7081 1.8599 0.3389 0.4700 0.4624 0.1567 5.1049 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 8.1722 0.9000 1.8703 527.4323 3.1143 0.1730 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 8.986E+05 1.0000 3.1143 3.9122 1.0000 0.0000 1004.5677 0.8037 0.3782 1.1778 3.9122 0.0000 7.0000 1004.5677 0.000E+00 0.0000 0.9500 1.1189 3.9635 0.2500 1.0000 1.0000 1.6547 698.5446 3.9635 851.2064 0.2500 250.0000 0.8920 282.7081 1.8858 0.3674 0.5136 0.4590 0.1686 4.7440 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 11.0324 0.9000 2.0410 575.5688 4.2043 0.1901 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 8.387E+05 1.0000 4.2043 3.5508 1.0000 0.0000 956.4312 0.7651 0.3040 1.2781 3.5508 0.0000 7.0000 956.4312 0.000E+00 0.0000 0.9500 1.2142 3.6021 0.2500 1.0000 1.0000 1.7082 652.0327 3.6021 848.9440 0.2500 250.0000 0.8920 282.7081 1.8786 0.3913 0.5535 0.4599 0.1800 4.4448 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 14.8937 0.9000 2.2264 627.8522 5.6758 0.2058 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.737E+05 1.0000 5.6758 3.1897 1.0000 0.0000 904.1478 0.7233 0.2367 1.3436 3.1897 0.0000 7.0000 904.1478 0.000E+00 0.0000 0.9500 1.2765 3.2410 0.2500 1.0000 1.0000 1.7406 608.9570 3.2410 836.0055 0.2500 250.0000 0.8920 282.7081 1.8378 0.4101 0.5902 0.4654 0.1909 4.1913 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.1066 0.9000 2.4278 684.6397 7.6623 0.2201 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.031E+05 1.0000 7.6623 2.8288 1.0000 0.0000 847.3603 0.6779 0.1774 1.3593 2.8288 0.0000 7.0000 847.3603 0.000E+00 0.0000 0.9500 1.2913 2.8801 0.2500 1.0000 1.0000 1.7481 569.1128 2.8801 811.6585 0.2500 250.0000 0.8920 282.7081 1.7610 0.4228 0.6239 0.4760 0.2013 3.9749 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 27.1439 0.9000 2.6465 746.3194 10.3441 0.2333 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 6.264E+05 1.0000 10.3441 2.4682 1.0000 0.0000 785.6806 0.6285 0.1267 1.3111 2.4682 0.0000 7.0000 785.6806 0.000E+00 0.0000 0.9500 1.2455 2.5195 0.2500 1.0000 1.0000 1.7247 532.3222 2.5195 774.5072 0.2500 250.0000 0.8920 282.7081 1.6438 0.4275 0.6548 0.4933 0.2109 3.7937 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 36.6442 0.9000 2.8841 813.3126 13.9646 0.2453 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 5.431E+05 1.0000 13.9646 2.1077 1.0000 0.0000 718.6874 0.5749 0.0853 1.1907 2.1077 0.0000 7.0000 718.6874 0.000E+00 0.0000 0.9500 1.1311 2.1590 0.2500 1.0000 1.0000 1.6618 498.4388 2.1590 722.1281 0.2500 250.0000 0.8920 282.7081 1.4785 0.4209 0.6832 0.5197 0.2188 3.6568 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 49.4697 0.9000 3.1421 886.0772 18.8521 0.2564 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 4.526E+05 1.0000 18.8521 1.7475 1.0000 0.0000 645.9228 0.5167 0.0530 0.9998 1.7475 0.0000 7.0000 645.9228 0.000E+00 0.0000 0.9500 0.9498 1.7988 0.2500 1.0000 1.0000 1.5453 467.3572 1.7988 650.2144 0.2500 250.0000 0.8920 282.7081 1.2516 0.3961 0.7092 0.5611 0.2222 3.6000 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 66.7841 0.9000 3.4224 965.1103 25.4504 0.2666 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 3.543E+05 1.0000 25.4504 1.3874 1.0000 0.0000 566.8897 0.4535 0.0297 0.7553 1.3874 0.0000 7.0000 566.8897 0.000E+00 0.0000 0.9500 0.7175 1.4387 0.2500 1.0000 1.0000 1.3491 439.0309 1.4387 550.2032 0.2500 250.0000 0.8920 282.7081 0.9360 0.3365 0.7331 0.6309 0.2123 3.7682 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 90.1585 0.9000 3.7268 1050.9519 34.3580 0.2759 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 2.475E+05 1.0000 34.3580 1.0275 1.0000 0.0000 481.0481 0.3848 0.0143 0.4912 1.0275 0.0000 7.0000 481.0481 0.000E+00 0.0000 0.9500 0.4666 1.0788 0.2500 1.0000 1.0000 1.0103 413.5115 1.0788 399.8779 0.2500 250.0000 0.8920 282.7081 0.4617 0.1931 0.7550 0.7761 0.1499 5.3375 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 121.7139 0.9000 4.0574 1144.1886 46.3834 0.2845 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 1.316E+05 1.0000 46.3834 0.6678 1.0000 0.0000 387.8114 0.3102 0.0055 0.2543 0.6678 0.0000 7.0000 387.8114 0.000E+00 0.0000 0.9500 0.2416 0.7191 0.2500 1.0000 1.0000 Err:502 Err:502 Err:502 Err:502 0.2500 250.0000 0.8920 282.7081 Err:502 Err:502 0.7752 Err:502 Err:502 Err:502 0.8000 0.8000 0.8000 0.0290 0.0290 0.0290 250.0000 250.0000 250.0000 0.2500 0.2500 0.2500 286.9865 286.9865 286.9865 316.9310 316.9310 316.9310 253.5448 253.5448 253.5448 0.0000 0.0000 0.0000 282.0000 282.0000 282.0000 1.0000 1.0000 1.0000 0.3811 0.3811 0.3811 0.0000 0.0000 0.0000 164.3138 221.8236 299.4619 0.9000 0.9000 0.9000 4.4165 4.8066 5.2302 1245.4575 1355.4505 1474.9191 62.6175 84.5337 114.1204 0.2924 0.2996 0.3063 1.1000 1.1000 1.1000 0.4192 0.4192 0.4192 1.0000 1.0000 1.0000 1.0276 1.0276 1.0276 289.7848 289.7848 289.7848 5.0000 5.0000 5.0000 1250.0000 1250.0000 1250.0000 5.649E+03 -1.311E+05 -2.797E+05 1.0000 1.0000 1.0000 62.6175 84.5337 114.1204 0.3082 -0.0513 -0.4107 1.0000 1.0000 1.0000 0.0000 0.0000 0.0000 286.5425 176.5495 57.0809 0.2292 0.1412 0.0457 0.0014 0.0002 0.0000 0.0893 0.0140 0.0001 0.3082 -0.0513 -0.4107 0.0000 0.0000 0.0000 7.0000 7.0000 7.0000 286.5425 176.5495 57.0809 0.000E+00 0.000E+00 0.000E+00 0.0000 0.0000 0.0000 0.9500 0.9500 0.9500 0.0849 0.0133 0.0001 0.3595 0.0000 -0.3594 0.2500 0.2500 0.2500 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 Err:502 Err:502 Err:502 Err:502 Err:502 Err:502 Err:502 Err:502 Err:502 Err:502 Err:502 Err:502 0.2500 0.2500 0.2500 250.0000 250.0000 250.0000 0.8920 0.8920 0.8920 282.7081 282.7081 282.7081 Err:502 Err:502 Err:502 Err:502 Err:502 Err:502 0.7936 0.8106 0.8262 Err:502 Err:502 Err:502 Err:502 Err:502 Err:502 Err:502 Err:502 Err:502 M_1 0.8000 MW 0.0290 T_1 250.0000 P_1 0.2500 Rgas 286.9865 a_1 316.9310 u_1 253.5448 S_1 0.0000 T_2 282.0000 n_diffuser 1.0000 P_2 0.3811 S_2 0.0000 Pi_c 20.0000 n_comp 0.9000 Tau_comp 2.4241 T_3 683.5929 P_3 7.6217 S_3 0.2199 Pi_fan 1.1000 P_3_fan 0.4192 n_fan 1.0000 Tau_fan 1.0276 T_3_fan 289.7848 Tau_lamda 3.0000 T_4 750.0000 q_in 8.258E+04 Pi_burner 1.0000 P_4 7.6217 S_4 0.6216 n_turb 1.0000 alpha 0.0000 T_5 348.4071 Tau_turb 0.4645 Pi_turb 0.0330 P_5 0.2517 S_5 0.6216 Afterburn 0.0000 Tau_lam_ab 7.0000 T_7 348.4071 q_in_ab 0.000E+00 q_ab/q_b 0.0000 Pi_ab 0.9500 P_7 0.2391 S_7 0.6729 P_9 0.2500 Pe/Pa 1.0000 n_nozzle 1.0000 M_9 Err:502 T_9 Err:502 S_9 Err:502 u_9 Err:502 P_9_fan 0.2500 T_9_fan 250.0000 M_9_fan 0.8920 u_9_fan 282.7081 Specific_thrust Err:502 Thermal_eff Err:502 Ideal thermal eff 0.6233 Propulsive_eff Err:502 Overall_eff Err:502 TSFC Err:502 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 3.1500 787.5000 1.292E+05 1.0000 7.6217 0.8330 1.0000 0.0000 385.9071 0.4900 0.0419 0.3192 0.8330 0.0000 7.0000 385.9071 0.000E+00 0.0000 0.9500 0.3033 0.8843 0.2500 1.0000 1.0000 0.5474 368.2499 0.8843 204.4646 0.2500 250.0000 0.8920 282.7081 -0.1549 -0.0870 0.6233 1.1072 -0.0963 -8.3073 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 3.3075 826.8750 1.782E+05 1.0000 7.6217 1.0445 1.0000 0.0000 425.2821 0.5143 0.0519 0.3959 1.0445 0.0000 7.0000 425.2821 0.000E+00 0.0000 0.9500 0.3761 1.0958 0.2500 1.0000 1.0000 0.8064 385.1996 1.0958 308.0599 0.2500 250.0000 0.8920 282.7081 0.1720 0.0859 0.6233 0.9029 0.0776 10.3132 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 3.4729 868.2188 2.296E+05 1.0000 7.6217 1.2559 1.0000 0.0000 466.6258 0.5375 0.0632 0.4814 1.2559 0.0000 7.0000 466.6258 0.000E+00 0.0000 0.9500 0.4574 1.3072 0.2500 1.0000 1.0000 0.9927 403.0678 1.3072 387.9209 0.2500 250.0000 0.8920 282.7081 0.4240 0.1877 0.6233 0.7905 0.1484 5.3913 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 3.6465 911.6297 2.836E+05 1.0000 7.6217 1.4673 1.0000 0.0000 510.0368 0.5595 0.0755 0.5756 1.4673 0.0000 7.0000 510.0368 0.000E+00 0.0000 0.9500 0.5468 1.5186 0.2500 1.0000 1.0000 1.1427 421.8911 1.5186 456.8339 0.2500 250.0000 0.8920 282.7081 0.6414 0.2546 0.6233 0.7138 0.1818 4.4016 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 3.8288 957.2112 3.403E+05 1.0000 7.6217 1.6787 1.0000 0.0000 555.6183 0.5805 0.0890 0.6780 1.6787 0.0000 7.0000 555.6183 0.000E+00 0.0000 0.9500 0.6441 1.7300 0.2500 1.0000 1.0000 1.2696 441.7096 1.7300 519.3213 0.2500 250.0000 0.8920 282.7081 0.8386 0.3018 0.6233 0.6561 0.1980 4.0397 Thrust & fuel consumption 7 Specific thrust & TSFC 6 5 4 3 2 1 0 3.0 3.5 4.0 4.5 5.0 5.5 6.0 6.5 7.0 7.5 8.0 Tau_lamda Specific_thrust TSFC T-s diagram 2000 Temperature (K) 1600 1200 800 400 0 Co lu m n Row 3 Co lu m n Co lu m n Co lu m n Co Co Co Co Co Co Co Co Co Co Co Co lu lu lu lu lu lu lu lu lu lu lu lu mmmmmmmmmmmm n n n nI nJ n n n n n n n Dimensionless entropy (S-S1)/R Row 16 Row 25 Row 32 Row 39 Co lu m n Co lu m n Co lu m n Co lu m n Row 9 Row 49 Effect of turbine inlet temperature limit (ideal turbojet) 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 4.0203 1005.0717 3.998E+05 1.0000 7.6217 1.8902 1.0000 0.0000 603.4788 0.6004 0.1034 0.7881 1.8902 0.0000 7.0000 603.4788 0.000E+00 0.0000 0.9500 0.7487 1.9415 0.2500 1.0000 1.0000 1.3798 462.5667 1.9415 577.6063 0.2500 250.0000 0.8920 282.7081 1.0225 0.3369 0.6233 0.6101 0.2055 3.8926 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 4.2213 1055.3253 4.623E+05 1.0000 7.6217 2.1016 1.0000 0.0000 653.7324 0.6195 0.1188 0.9055 2.1016 0.0000 7.0000 653.7324 0.000E+00 0.0000 0.9500 0.8602 2.1529 0.2500 1.0000 1.0000 1.4775 484.5090 2.1529 632.9770 0.2500 250.0000 0.8920 282.7081 1.1972 0.3638 0.6233 0.5720 0.2081 3.8443 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 4.4324 1108.0916 5.279E+05 1.0000 7.6217 2.3130 1.0000 0.0000 706.4987 0.6376 0.1351 1.0294 2.3130 0.0000 7.0000 706.4987 0.000E+00 0.0000 0.9500 0.9779 2.3643 0.2500 1.0000 1.0000 1.5650 507.5862 2.3643 686.2601 0.2500 250.0000 0.8920 282.7081 1.3653 0.3852 0.6233 0.5396 0.2078 3.8494 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 4.6540 1163.4962 5.968E+05 1.0000 7.6217 2.5244 1.0000 0.0000 761.9033 0.6548 0.1521 1.1592 2.5244 0.0000 7.0000 761.9033 0.000E+00 0.0000 0.9500 1.1013 2.5757 0.2500 1.0000 1.0000 1.6442 531.8511 2.5757 738.0246 0.2500 250.0000 0.8920 282.7081 1.5287 0.4025 0.6233 0.5114 0.2058 3.8868 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 4.8867 1221.6710 6.692E+05 1.0000 7.6217 2.7359 1.0000 0.0000 820.0781 0.6713 0.1698 1.2944 2.7359 0.0000 7.0000 820.0781 0.000E+00 0.0000 0.9500 1.2297 2.7871 0.2500 1.0000 1.0000 1.7164 557.3598 2.7871 788.6837 0.2500 250.0000 0.8920 282.7081 1.6885 0.4167 0.6233 0.4865 0.2028 3.9455 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.1310 1282.7545 7.451E+05 1.0000 7.6217 2.9473 1.0000 0.0000 881.1616 0.6869 0.1882 1.4341 2.9473 0.0000 7.0000 881.1616 0.000E+00 0.0000 0.9500 1.3624 2.9986 0.2500 1.0000 1.0000 1.7825 584.1715 2.9986 838.5495 0.2500 250.0000 0.8920 282.7081 1.8458 0.4287 0.6233 0.4643 0.1991 4.0189 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.3876 1346.8922 8.249E+05 1.0000 7.6217 3.1587 1.0000 0.0000 945.2993 0.7018 0.2070 1.5779 3.1587 0.0000 7.0000 945.2993 0.000E+00 0.0000 0.9500 1.4990 3.2100 0.2500 1.0000 1.0000 1.8434 612.3489 3.2100 887.8662 0.2500 250.0000 0.8920 282.7081 2.0014 0.4389 0.6233 0.4443 0.1950 4.1032 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.6569 1414.2369 9.086E+05 1.0000 7.6217 3.3701 1.0000 0.0000 1012.6440 0.7160 0.2263 1.7249 3.3701 0.0000 7.0000 1012.6440 0.000E+00 0.0000 0.9500 1.6386 3.4214 0.2500 1.0000 1.0000 1.8997 641.9579 3.4214 936.8301 0.2500 250.0000 0.8920 282.7081 2.1559 0.4476 0.6233 0.4260 0.1907 4.1959 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.9398 1484.9487 9.966E+05 1.0000 7.6217 3.5816 1.0000 0.0000 1083.3558 0.7296 0.2460 1.8746 3.5816 0.0000 7.0000 1083.3558 0.000E+00 0.0000 0.9500 1.7808 3.6328 0.2500 1.0000 1.0000 1.9519 673.0682 3.6328 985.6028 0.2500 250.0000 0.8920 282.7081 2.3098 0.4551 0.6233 0.4092 0.1862 4.2954 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 6.2368 1559.1961 1.089E+06 1.0000 7.6217 3.7930 1.0000 0.0000 1157.6032 0.7424 0.2659 2.0263 3.7930 0.0000 7.0000 1157.6032 0.000E+00 0.0000 0.9500 1.9250 3.8443 0.2500 1.0000 1.0000 2.0004 705.7532 3.8443 1034.3200 0.2500 250.0000 0.8920 282.7081 2.4635 0.4617 0.6233 0.3937 0.1818 4.4005 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 6.5486 1637.1559 1.186E+06 1.0000 7.6217 4.0044 1.0000 0.0000 1235.5630 0.7547 0.2860 2.1795 4.0044 0.0000 7.0000 1235.5630 0.000E+00 0.0000 0.9500 2.0705 4.0557 0.2500 1.0000 1.0000 2.0455 740.0899 4.0557 1083.0981 0.2500 250.0000 0.8920 282.7081 2.6175 0.4675 0.6233 0.3794 0.1774 4.5105 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 6.8761 1719.0137 1.288E+06 1.0000 7.6217 4.2158 1.0000 0.0000 1317.4208 0.7664 0.3062 2.3336 4.2158 0.0000 7.0000 1317.4208 0.000E+00 0.0000 0.9500 2.2169 4.2671 0.2500 1.0000 1.0000 2.0877 776.1596 4.2671 1132.0385 0.2500 250.0000 0.8920 282.7081 2.7719 0.4727 0.6233 0.3660 0.1730 4.6248 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 7.2199 1804.9644 1.395E+06 1.0000 7.6217 4.4272 1.0000 0.0000 1403.3715 0.7775 0.3265 2.4881 4.4272 0.0000 7.0000 1403.3715 0.000E+00 0.0000 0.9500 2.3637 4.4785 0.2500 1.0000 1.0000 2.1271 814.0476 4.4785 1181.2308 0.2500 250.0000 0.8920 282.7081 2.9271 0.4772 0.6233 0.3534 0.1687 4.7432 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 7.5809 1895.2126 1.507E+06 1.0000 7.6217 4.6387 1.0000 0.0000 1493.6197 0.7881 0.3467 2.6425 4.6387 0.0000 7.0000 1493.6197 0.000E+00 0.0000 0.9500 2.5104 4.6900 0.2500 1.0000 1.0000 2.1640 853.8438 4.6900 1230.7552 0.2500 250.0000 0.8920 282.7081 3.0834 0.4813 0.6233 0.3416 0.1644 4.8652 M_1 0.8000 0.8000 MW 0.0290 0.0290 T_1 250.0000 250.0000 P_1 0.2500 0.2500 Rgas 286.9865 286.9865 a_1 316.9310 316.9310 u_1 253.5448 253.5448 S_1 0.0000 0.0000 T_2 282.0000 282.0000 n_diffuser 1.0000 1.0000 P_2 0.3811 0.3811 S_2 0.0000 0.0000 Pi_c 20.0000 20.0000 n_comp 0.9000 0.9000 Tau_comp 2.4241 2.4241 T_3 683.5929 683.5929 P_3 7.6217 7.6217 S_3 0.2199 0.2199 Pi_fan 1.1000 1.1000 P_3_fan 0.4192 0.4192 n_fan 1.0000 1.0000 Tau_fan 1.0276 1.0276 T_3_fan 289.7848 289.7848 Tau_lamda 5.0000 5.0000 T_4 1250.0000 1250.0000 q_in 7.044E+05 7.044E+05 Pi_burner 1.0000 1.0000 P_4 7.6217 7.6217 S_4 2.8352 2.8352 n_turb 1.0000 1.0000 alpha 0.0000 0.0000 T_5 848.4071 848.4071 Tau_turb 0.6787 0.6787 Pi_turb 0.1784 0.1784 P_5 1.3595 1.3595 S_5 2.8352 2.8352 Afterburn TRUE 1.0000 Tau_lam_ab 3.1500 3.3075 T_7 787.5000 826.8750 q_in_ab -7.574E+04 -2.678E+04 q_ab/q_b -0.1075 -0.0380 Pi_ab 0.9500 0.9500 P_7 1.2915 1.2915 S_7 2.5637 2.7751 P_9 0.2500 0.2500 Pe/Pa 1.0000 1.0000 n_nozzle 1.0000 1.0000 M_9 1.7482 1.7482 T_9 528.8860 555.3303 S_9 2.5637 2.7751 u_9 782.4990 801.8229 P_9_fan 0.2500 0.2500 T_9_fan 250.0000 250.0000 M_9_fan 0.8920 0.8920 u_9_fan 282.7081 282.7081 Specific_thrust 1.6690 1.7300 Thermal_eff 0.4359 0.4107 Ideal thermal eff 0.6233 0.6233 Propulsive_eff 0.4894 0.4995 Overall_eff 0.2133 0.2052 TSFC 3.7499 3.8996 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 1.0000 3.4729 868.2188 2.464E+04 0.0350 0.9500 1.2915 2.9865 0.2500 1.0000 1.0000 1.7482 583.0968 2.9865 821.6239 0.2500 250.0000 0.8920 282.7081 1.7924 0.4336 0.6233 0.4557 0.1976 4.0492 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 1.0000 3.6465 911.6297 7.862E+04 0.1116 0.9500 1.2915 3.1979 0.2500 1.0000 1.0000 1.7482 612.2516 3.1979 841.9140 0.2500 250.0000 0.8920 282.7081 1.8565 0.4575 0.6233 0.4164 0.1905 4.1991 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 1.0000 3.8288 957.2112 1.353E+05 0.1921 0.9500 1.2915 3.4094 0.2500 1.0000 1.0000 1.7482 642.8642 3.4094 862.7051 0.2500 250.0000 0.8920 282.7081 1.9221 0.4827 0.6233 0.3811 0.1839 4.3494 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 1.0000 4.0203 1005.0717 1.948E+05 0.2766 0.9500 1.2915 3.6208 0.2500 1.0000 1.0000 1.7482 675.0074 3.6208 884.0097 0.2500 250.0000 0.8920 282.7081 1.9893 0.5091 0.6233 0.3492 0.1778 4.5003 Thrust & fuel consumption 7 Specific thrust & TSFC 6 5 4 3 2 1 0 3.0 3.5 4.0 4.5 5.0 5.5 6.0 6.5 7.0 7.5 8.0 Tau_lamda afterburner Specific_thrust TSFC T-s diagram 2000 Temperature (K) 1600 1200 800 400 0 Co lu m n Row 3 Co lu m n Co lu m n Co lu m n Co Co Co Co Co Co Co Co Co Co Co Co lu lu lu lu lu lu lu lu lu lu lu lu mmmmmmmmmmmm n n n nI nJ n n n n n n n Dimensionless entropy (S-S1)/R Row 16 Row 25 Row 32 Row 39 Co lu m n Co lu m n Co lu m n Co lu m n Row 9 Row 49 Effect of afterburner temperature limit (ideal turbojet) 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 1.0000 4.2213 1055.3253 2.573E+05 0.3653 0.9500 1.2915 3.8322 0.2500 1.0000 1.0000 1.7482 708.7578 3.8322 905.8404 0.2500 250.0000 0.8920 282.7081 2.0582 0.5368 0.6233 0.3203 0.1720 4.6520 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 1.0000 4.4324 1108.0916 3.229E+05 0.4585 0.9500 1.2915 4.0436 0.2500 1.0000 1.0000 1.7482 744.1957 4.0436 928.2102 0.2500 250.0000 0.8920 282.7081 2.1287 0.5659 0.6233 0.2942 0.1665 4.8046 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 1.0000 4.6540 1163.4962 3.918E+05 0.5563 0.9500 1.2915 4.2551 0.2500 1.0000 1.0000 1.7482 781.4054 4.2551 951.1324 0.2500 250.0000 0.8920 282.7081 2.2011 0.5965 0.6233 0.2705 0.1613 4.9584 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 1.0000 4.8867 1221.6710 4.642E+05 0.6590 0.9500 1.2915 4.4665 0.2500 1.0000 1.0000 1.7482 820.4757 4.4665 974.6207 0.2500 250.0000 0.8920 282.7081 2.2752 0.6286 0.6233 0.2489 0.1565 5.1134 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 1.0000 5.1310 1282.7545 5.402E+05 0.7668 0.9500 1.2915 4.6779 0.2500 1.0000 1.0000 1.7482 861.4995 4.6779 998.6890 0.2500 250.0000 0.8920 282.7081 2.3511 0.6623 0.6233 0.2292 0.1518 5.2699 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 1.0000 5.3876 1346.8922 6.199E+05 0.8801 0.9500 1.2915 4.8893 0.2500 1.0000 1.0000 1.7482 904.5745 4.8893 1023.3517 0.2500 250.0000 0.8920 282.7081 2.4289 0.6977 0.6233 0.2112 0.1474 5.4280 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 1.0000 5.6569 1414.2369 7.037E+05 0.9990 0.9500 1.2915 5.1008 0.2500 1.0000 1.0000 1.7482 949.8032 5.1008 1048.6235 0.2500 250.0000 0.8920 282.7081 2.5087 0.7349 0.6233 0.1948 0.1432 5.5879 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 1.0000 5.9398 1484.9487 7.916E+05 1.1238 0.9500 1.2915 5.3122 0.2500 1.0000 1.0000 1.7482 997.2933 5.3122 1074.5193 0.2500 250.0000 0.8920 282.7081 2.5904 0.7739 0.6233 0.1798 0.1391 5.7496 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 1.0000 6.2368 1559.1961 8.839E+05 1.2549 0.9500 1.2915 5.5236 0.2500 1.0000 1.0000 1.7482 1047.1580 5.5236 1101.0547 0.2500 250.0000 0.8920 282.7081 2.6741 0.8149 0.6233 0.1660 0.1353 5.9133 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 1.0000 6.5486 1637.1559 9.809E+05 1.3925 0.9500 1.2915 5.7350 0.2500 1.0000 1.0000 1.7482 1099.5159 5.7350 1128.2453 0.2500 250.0000 0.8920 282.7081 2.7599 0.8579 0.6233 0.1534 0.1316 6.0792 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 1.0000 6.8761 1719.0137 1.083E+06 1.5371 0.9500 1.2915 5.9464 0.2500 1.0000 1.0000 1.7482 1154.4917 5.9464 1156.1074 0.2500 250.0000 0.8920 282.7081 2.8478 0.9031 0.6233 0.1418 0.1281 6.2474 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 1.0000 7.2199 1804.9644 1.190E+06 1.6888 0.9500 1.2915 6.1579 0.2500 1.0000 1.0000 1.7482 1212.2163 6.1579 1184.6576 0.2500 250.0000 0.8920 282.7081 2.9379 0.9506 0.6233 0.1311 0.1246 6.4181 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 1.0000 7.5809 1895.2126 1.302E+06 1.8482 0.9500 1.2915 6.3693 0.2500 1.0000 1.0000 1.7482 1272.8271 6.3693 1213.9128 0.2500 250.0000 0.8920 282.7081 3.0302 1.0004 0.6233 0.1213 0.1214 6.5913 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 1.0000 7.9599 1989.9733 1.420E+06 2.0155 0.9500 1.2915 6.5807 0.2500 1.0000 1.0000 1.7482 1336.4685 6.5807 1243.8904 0.2500 250.0000 0.8920 282.7081 3.1248 1.0527 0.6233 0.1123 0.1182 6.7673 M_1 0.8000 MW 0.0290 T_1 250.0000 P_1 0.2500 Rgas 286.9865 a_1 316.9310 u_1 253.5448 S_1 0.0000 T_2 282.0000 n_diffuser 1.0000 P_2 0.3811 S_2 0.0000 Pi_c 20.0000 n_comp 0.9000 Tau_comp 2.4241 T_3 683.5929 P_3 7.6217 S_3 0.2199 Pi_fan 1.1000 P_3_fan 0.4192 n_fan 1.0000 Tau_fan 1.0276 T_3_fan 289.7848 Tau_lamda 5.0000 T_4 1250.0000 q_in 7.044E+05 Pi_burner 1.0000 P_4 7.6217 S_4 2.8352 n_turb 1.0000 alpha 0.0000 T_5 848.4071 Tau_turb 0.6787 Pi_turb 0.1784 P_5 1.3595 S_5 2.8352 Afterburn 0.0000 Tau_lam_ab 7.0000 T_7 848.4071 q_in_ab 0.000E+00 q_ab/q_b 0.0000 Pi_ab 0.9500 P_7 1.2915 S_7 2.8865 P_9 0.2500 Pe/Pa 1.0000 n_nozzle 1.0000 M_9 1.7482 T_9 569.7912 S_9 2.8865 u_9 812.1956 P_9_fan 0.2500 T_9_fan 250.0000 M_9_fan 0.8920 u_9_fan 282.7081 Specific_thrust 1.7627 Thermal_eff 0.4226 Ideal thermal eff 0.6233 Propulsive_eff 0.4758 Overall_eff 0.2011 TSFC 3.9784 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.5000 844.5147 0.6756 0.1748 1.3320 2.8352 0.0000 7.0000 844.5147 0.000E+00 0.0000 0.9500 1.2654 2.8865 0.2500 1.0000 1.0000 1.7350 569.9966 2.8865 806.2008 0.2500 250.0000 0.8920 282.7081 1.1932 0.4213 0.6233 0.4847 0.2042 3.9182 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 1.0000 840.6223 0.6725 0.1712 1.3049 2.8352 0.0000 7.0000 840.6223 0.000E+00 0.0000 0.9500 1.2396 2.8865 0.2500 1.0000 1.0000 1.7216 570.2030 2.8865 800.1595 0.2500 250.0000 0.8920 282.7081 0.9084 0.4199 0.6233 0.4935 0.2073 3.8600 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 1.5000 836.7299 0.6694 0.1677 1.2782 2.8352 0.0000 7.0000 836.7299 0.000E+00 0.0000 0.9500 1.2143 2.8865 0.2500 1.0000 1.0000 1.7082 570.4105 2.8865 794.0707 0.2500 250.0000 0.8920 282.7081 0.7374 0.4186 0.6233 0.5024 0.2103 3.8039 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 2.0000 832.8375 0.6663 0.1643 1.2520 2.8352 0.0000 7.0000 832.8375 0.000E+00 0.0000 0.9500 1.1894 2.8865 0.2500 1.0000 1.0000 1.6947 570.6189 2.8865 787.9333 0.2500 250.0000 0.8920 282.7081 0.6234 0.4173 0.6233 0.5113 0.2133 3.7497 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 2.5000 828.9451 0.6632 0.1609 1.2262 2.8352 0.0000 7.0000 828.9451 0.000E+00 0.0000 0.9500 1.1649 2.8865 0.2500 1.0000 1.0000 1.6811 570.8285 2.8865 781.7462 0.2500 250.0000 0.8920 282.7081 0.5419 0.4159 0.6233 0.5202 0.2164 3.6974 Thrust & fuel consumption 7 Specific thrust & TSFC 6 5 4 3 2 1 0 0.0 1.0 2.0 3.0 4.0 5.0 6.0 7.0 8.0 Specific_thrust TSFC Bypass ratio (alpha) T-s diagram 2000 Temperature (K) 1600 1200 800 400 0 Co lu m n Row 3 Co lu m n Co lu m n Co lu m n Co Co Co Co Co Co Co Co Co Co Co Co lu lu lu lu lu lu lu lu lu lu lu lu mmmmmmmmmmmm n n n nI nJ n n n n n n n Dimensionless entropy (S-S1)/R Row 16 Row 25 Row 32 Row 39 Co lu m n Co lu m n Co lu m n Co lu m n Row 9 Row 49 Effect of fan bypass ratio (ideal turbojet) 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 3.0000 825.0527 0.6600 0.1575 1.2008 2.8352 0.0000 7.0000 825.0527 0.000E+00 0.0000 0.9500 1.1407 2.8865 0.2500 1.0000 1.0000 1.6674 571.0391 2.8865 775.5080 0.2500 250.0000 0.8920 282.7081 0.4807 0.4146 0.6233 0.5292 0.2194 3.6468 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 3.5000 821.1603 0.6569 0.1543 1.1758 2.8352 0.0000 7.0000 821.1603 0.000E+00 0.0000 0.9500 1.1170 2.8865 0.2500 1.0000 1.0000 1.6536 571.2507 2.8865 769.2176 0.2500 250.0000 0.8920 282.7081 0.4331 0.4132 0.6233 0.5381 0.2224 3.5978 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 4.0000 817.2679 0.6538 0.1510 1.1512 2.8352 0.0000 7.0000 817.2679 0.000E+00 0.0000 0.9500 1.0936 2.8865 0.2500 1.0000 1.0000 1.6396 571.4635 2.8865 762.8736 0.2500 250.0000 0.8920 282.7081 0.3950 0.4119 0.6233 0.5471 0.2253 3.5505 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 4.5000 813.3755 0.6507 0.1479 1.1270 2.8352 0.0000 7.0000 813.3755 0.000E+00 0.0000 0.9500 1.0706 2.8865 0.2500 1.0000 1.0000 1.6256 571.6773 2.8865 756.4748 0.2500 250.0000 0.8920 282.7081 0.3638 0.4105 0.6233 0.5560 0.2283 3.5047 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 5.0000 809.4831 0.6476 0.1447 1.1032 2.8352 0.0000 7.0000 809.4831 0.000E+00 0.0000 0.9500 1.0480 2.8865 0.2500 1.0000 1.0000 1.6114 571.8923 2.8865 750.0196 0.2500 250.0000 0.8920 282.7081 0.3378 0.4092 0.6233 0.5650 0.2312 3.4603 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 5.5000 805.5907 0.6445 0.1417 1.0798 2.8352 0.0000 7.0000 805.5907 0.000E+00 0.0000 0.9500 1.0258 2.8865 0.2500 1.0000 1.0000 1.5971 572.1084 2.8865 743.5065 0.2500 250.0000 0.8920 282.7081 0.3157 0.4078 0.6233 0.5740 0.2341 3.4174 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 5.9493 802.0930 0.6417 0.1390 1.0591 2.8352 0.0000 7.0000 802.0930 0.000E+00 0.0000 0.9500 1.0061 2.8865 0.2500 1.0000 1.0000 1.5841 572.3035 2.8865 737.6033 0.2500 250.0000 0.8920 282.7081 0.2986 0.4066 0.6233 0.5821 0.2367 3.3800 M_1 0.8000 MW 0.0290 T_1 250.0000 P_1 0.2500 Rgas 286.9865 a_1 316.9310 u_1 253.5448 S_1 0.0000 T_2 282.0000 n_diffuser 1.0000 P_2 0.3811 S_2 0.0000 Pi_c 20.0000 n_comp 0.9000 Tau_comp 2.4241 T_3 683.5929 P_3 7.6217 S_3 0.2199 Pi_fan 1.0000 P_3_fan 0.3811 n_fan 1.0000 Tau_fan 1.0000 T_3_fan 282.0000 Tau_lamda 5.0000 T_4 1250.0000 q_in 7.044E+05 Pi_burner 1.0000 P_4 7.6217 S_4 2.8352 n_turb 1.0000 alpha 2.0000 T_5 848.4071 Tau_turb 0.6787 Pi_turb 0.1784 P_5 1.3595 S_5 2.8352 Afterburn 0.0000 Tau_lam_ab 7.0000 T_7 848.4071 q_in_ab 0.000E+00 q_ab/q_b 0.0000 Pi_ab 0.9500 P_7 1.2915 S_7 2.8865 P_9 0.2500 Pe/Pa 1.0000 n_nozzle 1.0000 M_9 1.7482 T_9 569.7912 S_9 2.8865 u_9 812.1956 P_9_fan 0.2500 T_9_fan 250.0000 M_9_fan 0.8000 u_9_fan 253.5448 Specific_thrust 0.5876 Thermal_eff 0.4226 Ideal thermal eff 0.6233 Propulsive_eff 0.4758 Overall_eff 0.2011 TSFC 3.9784 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 2.0000 832.8375 0.6663 0.1643 1.2520 2.8352 0.0000 7.0000 832.8375 0.000E+00 0.0000 0.9500 1.1894 2.8865 0.2500 1.0000 1.0000 1.6947 570.6189 2.8865 787.9333 0.2500 250.0000 0.8920 282.7081 0.6234 0.4173 0.6233 0.5113 0.2133 3.7497 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.2100 0.4611 1.0000 1.0560 297.7845 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 2.0000 816.8381 0.6535 0.1507 1.1485 2.8352 0.0000 7.0000 816.8381 0.000E+00 0.0000 0.9500 1.0911 2.8865 0.2500 1.0000 1.0000 1.6381 571.4870 2.8865 762.1698 0.2500 250.0000 0.9776 309.8298 0.6533 0.4117 0.6233 0.5431 0.2236 3.5778 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.3310 0.5072 1.0000 1.0851 306.0050 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 2.0000 800.3971 0.6403 0.1377 1.0492 2.8352 0.0000 7.0000 800.3971 0.000E+00 0.0000 0.9500 0.9967 2.8865 0.2500 1.0000 1.0000 1.5778 572.3984 2.8865 734.7234 0.2500 250.0000 1.0583 335.4233 0.6783 0.4060 0.6233 0.5718 0.2321 3.4461 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.4641 0.5579 1.0000 1.1151 314.4525 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 2.0000 783.5021 0.6268 0.1252 0.9542 2.8352 0.0000 7.0000 783.5021 0.000E+00 0.0000 0.9500 0.9065 2.8865 0.2500 1.0000 1.0000 1.5135 573.3563 2.8865 705.3719 0.2500 250.0000 1.1354 359.8319 0.6988 0.4001 0.6233 0.5977 0.2392 3.3452 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.6105 0.6137 1.0000 1.1459 323.1332 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 2.0000 766.1408 0.6129 0.1133 0.8637 2.8352 0.0000 7.0000 766.1408 0.000E+00 0.0000 0.9500 0.8205 2.8865 0.2500 1.0000 1.0000 1.4446 574.3640 2.8865 673.8384 0.2500 250.0000 1.2094 383.2983 0.7150 0.3940 0.6233 0.6211 0.2447 3.2694 Thrust & fuel consumption 7 Specific thrust & TSFC 6 5 4 3 2 1 0 0.0 1.0 2.0 3.0 4.0 5.0 6.0 Specific_thrust TSFC Fan pressure ratio (alpha = 2 = const.) T-s diagram 2000 Temperature (K) 1600 1200 800 400 0 Co lu m n Row 3 Co lu m n Co lu m n Co lu m n Co Co Co Co Co Co Co Co Co Co Co Co lu lu lu lu lu lu lu lu lu lu lu lu mmmmmmmmmmmm n n n nI nJ n n n n n n n Dimensionless entropy (S-S1)/R Row 16 Row 25 Row 32 Row 39 Co lu m n Co lu m n Co lu m n Co lu m n Row 9 Row 49 Effect of fan pressure ratio (ideal turbojet) 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.7716 0.6751 1.0000 1.1775 332.0535 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 2.0000 748.3002 0.5986 0.1020 0.7777 2.8352 0.0000 7.0000 748.3002 0.000E+00 0.0000 0.9500 0.7388 2.8865 0.2500 1.0000 1.0000 1.3703 575.4256 2.8865 639.7693 0.2500 250.0000 1.2810 406.0020 0.7269 0.3877 0.6233 0.6417 0.2488 3.2157 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.9487 0.7426 1.0000 1.2100 341.2200 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 2.0000 729.9671 0.5840 0.0914 0.6965 2.8352 0.0000 7.0000 729.9671 0.000E+00 0.0000 0.9500 0.6616 2.8865 0.2500 1.0000 1.0000 1.2896 576.5453 2.8865 602.7002 0.2500 250.0000 1.3507 428.0799 0.7344 0.3811 0.6233 0.6595 0.2513 3.1831 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 2.1436 0.8169 1.0000 1.2434 350.6396 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 2.0000 711.1279 0.5689 0.0813 0.6200 2.8352 0.0000 7.0000 711.1279 0.000E+00 0.0000 0.9500 0.5890 2.8865 0.2500 1.0000 1.0000 1.2013 577.7279 2.8865 561.9992 0.2500 250.0000 1.4187 449.6393 0.7369 0.3743 0.6233 0.6737 0.2522 3.1721 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 2.3579 0.8986 1.0000 1.2777 360.3192 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 2.0000 691.7686 0.5534 0.0719 0.5484 2.8352 0.0000 7.0000 691.7686 0.000E+00 0.0000 0.9500 0.5209 2.8865 0.2500 1.0000 1.0000 1.1034 578.9789 2.8865 516.7643 0.2500 250.0000 1.4854 470.7663 0.7338 0.3673 0.6233 0.6837 0.2511 3.1857 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 2.5937 0.9884 1.0000 1.3130 370.2661 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 2.0000 671.8749 0.5375 0.0632 0.4816 2.8352 0.0000 7.0000 671.8749 0.000E+00 0.0000 0.9500 0.4575 2.8865 0.2500 1.0000 1.0000 0.9931 580.3044 2.8865 465.6242 0.2500 250.0000 1.5509 491.5315 0.7237 0.3600 0.6233 0.6880 0.2477 3.2302 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 2.8531 1.0873 1.0000 1.3492 380.4875 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 2.0000 651.4321 0.5211 0.0551 0.4198 2.8352 0.0000 7.0000 651.4321 0.000E+00 0.0000 0.9500 0.3988 2.8865 0.2500 1.0000 1.0000 0.8655 581.7114 2.8865 406.2924 0.2500 250.0000 1.6155 511.9933 0.7043 0.3524 0.6233 0.6839 0.2410 3.3190 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 3.1384 1.1960 1.0000 1.3865 390.9911 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 2.0000 630.4249 0.5043 0.0476 0.3628 2.8352 0.0000 7.0000 630.4249 0.000E+00 0.0000 0.9500 0.3447 2.8865 0.2500 1.0000 1.0000 0.7113 583.2076 2.8865 334.3551 0.2500 250.0000 1.6792 532.2010 0.6711 0.3446 0.6233 0.6666 0.2297 3.4829 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 3.4523 1.3156 1.0000 1.4248 401.7847 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 2.0000 608.8377 0.4871 0.0408 0.3107 2.8352 0.0000 7.0000 608.8377 0.000E+00 0.0000 0.9500 0.2952 2.8865 0.2500 1.0000 1.0000 0.5068 584.8023 2.8865 238.5524 0.2500 250.0000 1.7423 552.1966 0.6124 0.3364 0.6233 0.6231 0.2096 3.8167 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 3.7975 1.4472 1.0000 1.4641 412.8762 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 2.0000 586.6547 0.4693 0.0346 0.2634 2.8352 0.0000 7.0000 586.6547 0.000E+00 0.0000 0.9500 0.2503 2.8865 0.2500 1.0000 1.0000 0.0398 586.5058 2.8865 18.7745 0.2500 250.0000 1.8049 572.0166 0.4230 0.3279 0.6233 0.4415 0.1448 5.5263 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 4.1772 1.5919 1.0000 1.5045 424.2739 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 2.0000 563.8593 0.4511 0.0290 0.2209 2.8352 0.0000 7.0000 563.8593 0.000E+00 0.0000 0.9500 0.2098 2.8865 0.2500 1.0000 1.0000 Err:502 Err:502 Err:502 Err:502 0.2500 250.0000 1.8669 591.6924 Err:502 Err:502 0.6233 Err:502 Err:502 Err:502 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 4.5950 1.7511 1.0000 1.5461 435.9863 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 2.0000 540.4346 0.4323 0.0240 0.1829 2.8352 0.0000 7.0000 540.4346 0.000E+00 0.0000 0.9500 0.1737 2.8865 0.2500 1.0000 1.0000 Err:502 Err:502 Err:502 Err:502 0.2500 250.0000 1.9287 611.2519 Err:502 Err:502 0.6233 Err:502 Err:502 Err:502 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 5.0545 1.9262 1.0000 1.5887 448.0220 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 2.0000 516.3632 0.4131 0.0196 0.1493 2.8352 0.0000 7.0000 516.3632 0.000E+00 0.0000 0.9500 0.1419 2.8865 0.2500 1.0000 1.0000 Err:502 Err:502 Err:502 Err:502 0.2500 250.0000 1.9901 630.7198 Err:502 Err:502 0.6233 Err:502 Err:502 Err:502 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 5.5599 2.1188 1.0000 1.6326 460.3899 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 2.0000 491.6273 0.3933 0.0157 0.1200 2.8352 0.0000 7.0000 491.6273 0.000E+00 0.0000 0.9500 0.1140 2.8865 0.2500 1.0000 1.0000 Err:502 Err:502 Err:502 Err:502 0.2500 250.0000 2.0513 650.1180 Err:502 Err:502 0.6233 Err:502 Err:502 Err:502 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 5.7800 2.2027 1.0000 1.6508 465.5248 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 2.0000 481.3576 0.3851 0.0143 0.1093 2.8352 0.0000 7.0000 481.3576 0.000E+00 0.0000 0.9500 0.1038 2.8865 0.2500 1.0000 1.0000 Err:502 Err:502 Err:502 Err:502 0.2500 250.0000 2.0762 658.0037 Err:502 Err:502 0.6233 Err:502 Err:502 Err:502 M_1 0.8000 0.8000 0.8000 0.8000 0.8000 0.8000 0.8000 0.8000 MW 0.0290 0.0290 0.0290 0.0290 0.0290 0.0290 0.0290 0.0290 T_1 250.0000 250.0000 250.0000 250.0000 250.0000 250.0000 250.0000 250.0000 P_1 0.2500 0.2500 0.2500 0.2500 0.2500 0.2500 0.2500 0.2500 Rgas 286.9865 286.9865 286.9865 286.9865 286.9865 286.9865 286.9865 286.9865 a_1 316.9310 316.9310 316.9310 316.9310 316.9310 316.9310 316.9310 316.9310 u_1 253.5448 253.5448 253.5448 253.5448 253.5448 253.5448 253.5448 253.5448 S_1 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 T_2 282.0000 282.0000 282.0000 282.0000 282.0000 282.0000 282.0000 282.0000 n_diffuser 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 P_2 0.3811 0.3811 0.3811 0.3811 0.3811 0.3811 0.3811 0.3811 S_2 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 Pi_c 20.0000 20.0000 20.0000 20.0000 20.0000 20.0000 20.0000 20.0000 n_comp 0.9000 0.9000 0.9000 0.9000 0.9000 0.9000 0.9000 0.9000 Tau_comp 2.4241 2.4241 2.4241 2.4241 2.4241 2.4241 2.4241 2.4241 T_3 683.5929 683.5929 683.5929 683.5929 683.5929 683.5929 683.5929 683.5929 P_3 7.6217 7.6217 7.6217 7.6217 7.6217 7.6217 7.6217 7.6217 S_3 0.2199 0.2199 0.2199 0.2199 0.2199 0.2199 0.2199 0.2199 Pi_fan 1.1000 1.1000 1.1000 1.1000 1.1000 1.1000 1.1000 1.1000 P_3_fan 0.4192 0.4192 0.4192 0.4192 0.4192 0.4192 0.4192 0.4192 n_fan 1.0000 0.9500 0.9000 0.8500 0.8000 0.7500 0.7000 0.6500 Tau_fan 1.0276 1.0291 1.0307 1.0325 1.0345 1.0368 1.0394 1.0425 T_3_fan 289.7848 290.1945 290.6498 291.1586 291.7310 292.3797 293.1211 293.9766 Tau_lamda 5.0000 5.0000 5.0000 5.0000 5.0000 5.0000 5.0000 5.0000 T_4 1250.0000 1250.0000 1250.0000 1250.0000 1250.0000 1250.0000 1250.0000 1250.0000 q_in 7.044E+05 7.044E+05 7.044E+05 7.044E+05 7.044E+05 7.044E+05 7.044E+05 7.044E+05 Pi_burner 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 P_4 7.6217 7.6217 7.6217 7.6217 7.6217 7.6217 7.6217 7.6217 S_4 2.8352 2.8352 2.8352 2.8352 2.8352 2.8352 2.8352 2.8352 n_turb 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 alpha 2.0000 2.0000 2.0000 2.0000 2.0000 2.0000 2.0000 2.0000 T_5 832.8375 832.0181 831.1076 830.0899 828.9451 827.6477 826.1648 824.4539 Tau_turb 0.6663 0.6656 0.6649 0.6641 0.6632 0.6621 0.6609 0.6596 Pi_turb 0.1643 0.1635 0.1628 0.1619 0.1609 0.1598 0.1585 0.1570 P_5 1.2520 1.2465 1.2405 1.2337 1.2262 1.2177 1.2080 1.1969 S_5 2.8352 2.8352 2.8352 2.8352 2.8352 2.8352 2.8352 2.8352 Afterburn 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 Tau_lam_ab 7.0000 7.0000 7.0000 7.0000 7.0000 7.0000 7.0000 7.0000 T_7 832.8375 832.0181 831.1076 830.0899 828.9451 827.6477 826.1648 824.4539 q_in_ab 0.000E+00 0.000E+00 0.000E+00 0.000E+00 0.000E+00 0.000E+00 0.000E+00 0.000E+00 q_ab/q_b 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 Pi_ab 0.9500 0.9500 0.9500 0.9500 0.9500 0.9500 0.9500 0.9500 P_7 1.1894 1.1842 1.1784 1.1720 1.1649 1.1568 1.1476 1.1370 S_7 2.8865 2.8865 2.8865 2.8865 2.8865 2.8865 2.8865 2.8865 P_9 0.2500 0.2500 0.2500 0.2500 0.2500 0.2500 0.2500 0.2500 Pe/Pa 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 n_nozzle 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 M_9 1.6947 1.6919 1.6887 1.6851 1.6811 1.6765 1.6713 1.6653 T_9 570.6189 570.6630 570.7119 570.7667 570.8285 570.8985 570.9788 571.0715 S_9 2.8865 2.8865 2.8865 2.8865 2.8865 2.8865 2.8865 2.8865 u_9 787.9333 786.6349 785.1897 783.5711 781.7462 779.6725 777.2956 774.5437 P_9_fan 0.2500 0.2500 0.2500 0.2500 0.2500 0.2500 0.2500 0.2500 T_9_fan 250.0000 250.3535 250.7462 251.1852 251.6790 252.2387 252.8783 253.6163 M_9_fan 0.8920 0.8920 0.8920 0.8920 0.8920 0.8920 0.8920 0.8920 u_9_fan 282.7081 282.9079 283.1298 283.3775 283.6559 283.9711 284.3309 284.7455 Specific_thrust 0.6234 0.6224 0.6214 0.6202 0.6189 0.6174 0.6156 0.6136 Thermal_eff 0.4173 0.4160 0.4145 0.4129 0.4111 0.4091 0.4068 0.4041 Ideal thermal eff 0.6233 0.6233 0.6233 0.6233 0.6233 0.6233 0.6233 0.6233 Propulsive_eff 0.5113 0.5121 0.5130 0.5140 0.5152 0.5165 0.5180 0.5197 Overall_eff 0.2133 0.2130 0.2127 0.2123 0.2118 0.2113 0.2107 0.2100 TSFC 3.7497 3.7554 3.7618 3.7690 3.7771 3.7864 3.7971 3.8096 Thrust & fuel consumption 3.0 2.8 2.5 2.3 2.0 1.8 1.5 1.3 1.0 0.8 0.5 0.3 0.0 0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 Fan efficiency (alpha = 2 = const.) Specific thrust & TSFC Specific_thrust TSFC T-s diagram 2000 Temperature (K) 1600 1200 800 400 0 Co Co Co Co Co Co Co Co Co Co Co Co Co Co Co Co Co Co Co Co lu lu lu lu lu lu lu lu lu lu lu lu lu lu lu lu lu lu lu lu mmmmmmmmmmmmmmmmmmmm Dimensionless entropy (S-S1)/R Row 3 Row 49 Row 9 Row 16 Row 25 Row 32 Row 39 Effect of fan efficiency (alpha = 2 = const., pi_c = 2 = const.) 0.8000 0.8000 0.8000 0.8000 0.8000 0.8000 0.8000 0.0290 0.0290 0.0290 0.0290 0.0290 0.0290 0.0290 250.0000 250.0000 250.0000 250.0000 250.0000 250.0000 250.0000 0.2500 0.2500 0.2500 0.2500 0.2500 0.2500 0.2500 286.9865 286.9865 286.9865 286.9865 286.9865 286.9865 286.9865 316.9310 316.9310 316.9310 316.9310 316.9310 316.9310 316.9310 253.5448 253.5448 253.5448 253.5448 253.5448 253.5448 253.5448 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 282.0000 282.0000 282.0000 282.0000 282.0000 282.0000 282.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 0.3811 0.3811 0.3811 0.3811 0.3811 0.3811 0.3811 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 20.0000 20.0000 20.0000 20.0000 20.0000 20.0000 20.0000 0.9000 0.9000 0.9000 0.9000 0.9000 0.9000 0.9000 2.4241 2.4241 2.4241 2.4241 2.4241 2.4241 2.4241 683.5929 683.5929 683.5929 683.5929 683.5929 683.5929 683.5929 7.6217 7.6217 7.6217 7.6217 7.6217 7.6217 7.6217 0.2199 0.2199 0.2199 0.2199 0.2199 0.2199 0.2199 1.1000 1.1000 1.1000 1.1000 1.1000 1.1000 1.1000 0.4192 0.4192 0.4192 0.4192 0.4192 0.4192 0.4192 0.6000 0.5500 0.5000 0.4500 0.4000 0.3500 0.3370 1.0460 1.0502 1.0552 1.0613 1.0690 1.0789 1.0819 294.9747 296.1542 297.5696 299.2995 301.4620 304.2423 305.1003 5.0000 5.0000 5.0000 5.0000 5.0000 5.0000 5.0000 1250.0000 1250.0000 1250.0000 1250.0000 1250.0000 1250.0000 1250.0000 7.044E+05 7.044E+05 7.044E+05 7.044E+05 7.044E+05 7.044E+05 7.044E+05 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 7.6217 7.6217 7.6217 7.6217 7.6217 7.6217 7.6217 2.8352 2.8352 2.8352 2.8352 2.8352 2.8352 2.8352 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 2.0000 2.0000 2.0000 2.0000 2.0000 2.0000 2.0000 822.4578 820.0988 817.2679 813.8080 809.4831 803.9226 802.2066 0.6580 0.6561 0.6538 0.6510 0.6476 0.6431 0.6418 0.1554 0.1534 0.1510 0.1482 0.1447 0.1404 0.1390 1.1841 1.1690 1.1512 1.1297 1.1032 1.0699 1.0598 2.8352 2.8352 2.8352 2.8352 2.8352 2.8352 2.8352 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 7.0000 7.0000 7.0000 7.0000 7.0000 7.0000 7.0000 822.4578 820.0988 817.2679 813.8080 809.4831 803.9226 802.2066 0.000E+00 0.000E+00 0.000E+00 0.000E+00 0.000E+00 0.000E+00 0.000E+00 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.9500 0.9500 0.9500 0.9500 0.9500 0.9500 0.9500 1.1249 1.1106 1.0936 1.0732 1.0480 1.0164 1.0068 2.8865 2.8865 2.8865 2.8865 2.8865 2.8865 2.8865 0.2500 0.2500 0.2500 0.2500 0.2500 0.2500 0.2500 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.6582 1.6498 1.6396 1.6271 1.6114 1.5909 1.5846 571.1800 571.3086 571.4635 571.6535 571.8923 572.2013 572.2971 2.8865 2.8865 2.8865 2.8865 2.8865 2.8865 2.8865 771.3203 767.4928 762.8736 757.1885 750.0196 740.6972 737.7957 0.2500 0.2500 0.2500 0.2500 0.2500 0.2500 0.2500 254.4773 255.4949 256.7160 258.2085 260.0740 262.4726 263.2128 0.8920 0.8920 0.8920 0.8920 0.8920 0.8920 0.8920 285.2285 285.7982 286.4803 287.3119 288.3479 289.6745 290.0827 0.6112 0.6084 0.6050 0.6007 0.5954 0.5884 0.5862 0.4009 0.3972 0.3927 0.3873 0.3804 0.3717 0.3690 0.6233 0.6233 0.6233 0.6233 0.6233 0.6233 0.6233 0.5218 0.5242 0.5272 0.5309 0.5356 0.5418 0.5437 0.2092 0.2082 0.2070 0.2056 0.2038 0.2014 0.2006 3.8244 3.8422 3.8639 3.8911 3.9262 3.9730 3.9878 M_1 0.8000 MW 0.0290 T_1 250.0000 P_1 0.2500 Rgas 286.9865 a_1 316.9310 u_1 253.5448 S_1 0.0000 T_2 282.0000 n_diffuser 1.0000 P_2 0.3811 S_2 0.0000 Pi_c 20.0000 n_comp 0.9000 Tau_comp 2.4241 T_3 683.5929 P_3 7.6217 S_3 0.2199 Pi_fan 1.1000 P_3_fan 0.4192 n_fan 1.0000 Tau_fan 1.0276 T_3_fan 289.7848 Tau_lamda 5.0000 T_4 1250.0000 q_in 7.044E+05 Pi_burner 1.0000 P_4 7.6217 S_4 2.8352 n_turb 1.0000 alpha 0.0000 T_5 848.4071 Tau_turb 0.6787 Pi_turb 0.1784 P_5 1.3595 S_5 2.8352 Afterburn 0.0000 Tau_lam_ab 7.0000 T_7 848.4071 q_in_ab 0.000E+00 q_ab/q_b 0.0000 Pi_ab 0.9500 P_7 1.2915 S_7 2.8865 P_9 0.2500 Pe/Pa 1.0000 n_nozzle 1.0000 M_9 1.7482 T_9 569.7912 S_9 2.8865 u_9 812.1956 P_9_fan 0.2500 T_9_fan 250.0000 M_9_fan 0.8920 u_9_fan 282.7081 Specific_thrust 1.7627 Thermal_eff 0.4226 Ideal thermal eff 0.6233 Propulsive_eff 0.4758 Overall_eff 0.2011 TSFC 3.9784 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 0.9800 0.3551 0.0707 20.0000 0.9000 2.4241 683.5929 7.1014 0.2906 1.1000 0.3906 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.1014 2.9059 1.0000 0.0000 848.4071 0.6787 0.1784 1.2667 2.9059 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2034 2.9572 0.2500 1.0000 1.0000 1.7023 579.6426 2.9572 797.7075 0.2500 255.1020 0.8245 263.9590 1.7170 0.4061 0.6156 0.4824 0.1959 4.0843 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 0.9600 0.3303 0.1429 20.0000 0.9000 2.4241 683.5929 6.6070 0.3627 1.1000 0.3634 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 6.6070 2.9781 1.0000 0.0000 848.4071 0.6787 0.1784 1.1785 2.9781 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.1196 3.0294 0.2500 1.0000 1.0000 1.6551 589.8728 3.0294 782.3784 0.2500 260.4167 0.7509 242.8946 1.6686 0.3889 0.6076 0.4895 0.1904 4.2027 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 0.9400 0.3069 0.2166 20.0000 0.9000 2.4241 683.5929 6.1376 0.4364 1.1000 0.3376 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 6.1376 3.0518 1.0000 0.0000 848.4071 0.6787 0.1784 1.0948 3.0518 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.0400 3.1031 0.2500 1.0000 1.0000 1.6063 600.5046 3.1031 766.1224 0.2500 265.9574 0.6693 218.7850 1.6173 0.3710 0.5993 0.4973 0.1845 4.3360 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 0.9200 0.2846 0.2918 20.0000 0.9000 2.4241 683.5929 5.6926 0.5117 1.1000 0.3131 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 5.6926 3.1270 1.0000 0.0000 848.4071 0.6787 0.1784 1.0154 3.1270 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.9646 3.1783 0.2500 1.0000 1.0000 1.5558 611.5631 3.1783 748.8399 0.2500 271.7391 0.5762 190.3997 1.5628 0.3524 0.5906 0.5059 0.1783 4.4873 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 0.9000 0.2636 0.3688 20.0000 0.9000 2.4241 683.5929 5.2711 0.5886 1.1000 0.2899 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 5.2711 3.2040 1.0000 0.0000 848.4071 0.6787 0.1784 0.9402 3.2040 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.8932 3.2552 0.2500 1.0000 1.0000 1.5034 623.0750 3.2552 730.4144 0.2500 277.7778 0.4649 155.3092 1.5046 0.3331 0.5815 0.5154 0.1716 4.6607 Thrust & fuel consumption 7 Specific thrust & TSFC 6 5 4 3 2 1 0 0.6 0.7 0.7 0.8 0.8 0.9 0.9 1.0 1.0 Specific_thrust TSFC Diffuser efficiency T-s diagram 2000 Temperature (K) 1600 1200 800 400 0 Co lu m n Row 3 Co lu m n Co lu m n Co lu m n Co Co Co Co Co Co Co Co Co Co Co Co lu lu lu lu lu lu lu lu lu lu lu lu mmmmmmmmmmmm n n n nI nJ n n n n n n n Dimensionless entropy (S-S1)/R Row 16 Row 25 Row 32 Row 39 Co lu m n Co lu m n Co lu m n Co lu m n Row 9 Row 49 Effect of diffuser efficiency 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 0.8800 0.2436 0.4474 20.0000 0.9000 2.4241 683.5929 4.8724 0.6673 1.1000 0.2680 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 4.8724 3.2826 1.0000 0.0000 848.4071 0.6787 0.1784 0.8691 3.2826 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.8256 3.3339 0.2500 1.0000 1.0000 1.4490 635.0697 3.3339 710.7081 0.2500 284.0909 0.3166 106.9508 1.4425 0.3129 0.5720 0.5259 0.1646 4.8616 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 0.8600 0.2248 0.5279 20.0000 0.9000 2.4241 683.5929 4.4957 0.7477 1.1000 0.2473 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 4.4957 3.3631 1.0000 0.0000 848.4071 0.6787 0.1784 0.8019 3.3631 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.7618 3.4144 0.2500 1.0000 1.0000 1.3922 647.5791 3.4144 689.5565 0.2500 290.6977 Err:502 Err:502 Err:502 Err:502 0.5620 Err:502 Err:502 Err:502 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 0.8400 0.2070 0.6102 20.0000 0.9000 2.4241 683.5929 4.1403 0.8301 1.1000 0.2277 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 4.1403 3.4454 1.0000 0.0000 848.4071 0.6787 0.1784 0.7385 3.4454 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.7016 3.4967 0.2500 1.0000 1.0000 1.3328 660.6381 3.4967 666.7601 0.2500 297.6190 Err:502 Err:502 Err:502 Err:502 0.5516 Err:502 Err:502 Err:502 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 0.8200 0.1903 0.6946 20.0000 0.9000 2.4241 683.5929 3.8054 0.9144 1.1000 0.2093 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 3.8054 3.5298 1.0000 0.0000 848.4071 0.6787 0.1784 0.6788 3.5298 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.6448 3.5811 0.2500 1.0000 1.0000 1.2704 674.2849 3.5811 642.0737 0.2500 304.8780 Err:502 Err:502 Err:502 Err:502 0.5406 Err:502 Err:502 Err:502 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 0.8000 0.1745 0.7810 20.0000 0.9000 2.4241 683.5929 3.4903 1.0009 1.1000 0.1920 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 3.4903 3.6162 1.0000 0.0000 848.4071 0.6787 0.1784 0.6226 3.6162 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.5915 3.6675 0.2500 1.0000 1.0000 1.2045 688.5610 3.6675 615.1892 0.2500 312.5000 Err:502 Err:502 Err:502 Err:502 0.5292 Err:502 Err:502 Err:502 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 0.7800 0.1597 0.8696 20.0000 0.9000 2.4241 683.5929 3.1944 1.0895 1.1000 0.1757 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 3.1944 3.7048 1.0000 0.0000 848.4071 0.6787 0.1784 0.5698 3.7048 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.5413 3.7561 0.2500 1.0000 1.0000 1.1346 703.5126 3.7561 585.7115 0.2500 320.5128 Err:502 Err:502 Err:502 Err:502 0.5171 Err:502 Err:502 Err:502 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 0.7600 0.1458 0.9605 20.0000 0.9000 2.4241 683.5929 2.9168 1.1804 1.1000 0.1604 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 2.9168 3.7957 1.0000 0.0000 848.4071 0.6787 0.1784 0.5203 3.7957 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.4943 3.8470 0.2500 1.0000 1.0000 1.0597 719.1900 3.8470 553.1180 0.2500 328.9474 Err:502 Err:502 Err:502 Err:502 0.5044 Err:502 Err:502 Err:502 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 0.7400 0.1328 1.0539 20.0000 0.9000 2.4241 683.5929 2.6568 1.2737 1.1000 0.1461 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 2.6568 3.8891 1.0000 0.0000 848.4071 0.6787 0.1784 0.4739 3.8891 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.4502 3.9404 0.2500 1.0000 1.0000 0.9788 735.6490 3.9404 516.6918 0.2500 337.8378 Err:502 Err:502 Err:502 Err:502 0.4910 Err:502 Err:502 Err:502 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 0.7280 0.1255 1.1111 20.0000 0.9000 2.4241 683.5929 2.5091 1.3310 1.1000 0.1380 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 2.5091 3.9463 1.0000 0.0000 848.4071 0.6787 0.1784 0.4475 3.9463 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.4252 3.9976 0.2500 1.0000 1.0000 0.9267 745.9251 3.9976 492.5855 0.2500 343.4066 Err:502 Err:502 Err:502 Err:502 0.4826 Err:502 Err:502 Err:502 M_1 0.8000 MW 0.0290 T_1 250.0000 P_1 0.2500 Rgas 286.9865 a_1 316.9310 u_1 253.5448 S_1 0.0000 T_2 282.0000 n_diffuser 1.0000 P_2 0.3811 S_2 0.0000 Pi_c 20.0000 n_comp 0.9000 Tau_comp 2.4241 T_3 683.5929 P_3 7.6217 S_3 0.2199 Pi_fan 1.1000 P_3_fan 0.4192 n_fan 1.0000 Tau_fan 1.0276 T_3_fan 289.7848 Tau_lamda 5.0000 T_4 1250.0000 q_in 7.044E+05 Pi_burner 1.0000 P_4 7.6217 S_4 2.8352 n_turb 1.0000 alpha 0.0000 T_5 848.4071 Tau_turb 0.6787 Pi_turb 0.1784 P_5 1.3595 S_5 2.8352 Afterburn 0.0000 Tau_lam_ab 7.0000 T_7 848.4071 q_in_ab 0.000E+00 q_ab/q_b 0.0000 Pi_ab 0.9500 P_7 1.2915 S_7 2.8865 P_9 0.2500 Pe/Pa 1.0000 n_nozzle 1.0000 M_9 1.7482 T_9 569.7912 S_9 2.8865 u_9 812.1956 P_9_fan 0.2500 T_9_fan 250.0000 M_9_fan 0.8920 u_9_fan 282.7081 Specific_thrust 1.7627 Thermal_eff 0.4226 Ideal thermal eff 0.6233 Propulsive_eff 0.4758 Overall_eff 0.2011 TSFC 3.9784 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.8700 2.4732 697.4409 7.6217 0.2927 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 6.872E+05 1.0000 7.6217 2.8211 1.0000 0.0000 834.5591 0.6676 0.1658 1.2635 2.8211 0.0000 7.0000 834.5591 0.000E+00 0.0000 0.9500 1.2004 2.8724 0.2500 1.0000 1.0000 1.7007 570.5266 2.8724 790.6539 0.2500 250.0000 0.8920 282.7081 1.6947 0.4081 0.6233 0.4856 0.1982 4.0368 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.8400 2.5258 712.2781 7.6217 0.3691 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 6.687E+05 1.0000 7.6217 2.8063 1.0000 0.0000 819.7219 0.6558 0.1531 1.1666 2.8063 0.0000 7.0000 819.7219 0.000E+00 0.0000 0.9500 1.1083 2.8576 0.2500 1.0000 1.0000 1.6484 571.3292 2.8576 766.8795 0.2500 250.0000 0.8920 282.7081 1.6197 0.3917 0.6233 0.4969 0.1946 4.1103 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.8100 2.5823 728.2143 7.6217 0.4495 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 6.489E+05 1.0000 7.6217 2.7908 1.0000 0.0000 803.7857 0.6430 0.1403 1.0691 2.7908 0.0000 7.0000 803.7857 0.000E+00 0.0000 0.9500 1.0156 2.8421 0.2500 1.0000 1.0000 1.5904 572.2089 2.8421 740.4661 0.2500 250.0000 0.8920 282.7081 1.5364 0.3729 0.6233 0.5101 0.1903 4.2049 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.7800 2.6432 745.3764 7.6217 0.5341 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 6.276E+05 1.0000 7.6217 2.7745 1.0000 0.0000 786.6236 0.6293 0.1274 0.9712 2.7745 0.0000 7.0000 786.6236 0.000E+00 0.0000 0.9500 0.9226 2.8258 0.2500 1.0000 1.0000 1.5256 573.1776 2.8258 710.8888 0.2500 250.0000 0.8920 282.7081 1.4430 0.3514 0.6233 0.5258 0.1848 4.3296 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.7500 2.7089 763.9115 7.6217 0.6233 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 6.045E+05 1.0000 7.6217 2.7572 1.0000 0.0000 768.0885 0.6145 0.1146 0.8735 2.7572 0.0000 7.0000 768.0885 0.000E+00 0.0000 0.9500 0.8298 2.8085 0.2500 1.0000 1.0000 1.4525 574.2497 2.8085 677.4513 0.2500 250.0000 0.8920 282.7081 1.3375 0.3264 0.6233 0.5447 0.1778 4.4995 Thrust & fuel consumption 7 Specific thrust & TSFC 6 5 4 3 2 1 0 0.6 0.7 0.7 0.8 0.8 0.9 0.9 1.0 1.0 Specific_thrust TSFC Compressor efficiency T-s diagram 2000 Temperature (K) 1600 1200 800 400 0 Co lu m n Row 3 Co lu m n Co lu m n Co lu m n Co Co Co Co Co Co Co Co Co Co Co Co lu lu lu lu lu lu lu lu lu lu lu lu mmmmmmmmmmmm n n n nI nJ n n n n n n n Dimensionless entropy (S-S1)/R Row 16 Row 25 Row 32 Row 39 Co lu m n Co lu m n Co lu m n Co lu m n Row 9 Row 49 Effect of compressor efficiency 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.7200 2.7801 783.9911 7.6217 0.7175 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 5.795E+05 1.0000 7.6217 2.7390 1.0000 0.0000 748.0089 0.5984 0.1019 0.7764 2.7390 0.0000 7.0000 748.0089 0.000E+00 0.0000 0.9500 0.7376 2.7903 0.2500 1.0000 1.0000 1.3690 575.4431 2.7903 639.1974 0.2500 250.0000 0.8920 282.7081 1.2168 0.2970 0.6233 0.5680 0.1687 4.7415 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.6900 2.8575 805.8168 7.6217 0.8172 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 5.524E+05 1.0000 7.6217 2.7198 1.0000 0.0000 726.1832 0.5809 0.0893 0.6806 2.7198 0.0000 7.0000 726.1832 0.000E+00 0.0000 0.9500 0.6465 2.7711 0.2500 1.0000 1.0000 1.2724 576.7801 2.7711 594.7541 0.2500 250.0000 0.8920 282.7081 1.0766 0.2620 0.6233 0.5978 0.1566 5.1081 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.6600 2.9419 829.6267 7.6217 0.9230 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 5.228E+05 1.0000 7.6217 2.6993 1.0000 0.0000 702.3733 0.5619 0.0770 0.5868 2.6993 0.0000 7.0000 702.3733 0.000E+00 0.0000 0.9500 0.5574 2.7506 0.2500 1.0000 1.0000 1.1580 578.2890 2.7506 542.0211 0.2500 250.0000 0.8920 282.7081 0.9102 0.2195 0.6233 0.6374 0.1399 5.7180 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.6300 3.0344 855.7041 7.6217 1.0354 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 4.903E+05 1.0000 7.6217 2.6776 1.0000 0.0000 676.2959 0.5410 0.0651 0.4959 2.6776 0.0000 7.0000 676.2959 0.000E+00 0.0000 0.9500 0.4711 2.7289 0.2500 1.0000 1.0000 1.0186 580.0062 2.7289 477.4715 0.2500 250.0000 0.8920 282.7081 0.7065 0.1669 0.6233 0.6937 0.1158 6.9093 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.6000 3.1361 884.3894 7.6217 1.1551 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 4.547E+05 1.0000 7.6217 2.6545 1.0000 0.0000 647.6106 0.5181 0.0537 0.4089 2.6545 0.0000 7.0000 647.6106 0.000E+00 0.0000 0.9500 0.3885 2.7058 0.2500 1.0000 1.0000 0.8395 581.9796 2.7058 394.1960 0.2500 250.0000 0.8920 282.7081 0.4438 0.1002 0.6233 0.7829 0.0784 10.1999 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.5700 3.2486 916.0941 7.6217 1.2830 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 4.152E+05 1.0000 7.6217 2.6297 1.0000 0.0000 615.9059 0.4927 0.0429 0.3271 2.6297 0.0000 7.0000 615.9059 0.000E+00 0.0000 0.9500 0.3107 2.6810 0.2500 1.0000 1.0000 0.5817 584.2736 2.6810 273.6678 0.2500 250.0000 0.8920 282.7081 0.0635 0.0128 0.6233 0.9618 0.0123 65.1104 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.5400 3.3735 951.3215 7.6217 1.4201 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 3.714E+05 1.0000 7.6217 2.6033 1.0000 0.0000 580.6785 0.4645 0.0330 0.2517 2.6033 0.0000 7.0000 580.6785 0.000E+00 0.0000 0.9500 0.2391 2.6546 0.2500 1.0000 1.0000 Err:502 Err:502 Err:502 Err:502 0.2500 250.0000 0.8920 282.7081 Err:502 Err:502 0.6233 Err:502 Err:502 Err:502 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.5100 3.5131 990.6934 7.6217 1.5673 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 3.225E+05 1.0000 7.6217 2.5748 1.0000 0.0000 541.3066 0.4330 0.0242 0.1842 2.5748 0.0000 7.0000 541.3066 0.000E+00 0.0000 0.9500 0.1750 2.6261 0.2500 1.0000 1.0000 Err:502 Err:502 Err:502 Err:502 0.2500 250.0000 0.8920 282.7081 Err:502 Err:502 0.6233 Err:502 Err:502 Err:502 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.4800 3.6702 1034.9867 7.6217 1.7262 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 2.674E+05 1.0000 7.6217 2.5441 1.0000 0.0000 497.0133 0.3976 0.0165 0.1260 2.5441 0.0000 7.0000 497.0133 0.000E+00 0.0000 0.9500 0.1197 2.5954 0.2500 1.0000 1.0000 Err:502 Err:502 Err:502 Err:502 0.2500 250.0000 0.8920 282.7081 Err:502 Err:502 0.6233 Err:502 Err:502 Err:502 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.4500 3.8482 1085.1858 7.6217 1.8982 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 2.050E+05 1.0000 7.6217 2.5109 1.0000 0.0000 446.8142 0.3575 0.0103 0.0785 2.5109 0.0000 7.0000 446.8142 0.000E+00 0.0000 0.9500 0.0745 2.5622 0.2500 1.0000 1.0000 Err:502 Err:502 Err:502 Err:502 0.2500 250.0000 0.8920 282.7081 Err:502 Err:502 0.6233 Err:502 Err:502 Err:502 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.4200 4.0516 1142.5562 7.6217 2.0853 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 1.336E+05 1.0000 7.6217 2.4747 1.0000 0.0000 389.4438 0.3116 0.0056 0.0426 2.4747 0.0000 7.0000 389.4438 0.000E+00 0.0000 0.9500 0.0404 2.5260 0.2500 1.0000 1.0000 Err:502 Err:502 Err:502 Err:502 0.2500 250.0000 0.8920 282.7081 Err:502 Err:502 0.6233 Err:502 Err:502 Err:502 0.8000 0.8000 0.8000 0.0290 0.0290 0.0290 250.0000 250.0000 250.0000 0.2500 0.2500 0.2500 286.9865 286.9865 286.9865 316.9310 316.9310 316.9310 253.5448 253.5448 253.5448 0.0000 0.0000 0.0000 282.0000 282.0000 282.0000 1.0000 1.0000 1.0000 0.3811 0.3811 0.3811 0.0000 0.0000 0.0000 20.0000 20.0000 20.0000 0.3900 0.3600 0.3300 4.2864 4.5602 4.8839 1208.7529 1285.9823 1377.2534 7.6217 7.6217 7.6217 2.2898 2.5147 2.7637 1.1000 1.1000 1.1000 0.4192 0.4192 0.4192 1.0000 1.0000 1.0000 1.0276 1.0276 1.0276 289.7848 289.7848 289.7848 5.0000 5.0000 5.0000 1250.0000 1250.0000 1250.0000 5.130E+04 -4.475E+04 -1.583E+05 1.0000 1.0000 1.0000 7.6217 7.6217 7.6217 2.4352 2.3917 2.3436 1.0000 1.0000 1.0000 0.0000 0.0000 0.0000 323.2471 246.0177 154.7466 0.2586 0.1968 0.1238 0.0024 0.0007 0.0001 0.0186 0.0055 0.0007 2.4352 2.3917 2.3436 0.0000 0.0000 0.0000 7.0000 7.0000 7.0000 323.2471 246.0177 154.7466 0.000E+00 0.000E+00 0.000E+00 0.0000 0.0000 0.0000 0.9500 0.9500 0.9500 0.0177 0.0052 0.0007 2.4865 2.4430 2.3949 0.2500 0.2500 0.2500 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 Err:502 Err:502 Err:502 Err:502 Err:502 Err:502 Err:502 Err:502 Err:502 Err:502 Err:502 Err:502 0.2500 0.2500 0.2500 250.0000 250.0000 250.0000 0.8920 0.8920 0.8920 282.7081 282.7081 282.7081 Err:502 Err:502 Err:502 Err:502 Err:502 Err:502 0.6233 0.6233 0.6233 Err:502 Err:502 Err:502 Err:502 Err:502 Err:502 Err:502 Err:502 Err:502 M_1 0.8000 MW 0.0290 T_1 250.0000 P_1 0.2500 Rgas 286.9865 a_1 316.9310 u_1 253.5448 S_1 0.0000 T_2 282.0000 n_diffuser 1.0000 P_2 0.3811 S_2 0.0000 Pi_c 20.0000 n_comp 0.9000 Tau_comp 2.4241 T_3 683.5929 P_3 7.6217 S_3 0.2199 Pi_fan 1.1000 P_3_fan 0.4192 n_fan 1.0000 Tau_fan 1.0276 T_3_fan 289.7848 Tau_lamda 5.0000 T_4 1250.0000 q_in 7.044E+05 Pi_burner 1.0000 P_4 7.6217 S_4 2.8352 n_turb 1.0000 alpha 0.0000 T_5 848.4071 Tau_turb 0.6787 Pi_turb 0.1784 P_5 1.3595 S_5 2.8352 Afterburn 0.0000 Tau_lam_ab 7.0000 T_7 848.4071 q_in_ab 0.000E+00 q_ab/q_b 0.0000 Pi_ab 0.9500 P_7 1.2915 S_7 2.8865 P_9 0.2500 Pe/Pa 1.0000 n_nozzle 1.0000 M_9 1.7482 T_9 569.7912 S_9 2.8865 u_9 812.1956 P_9_fan 0.2500 T_9_fan 250.0000 M_9_fan 0.8920 u_9_fan 282.7081 Specific_thrust 1.7627 Thermal_eff 0.4226 Ideal thermal eff 0.6233 Propulsive_eff 0.4758 Overall_eff 0.2011 TSFC 3.9784 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 0.9500 7.2406 2.8865 1.0000 0.0000 848.4071 0.6787 0.1784 1.2915 2.8865 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2270 2.9378 0.2500 1.0000 1.0000 1.7150 576.9207 2.9378 801.7368 0.2500 250.0000 0.8920 282.7081 1.7297 0.4106 0.6233 0.4805 0.1973 4.0543 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 0.9000 6.8595 2.9406 1.0000 0.0000 848.4071 0.6787 0.1784 1.2236 2.9406 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.1624 2.9918 0.2500 1.0000 1.0000 1.6797 584.5323 2.9918 790.4178 0.2500 250.0000 0.8920 282.7081 1.6940 0.3978 0.6233 0.4857 0.1932 4.1398 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 0.8500 6.4784 2.9977 1.0000 0.0000 848.4071 0.6787 0.1784 1.1556 2.9977 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.0978 3.0490 0.2500 1.0000 1.0000 1.6421 592.6883 3.0490 778.1066 0.2500 250.0000 0.8920 282.7081 1.6551 0.3841 0.6233 0.4915 0.1888 4.2369 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 0.8000 6.0974 3.0583 1.0000 0.0000 848.4071 0.6787 0.1784 1.0876 3.0583 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.0332 3.1096 0.2500 1.0000 1.0000 1.6019 601.4633 3.1096 764.6397 0.2500 250.0000 0.8920 282.7081 1.6126 0.3694 0.6233 0.4980 0.1840 4.3486 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 0.7500 5.7163 3.1229 1.0000 0.0000 848.4071 0.6787 0.1784 1.0196 3.1229 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.9686 3.1742 0.2500 1.0000 1.0000 1.5586 610.9476 3.1742 749.8123 0.2500 250.0000 0.8920 282.7081 1.5659 0.3535 0.6233 0.5054 0.1786 4.4785 Thrust & fuel consumption 7 Specific thrust & TSFC 6 5 4 3 2 1 0 0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 Burner pressure ratio Specific_thrust TSFC T-s diagram 2000 Temperature (K) 1600 1200 800 400 0 Co lu m n Row 3 Co lu m n Co lu m n Co lu m n Co Co Co Co Co Co Co Co Co Co Co Co lu lu lu lu lu lu lu lu lu lu lu lu mmmmmmmmmmmm n n n nI nJ n n n n n n n Dimensionless entropy (S-S1)/R Row 16 Row 25 Row 32 Row 39 Co lu m n Co lu m n Co lu m n Co lu m n Row 9 Row 49 Effect of burner pressure ratio 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 0.7000 5.3352 3.1919 1.0000 0.0000 848.4071 0.6787 0.1784 0.9517 3.1919 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.9041 3.2432 0.2500 1.0000 1.0000 1.5117 621.2519 3.2432 733.3631 0.2500 250.0000 0.8920 282.7081 1.5140 0.3361 0.6233 0.5138 0.1727 4.6320 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 0.6500 4.9541 3.2660 1.0000 0.0000 848.4071 0.6787 0.1784 0.8837 3.2660 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.8395 3.3173 0.2500 1.0000 1.0000 1.4606 632.5139 3.3173 714.9525 0.2500 250.0000 0.8920 282.7081 1.4559 0.3172 0.6233 0.5236 0.1661 4.8168 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 0.6000 4.5730 3.3460 1.0000 0.0000 848.4071 0.6787 0.1784 0.8157 3.3460 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.7749 3.3973 0.2500 1.0000 1.0000 1.4043 644.9073 3.3973 694.1283 0.2500 250.0000 0.8920 282.7081 1.3902 0.2964 0.6233 0.5351 0.1586 5.0445 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 0.5500 4.1919 3.4330 1.0000 0.0000 848.4071 0.6787 0.1784 0.7477 3.4330 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.7103 3.4843 0.2500 1.0000 1.0000 1.3418 658.6552 3.4843 670.2715 0.2500 250.0000 0.8920 282.7081 1.3149 0.2733 0.6233 0.5489 0.1500 5.3333 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 0.5000 3.8109 3.5283 1.0000 0.0000 848.4071 0.6787 0.1784 0.6798 3.5283 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.6458 3.5796 0.2500 1.0000 1.0000 1.2715 674.0510 3.5796 642.5048 0.2500 250.0000 0.8920 282.7081 1.2273 0.2474 0.6233 0.5659 0.1400 5.7140 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 0.4500 3.4298 3.6337 1.0000 0.0000 848.4071 0.6787 0.1784 0.6118 3.6337 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.5812 3.6850 0.2500 1.0000 1.0000 1.1909 691.4893 3.6850 609.5283 0.2500 250.0000 0.8920 282.7081 1.1232 0.2181 0.6233 0.5875 0.1281 6.2434 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 0.4000 3.0487 3.7515 1.0000 0.0000 848.4071 0.6787 0.1784 0.5438 3.7515 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.5166 3.8028 0.2500 1.0000 1.0000 1.0966 711.5183 3.8028 569.3007 0.2500 250.0000 0.8920 282.7081 0.9963 0.1844 0.6233 0.6163 0.1137 7.0388 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 0.3500 2.6676 3.8850 1.0000 0.0000 848.4071 0.6787 0.1784 0.4758 3.8850 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.4520 3.9363 0.2500 1.0000 1.0000 0.9824 734.9279 3.9363 518.3414 0.2500 250.0000 0.8920 282.7081 0.8355 0.1451 0.6233 0.6569 0.0953 8.3933 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 0.3000 2.2865 4.0392 1.0000 0.0000 848.4071 0.6787 0.1784 0.4079 4.0392 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.3875 4.0905 0.2500 1.0000 1.0000 0.8369 762.9117 4.0905 449.9137 0.2500 250.0000 0.8920 282.7081 0.6196 0.0981 0.6233 0.7209 0.0707 11.3181 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 0.2500 1.9054 4.2215 1.0000 0.0000 848.4071 0.6787 0.1784 0.3399 4.2215 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.3229 4.2728 0.2500 1.0000 1.0000 0.6324 797.3880 4.2728 347.5554 0.2500 250.0000 0.8920 282.7081 0.2966 0.0401 0.6233 0.8436 0.0338 23.6413 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 0.2000 1.5243 4.4446 1.0000 0.0000 848.4071 0.6787 0.1784 0.2719 4.4446 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.2583 4.4959 0.2500 1.0000 1.0000 0.2230 841.7111 4.4959 125.9118 0.2500 250.0000 0.8920 282.7081 -0.4027 -0.0344 0.6233 1.3364 -0.0459 -17.4134 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 0.1500 1.1433 4.7323 1.0000 0.0000 848.4071 0.6787 0.1784 0.2039 4.7323 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.1937 4.7836 0.2500 1.0000 1.0000 Err:502 Err:502 Err:502 Err:502 0.2500 250.0000 0.8920 282.7081 Err:502 Err:502 0.6233 Err:502 Err:502 Err:502 M_1 0.8000 MW 0.0290 T_1 250.0000 P_1 0.2500 Rgas 286.9865 a_1 316.9310 u_1 253.5448 S_1 0.0000 T_2 282.0000 n_diffuser 1.0000 P_2 0.3811 S_2 0.0000 Pi_c 20.0000 n_comp 0.9000 Tau_comp 2.4241 T_3 683.5929 P_3 7.6217 S_3 0.2199 Pi_fan 1.1000 P_3_fan 0.4192 n_fan 1.0000 Tau_fan 1.0276 T_3_fan 289.7848 Tau_lamda 5.0000 T_4 1250.0000 q_in 7.044E+05 Pi_burner 1.0000 P_4 7.6217 S_4 2.8352 n_turb 1.0000 alpha 0.0000 T_5 848.4071 Tau_turb 0.6787 Pi_turb 0.1784 P_5 1.3595 S_5 2.8352 Afterburn 0.0000 Tau_lam_ab 7.0000 T_7 848.4071 q_in_ab 0.000E+00 q_ab/q_b 0.0000 Pi_ab 0.9500 P_7 1.2915 S_7 2.8865 P_9 0.2500 Pe/Pa 1.0000 n_nozzle 1.0000 M_9 1.7482 T_9 569.7912 S_9 2.8865 u_9 812.1956 P_9_fan 0.2500 T_9_fan 250.0000 M_9_fan 0.8920 u_9_fan 282.7081 Specific_thrust 1.7627 Thermal_eff 0.4226 Ideal thermal eff 0.6233 Propulsive_eff 0.4758 Overall_eff 0.2011 TSFC 3.9784 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 0.9700 0.0000 848.4071 0.6787 0.1670 1.2732 2.9008 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2095 2.9521 0.2500 1.0000 1.0000 1.7057 578.9255 2.9521 798.7711 0.2500 250.0000 0.8920 282.7081 1.7203 0.4073 0.6233 0.4819 0.1963 4.0763 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 0.9400 0.0000 848.4071 0.6787 0.1556 1.1861 2.9717 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.1268 3.0230 0.2500 1.0000 1.0000 1.6593 588.9575 3.0230 783.7621 0.2500 250.0000 0.8920 282.7081 1.6730 0.3904 0.6233 0.4889 0.1909 4.1917 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 0.9100 0.0000 848.4071 0.6787 0.1441 1.0984 3.0485 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.0435 3.0998 0.2500 1.0000 1.0000 1.6085 600.0264 3.0998 766.8611 0.2500 250.0000 0.8920 282.7081 1.6196 0.3718 0.6233 0.4969 0.1848 4.3297 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 0.8800 0.0000 848.4071 0.6787 0.1326 1.0104 3.1320 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.9598 3.1833 0.2500 1.0000 1.0000 1.5524 612.3012 3.1833 747.6721 0.2500 250.0000 0.8920 282.7081 1.5591 0.3512 0.6233 0.5065 0.1779 4.4979 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 0.8500 0.0000 848.4071 0.6787 0.1210 0.9223 3.2232 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.8762 3.2745 0.2500 1.0000 1.0000 1.4902 625.9901 3.2745 725.6743 0.2500 250.0000 0.8920 282.7081 1.4897 0.3282 0.6233 0.5179 0.1699 4.7075 Thrust & fuel consumption 7 Specific thrust & TSFC 6 5 4 3 2 1 0 0.6 0.7 0.7 0.8 0.8 0.9 0.9 1.0 1.0 Specific_thrust TSFC Turbine efficiency T-s diagram 2000 Temperature (K) 1600 1200 800 400 0 Co lu m n Row 3 Co lu m n Co lu m n Co lu m n Co Co Co Co Co Co Co Co Co Co Co Co lu lu lu lu lu lu lu lu lu lu lu lu mmmmmmmmmmmm n n n nI nJ n n n n n n n Dimensionless entropy (S-S1)/R Row 16 Row 25 Row 32 Row 39 Co lu m n Co lu m n Co lu m n Co lu m n Row 9 Row 49 Effect of turbine efficiency 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 0.8200 0.0000 848.4071 0.6787 0.1095 0.8345 3.3232 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.7928 3.3745 0.2500 1.0000 1.0000 1.4205 641.3516 3.3745 700.1661 0.2500 250.0000 0.8920 282.7081 1.4092 0.3024 0.6233 0.5317 0.1608 4.9763 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 0.7900 0.0000 848.4071 0.6787 0.0981 0.7475 3.4334 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.7101 3.4847 0.2500 1.0000 1.0000 1.3416 658.7117 3.4847 670.1717 0.2500 250.0000 0.8920 282.7081 1.3146 0.2732 0.6233 0.5490 0.1500 5.3346 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 0.7600 0.0000 848.4071 0.6787 0.0868 0.6616 3.5554 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.6285 3.6067 0.2500 1.0000 1.0000 1.2511 678.4864 3.6067 634.2798 0.2500 250.0000 0.8920 282.7081 1.2013 0.2399 0.6233 0.5712 0.1370 5.8375 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 0.7300 0.0000 848.4071 0.6787 0.0758 0.5775 3.6913 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.5486 3.7426 0.2500 1.0000 1.0000 1.1454 701.2156 3.7426 590.3358 0.2500 250.0000 0.8920 282.7081 1.0627 0.2017 0.6233 0.6009 0.1212 6.5991 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 0.7000 0.0000 848.4071 0.6787 0.0651 0.4959 3.8438 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.4711 3.8950 0.2500 1.0000 1.0000 1.0186 727.6126 3.8950 534.7875 0.2500 250.0000 0.8920 282.7081 0.8874 0.1574 0.6233 0.6432 0.1012 7.9025 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 0.6700 0.0000 848.4071 0.6787 0.0548 0.4174 4.0160 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.3965 4.0673 0.2500 1.0000 1.0000 0.8600 758.6401 4.0673 461.0160 0.2500 250.0000 0.8920 282.7081 0.6546 0.1052 0.6233 0.7097 0.0747 10.7125 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 0.6400 0.0000 848.4071 0.6787 0.0450 0.3430 4.2124 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.3258 4.2637 0.2500 1.0000 1.0000 0.6439 795.6286 4.2637 353.4976 0.2500 250.0000 0.8920 282.7081 0.3154 0.0431 0.6233 0.8353 0.0360 22.2358 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 0.6100 0.0000 848.4071 0.6787 0.0359 0.2736 4.4385 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.2599 4.4898 0.2500 1.0000 1.0000 0.2429 840.4703 4.4898 137.0816 0.2500 250.0000 0.8920 282.7081 -0.3675 -0.0323 0.6233 1.2981 -0.0419 -19.0835 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 0.5800 0.0000 848.4071 0.6787 0.0276 0.2102 4.7022 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 0.1996 4.7535 0.2500 1.0000 1.0000 Err:502 Err:502 Err:502 Err:502 0.2500 250.0000 0.8920 282.7081 Err:502 Err:502 0.6233 Err:502 Err:502 Err:502 M_1 0.8000 MW 0.0290 T_1 250.0000 P_1 0.2500 Rgas 286.9865 a_1 316.9310 u_1 253.5448 S_1 0.0000 T_2 282.0000 n_diffuser 1.0000 P_2 0.3811 S_2 0.0000 Pi_c 20.0000 n_comp 0.9000 Tau_comp 2.4241 T_3 683.5929 P_3 7.6217 S_3 0.2199 Pi_fan 1.1000 P_3_fan 0.4192 n_fan 1.0000 Tau_fan 1.0276 T_3_fan 289.7848 Tau_lamda 5.0000 T_4 1250.0000 q_in 7.044E+05 Pi_burner 1.0000 P_4 7.6217 S_4 2.8352 n_turb 1.0000 alpha 0.0000 T_5 848.4071 Tau_turb 0.6787 Pi_turb 0.1784 P_5 1.3595 S_5 2.8352 Afterburn 0.0000 Tau_lam_ab 7.0000 T_7 848.4071 q_in_ab 0.000E+00 q_ab/q_b 0.0000 Pi_ab 0.9500 P_7 1.2915 S_7 2.8865 P_9 0.2500 Pe/Pa 1.0000 n_nozzle 1.0000 M_9 1.7482 T_9 569.7912 S_9 2.8865 u_9 812.1956 P_9_fan 0.2500 T_9_fan 250.0000 M_9_fan 0.8920 u_9_fan 282.7081 Specific_thrust 1.7627 Thermal_eff 0.4226 Ideal thermal eff 0.6233 Propulsive_eff 0.4758 Overall_eff 0.2011 TSFC 3.9784 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.2500 1.0000 0.9600 1.6383 593.5325 3.0549 776.8210 0.2500 250.0000 0.8920 282.7081 1.6511 0.3827 0.6233 0.4921 0.1884 4.2473 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.2500 1.0000 0.9200 1.5204 619.3383 3.2304 736.4457 0.2500 250.0000 0.8920 282.7081 1.5237 0.3393 0.6233 0.5122 0.1738 4.6025 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.2500 1.0000 0.8800 1.3926 647.4900 3.4138 689.7094 0.2500 250.0000 0.8920 282.7081 1.3762 0.2920 0.6233 0.5376 0.1570 5.0956 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.2500 1.0000 0.8400 1.2519 678.3229 3.6057 634.5849 0.2500 250.0000 0.8920 282.7081 1.2023 0.2402 0.6233 0.5710 0.1372 5.8328 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.2500 1.0000 0.8000 1.0931 712.2390 3.8070 567.7999 0.2500 250.0000 0.8920 282.7081 0.9916 0.1832 0.6233 0.6174 0.1131 7.0724 Thrust & fuel consumption 7 Specific thrust & TSFC 6 5 4 3 2 1 0 0.6 0.7 0.7 0.8 0.8 0.9 0.9 1.0 1.0 Specific_thrust TSFC Nozzle efficiency T-s diagram 2000 Temperature (K) 1600 1200 800 400 0 Co lu m n Row 3 Co lu m n Co lu m n Co lu m n Co Co Co Co Co Co Co Co Co Co Co Co lu lu lu lu lu lu lu lu lu lu lu lu mmmmmmmmmmmm n n n nI nJ n n n n n n n Dimensionless entropy (S-S1)/R Row 16 Row 25 Row 32 Row 39 Co lu m n Co lu m n Co lu m n Co lu m n Row 9 Row 49 Effect of nozzle efficiency 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.2500 1.0000 0.7600 0.9070 749.7253 4.0185 483.3662 0.2500 250.0000 0.8920 282.7081 0.7251 0.1202 0.6233 0.6881 0.0827 9.6707 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.2500 1.0000 0.7200 0.6711 791.3767 4.2416 367.4607 0.2500 250.0000 0.8920 282.7081 0.3594 0.0502 0.6233 0.8166 0.0410 19.5103 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.2500 1.0000 0.6800 0.2796 837.9283 4.4773 157.5120 0.2500 250.0000 0.8920 282.7081 -0.3030 -0.0280 0.6233 1.2336 -0.0346 -23.1434 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.2500 1.0000 0.6400 Err:502 Err:502 Err:502 Err:502 0.2500 250.0000 0.8920 282.7081 Err:502 Err:502 0.6233 Err:502 Err:502 Err:502 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.2500 1.0000 0.6000 Err:502 Err:502 Err:502 Err:502 0.2500 250.0000 0.8920 282.7081 Err:502 Err:502 0.6233 Err:502 Err:502 Err:502 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.2500 1.0000 0.5600 Err:502 Err:502 Err:502 Err:502 0.2500 250.0000 0.8920 282.7081 Err:502 Err:502 0.6233 Err:502 Err:502 Err:502 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.2500 1.0000 0.5200 Err:502 Err:502 Err:502 Err:502 0.2500 250.0000 0.8920 282.7081 Err:502 Err:502 0.6233 Err:502 Err:502 Err:502 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.2500 1.0000 0.4800 Err:502 Err:502 Err:502 Err:502 0.2500 250.0000 0.8920 282.7081 Err:502 Err:502 0.6233 Err:502 Err:502 Err:502 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.2500 1.0000 0.4400 Err:502 Err:502 Err:502 Err:502 0.2500 250.0000 0.8920 282.7081 Err:502 Err:502 0.6233 Err:502 Err:502 Err:502 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.2500 1.0000 0.4000 Err:502 Err:502 Err:502 Err:502 0.2500 250.0000 0.8920 282.7081 Err:502 Err:502 0.6233 Err:502 Err:502 Err:502 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.2500 1.0000 0.3600 Err:502 Err:502 Err:502 Err:502 0.2500 250.0000 0.8920 282.7081 Err:502 Err:502 0.6233 Err:502 Err:502 Err:502 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.2500 1.0000 0.3200 Err:502 Err:502 Err:502 Err:502 0.2500 250.0000 0.8920 282.7081 Err:502 Err:502 0.6233 Err:502 Err:502 Err:502 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.2500 1.0000 0.2800 Err:502 Err:502 Err:502 Err:502 0.2500 250.0000 0.8920 282.7081 Err:502 Err:502 0.6233 Err:502 Err:502 Err:502 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.2500 1.0000 0.2400 Err:502 Err:502 Err:502 Err:502 0.2500 250.0000 0.8920 282.7081 Err:502 Err:502 0.6233 Err:502 Err:502 Err:502 M_1 0.8000 MW 0.0290 T_1 250.0000 P_1 0.2500 Rgas 286.9865 a_1 316.9310 u_1 253.5448 S_1 0.0000 T_2 282.0000 n_diffuser 1.0000 P_2 0.3811 S_2 0.0000 Pi_c 20.0000 n_comp 0.9000 Tau_comp 2.4241 T_3 683.5929 P_3 7.6217 S_3 0.2199 Pi_fan 1.1000 P_3_fan 0.4192 n_fan 1.0000 Tau_fan 1.0276 T_3_fan 289.7848 Tau_lamda 5.0000 T_4 1250.0000 q_in 7.044E+05 Pi_burner 1.0000 P_4 7.6217 S_4 2.8352 n_turb 1.0000 alpha 0.0000 T_5 848.4071 Tau_turb 0.6787 Pi_turb 0.1784 P_5 1.3595 S_5 2.8352 Afterburn 0.0000 Tau_lam_ab 7.0000 T_7 848.4071 q_in_ab 0.000E+00 q_ab/q_b 0.0000 Pi_ab 0.9500 P_7 1.2915 S_7 2.8865 P_9 0.0250 Pe/Pa 0.1000 n_nozzle 1.0000 M_9 3.1643 T_9 326.0555 S_9 2.8865 u_9 1112.0881 P_9_fan 0.2500 T_9_fan 250.0000 M_9_fan 0.8920 u_9_fan 282.7081 Specific_thrust 0.3195 Thermal_eff 0.8323 Ideal thermal eff 0.6233 Propulsive_eff 0.0438 Overall_eff 0.0364 TSFC 21.9480 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.0325 0.1300 1.0000 3.0018 347.4675 2.8865 1089.0565 0.2500 250.0000 0.8920 282.7081 0.7028 0.7963 0.6233 0.1007 0.0802 9.9783 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.0423 0.1690 1.0000 2.8408 370.2856 2.8865 1063.9639 0.2500 250.0000 0.8920 282.7081 1.0075 0.7579 0.6233 0.1516 0.1149 6.9606 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.0549 0.2197 1.0000 2.6810 394.6021 2.8865 1036.5550 0.2500 250.0000 0.8920 282.7081 1.2463 0.7170 0.6233 0.1983 0.1422 5.6269 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.0714 0.2856 1.0000 2.5218 420.5155 2.8865 1006.5251 0.2500 250.0000 0.8920 282.7081 1.4296 0.6735 0.6233 0.2421 0.1631 4.9054 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.0928 0.3713 1.0000 2.3627 448.1307 2.8865 973.5040 0.2500 250.0000 0.8920 282.7081 1.5658 0.6271 0.6233 0.2849 0.1786 4.4785 Thrust & fuel consumption 7 Specific thrust & TSFC 6 5 4 3 2 1 0 1.0 Pe/Pa 10.0 Specific_thrust TSFC T-s diagram 2000 Temperature (K) 1600 1200 800 400 0 Co lu m n Row 3 Co lu m n Co lu m n Co lu m n Co Co Co Co Co Co Co Co Co Co Co Co lu lu lu lu lu lu lu lu lu lu lu lu mmmmmmmmmmmm n n n nI nJ n n n n n n n Dimensionless entropy (S-S1)/R Row 16 Row 25 Row 32 Row 39 Co lu m n Co lu m n Co lu m n Co lu m n Row 9 Row 49 Effect of exit pressure not equal ambient pressure 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.1207 0.4827 1.0000 2.2030 477.5593 2.8865 937.0345 0.2500 250.0000 0.8920 282.7081 1.6620 0.5776 0.6233 0.3282 0.1896 4.2195 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.1569 0.6275 1.0000 2.0419 508.9205 2.8865 896.5387 0.2500 250.0000 0.8920 282.7081 1.7237 0.5249 0.6233 0.3746 0.1966 4.0685 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.2039 0.8157 1.0000 1.8781 542.3412 2.8865 851.2659 0.2500 250.0000 0.8920 282.7081 1.7556 0.4688 0.6233 0.4273 0.2003 3.9943 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.2651 1.0604 1.0000 1.7102 577.9566 2.8865 800.2057 0.2500 250.0000 0.8920 282.7081 1.7621 0.4089 0.6233 0.4916 0.2010 3.9796 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.3446 1.3786 1.0000 1.5360 615.9108 2.8865 741.9348 0.2500 250.0000 0.8920 282.7081 1.7474 0.3451 0.6233 0.5776 0.1993 4.0131 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.4480 1.7922 1.0000 1.3523 656.3575 2.8865 674.3175 0.2500 250.0000 0.8920 282.7081 1.7172 0.2771 0.6233 0.7069 0.1959 4.0837 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.5825 2.3298 1.0000 1.1536 699.4603 2.8865 593.8452 0.2500 250.0000 0.8920 282.7081 1.6825 0.2047 0.6233 0.9377 0.1919 4.1680 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.7572 3.0288 1.0000 0.9294 745.3937 2.8865 493.8608 0.2500 250.0000 0.8920 282.7081 1.6737 0.1275 0.6233 1.4976 0.1909 4.1898 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 0.9843 3.9374 1.0000 0.6522 794.3435 2.8865 357.7751 0.2500 250.0000 0.8920 282.7081 1.8287 0.0452 0.6233 4.6125 0.2086 3.8347 0.8000 0.0290 250.0000 0.2500 286.9865 316.9310 253.5448 0.0000 282.0000 1.0000 0.3811 0.0000 20.0000 0.9000 2.4241 683.5929 7.6217 0.2199 1.1000 0.4192 1.0000 1.0276 289.7848 5.0000 1250.0000 7.044E+05 1.0000 7.6217 2.8352 1.0000 0.0000 848.4071 0.6787 0.1784 1.3595 2.8352 0.0000 7.0000 848.4071 0.000E+00 0.0000 0.9500 1.2915 2.8865 1.2796 5.1186 1.0000 0.1184 846.5078 2.8865 67.0578 0.2500 250.0000 0.8920 282.7081 8.6092 -0.0424 0.6233 -23.1418 0.9821 0.8146
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USC - AME - 436
Diesel FuturesForget the black soot and smoke. Modern diesel-powered cars are quiet, clean and fast.BY PAUL WEISSLER Photo by Thorsten WeiglYou would expect the 6-cylinder engine in the Mercedes E-Class and the V8 in the BMW 7 Series to be so smo
USC - CHEM - 004
Distinguished Lecture SeriesDynamical Order and Complexity in Rhythmic Chemical SystemsProfessor John L. HudsonChemical Engineering University of Virginia Charlottesville, VirginiaAbstract The interaction and synchronization of populations of rhy
USC - ISE - 006
SAE 599 Economic Considerations for Systems Architecting and EngineeringStan Settles, Marilee Wheaton 2008 FallCourse objectives: This course is intended to give the systems architect (SA) or systems engineer (SE) insight into the impact of econom
USC - ISE - 005
RISK & RELIABILITY ENGINEERING ISE 599: (3 units) Fridays 5:00-7:00 pm Instructor: Dr. Leila Meshkat Spring 2008 Building and maintaining reliable and robust systems is a key focus of engineering design. The reliability and risk attributes of a syste
USC - ISE - 005
What will you contribute to systems architecting?If this is a question you contemplate, we are opening a new conversation that may lead to something interesting.SAE 599 Advanced Systems Architecting Research and Practice University of Southern Cal
USC - ISE - 004
Health Care Operations ImprovementISE/PPD 508: (3 units) 048-31508R (on campus section, RTH 109), 034-31708D (off campus section, DEN) Fall 07, T 6:30 PMThe largest piece of the US economy and a field with many job opportunities, health care, need
USC - ISE - 004
Industrial Ecology (ISE 576)FALL 2007 TECHNICAL ELECTIVE(31576D on campus, 31776D DEN, Mondays 6:30-9:10, no prerequisite)Future demand for fuels and energy must be met taking into account increasingly severe environmental constraints, including
USC - ISE - 004
Research and Development PlanningISE 599: (3 units) MW 2-3:20 PM Instructor: Dr. Jeffrey H. Smith 31598D (on campus section, OHE 100C), 31798D (off campus section, DEN) Fall 07 As the rate of technology evolution continues to accelerate across an ex
USC - ISE - 005
Modeling and Simulation for Systems Architecting and Engineering ISE 599: (3 units) Wednesdays 6:30pm 9:10pm Instructor: Dr. Raymond Madachy Fall 2007 The architecting and engineering of complex systems requires the use of computerassisted modeling
USC - ISE - 004
University of Southern California - Industrial & Systems Engineering ISE 508: Health Care Operations Improvement Syllabus David L. Belson, Ph.D. Description Hospital productivity is critical to cost-effective health care. The course covers topics in
USC - ISE - 005
Syllabus(Draft 8/07)Health Care Operations Improvement ISE 508Instructor: David Belson, Ph.D belson@usc.eduCourse Text: "Quantitative Methods in Healthcare Management" , Yasar A. Ozcan, Ph.D., 2005, Jossey-Bass/Wiley Publisher.Additional readin
USC - ISE - 006
University of Southern California - Industrial & Systems Engineering Syllabus (Draft 9/5/08) ISE 508 Health Care Operations ImprovementInstructor:David Belson, Ph.Dbelson@usc.eduCourse Text: Healthcare Operations Management by McLaughlin & Ha
USC - ISE - 005
ISE 511 - Computer-Aided ManufacturingSpring 2008 COURSE SYLLABUS INSTRUCTOR LAB ASSISTANT Behrokh Khoshnevis, khoshnev@rcf.usc.edu Office Hours: Thursdays 2-5 PM, GER 202C Farshad Tajalli, Tajalli@usc.edu Office Hours: Th 2-6OBJECTIVES To enh
USC - ISE - 001
ISE 513 INVENTORY SYSTEMS Spring 2005 TEXT: Inventory Management and Production Planning and Scheduling by E. A. Silver, R. Peterson, and Pyke, Third Edition, John Wiley & Sons, 1998. INSTRUCTOR:Maged M. Dessouky GER 206 Phone: (213) 740-4891 Office
USC - ISE - 006
ISE 513 INVENTORY SYSTEMS Spring 2008 TEXT: Inventory Management and Production Planning and Scheduling by E. A. Silver, R. Peterson, and Pyke,Third Edition, John Wiley & Sons, 1998.INSTRUCTOR:Maged M. Dessouky GER 206 Phone: (213) 740-4891 Offi
USC - ISE - 006
ISE 513 INVENTORY SYSTEMS Spring 2008 TEXT: Inventory Management and Production Planning and Scheduling by E. A. Silver, R. Peterson, and Pyke,Third Edition, John Wiley & Sons, 1998.INSTRUCTOR:Maged M. Dessouky GER 206 Phone: (213) 740-4891 Offi
USC - ISE - 003
ISE514 Fall 2006Advanced Production Planning and Scheduling (ISE514) Fall 2006 (rev. 08/06/06) Instructor: TA: TA Office hours: Instructor Office hours: Class time/place: Test schedule: Midterm Thursday, September 29, 2006 Midterm Thursday, Novembe
USC - ISE - 005
ISE514 Fall 2007Advanced Production Planning and Scheduling (ISE514) Fall 2007 (rev. 08/11/07) Instructor: Office Hours: TA: Office Hours: Class time/place: Test schedule: Midterm: Midterm: Final: Web Page: Thursday, September 27, 2007 Thursday, No
USC - ISE - 006
Advanced Production Planning and Scheduling (ISE514) Fall 2008 (rev. 08/25/08) Instructor: Geza Bottlik, E-mail: bottlik514@gezabottlik.com Office Hours: Tuesdays and Thursdays, 2:00 P.M. 3:00 P.M, Room GER 202 Phone 213 740 - 5050 Qian An qan@usc.e
USC - ISE - 005
University Of Southern CaliforniaIndustrial and System Engineering ISE 515 Engineering Project Management Al Morelli E-mail: Morelli4@gmail.comFall Semester, 2007 Wednesdays, 6:30pm - 9:10pm 6:30 - 7:45pm - lecture 7:45 - 8:00pm - break 8:00 - 9:1
USC - ISE - 006
ISE515 Fall 2008Project Management (ISE515) Fall 2008 (08/25/08) Instructor: Office Hours: Class time/place: TA: TA Office hours: Geza Bottlik, E-mail: bottlik515@gezabottlik.com Tuesday/Thursday, 2:00 P.M. 3:00 P.M. GER 202 Phone 213 740 5050 Th
USC - ISE - 006
ISE 515: Project Management (Knopp-McKendree) Spring 2008 SYLLABUS Class Sessions: Day: Time: Room: Class Number: Tuesday (evening) 6:30 pm 9:10 pm OHE 100C (Webcasted Course) 31505D (on campus) and 31705D (DEN)1 (of 7)Contact Information: Instr
USC - ISE - 006
Industrial and Systems EngineeringSyllabus ISE 515: Engineering Project ManagementFall 2008, Monday 6:30pm 9:10pm Instructor Office Office Hours TA Office Office Hours Prof. Erich Kreidler GER 205 Monday 4:30pm 5:30pm or by appointment TBD TBD
USC - ISE - 005
ISE 517 Modern Enterprise Systems: Managing the Enterprise as a system SyllabusFall Semester, 2007 Mike G. Kazeef, Adjunct Associate ProfessorPurpose and focus of ISE 517 20073. The pursuit of improvement, as one of the major dimensions of IE, requ
USC - ISE - 006
Course Description and SyllabusModern Enterprise Systems ISE 517; Fall 2008Wednesdays: 3:30pm to 6:20pm in OHE 120Overview This course is designed to enhance student understanding of modern enterprises and, secondarily, to strengthen skills neces
USC - ISE - 006
ISE 517 Modern Enterprise Systems: Managing the Enterprise As a system With the state of its processes SyllabusSpring Semester, 2009. Mike G. Kazeef, Adjunct Associate ProfessorPurpose and focus of ISE 517 20091. The pursuit of improvement, as one
USC - ISE - 003
University of Southern California Daniel J. Epstein Department of Industrial and Systems Engineering ISE 520: Optimization: Theory and Algorithms Fall 2006 Course Syllabus Instructor: Fernando Ordnez o GER - 203 (213) 821-2413 fordon@usc.edu Oce Hou
USC - ISE - 005
Optimization: Theory and Algorithms ISE 520SyllabusInstructor: Richard Waltz <rwaltz@usc.edu> Class: Tuesday and Thursday 11:00-12:20 (room to be announced) Office Hours: Tuesday and Thursday 1:30-3:00 (room to be announced) Required Text: Numeric
USC - ISE - 003
ISE 525 Design of Experiments Spring Semester 2007 M,W 2:00 - 3:30 pm Room: OHE 120 Web site: www.uscden.netKurt Palmer Office: GER 206B Hours: Tu 1:00 - 3:00 pm Phone: 740-5960 E-mail: kpalmer@usc.eduRecommended Preparation: ISE 225 Engineering
USC - ISE - 003
ISE 527 Quality Management for Engineers Spring Semester 2007 Tu,Th 3:30 - 4:50 pm Room: OHE 120Ali Nowroozi Office: Hours: Tu,Th 5:00 - 6:00 pm Phone: E-mail: anowrooz@sbcglobal.netObjective: In this course, you will learn how to develop, deploy
USC - ISE - 005
ISE 527 - Quality Management for Engineers (3 Units) Fall Semester 2007 Mon 6:30 - 9:10 pm Room: OHE 120 Instructor: Ali Nowroozi Office: GER235 Hours: Mon. 4:00 6:00 pm Phone: (213) 740-5960 E-mail: nowroozi@usc.edu Teaching Assistant: Haifeng Ji O
USC - ISE - 006
ISE 527 Quality Management for Engineers Fall Semester 2008 Tu,Th 3:30 - 4:50 pm Room: OHE 100C (Studio C) Web Site: www.uscden.netKurt Palmer Office: GER 206B Hours: M,W 10:30 am - 12:00 pm Phone: 740-5960 E-mail: kpalmer@usc.eduObjective: In th
USC - ISE - 001
University of Southern California School of Engineering Daniel J. Epstein Department of Industrial and Systems EngineeringISE 530: Introduction to Operations Research Spring, 2002-03 (3 units) Tuesday Evenings, 6:30-9:10 PM OHE 100 Professor James M
USC - ISE - 002
University of Southern California Department of Industrial and Systems Engineering Course Syllabus ISE 532: Network Flows Spring 2006Meeting Time and Location: Meeting Hour: Thursday 6:30 9: 10 pm Classroom: OHE 100B Instruction Staff: Instructor
USC - ISE - 006
University of Southern California Daniel J. Epstein Department of Industrial and Systems Engineering ISE 532: Network Flows Spring 2008 Course Syllabus Instructor: Fernando Ordnez o GER - 203 (213) 821-2413 fordon@usc.edu http:/www-rcf.usc.edu/fordo
USC - ISE - 003
University of Southern California Daniel J. Epstein Department of Industrial and Systems Engineering ISE 536: Linear Programming and Extensions Fall 2006 Course Syllabus Instructor: Fernando Ordnez o GER - 203 (213) 821-2413 fordon@usc.edu Oce Hours
USC - ISE - 005
University of Southern California Daniel J. Epstein Department of Industrial and Systems Engineering ISE 536: Linear Programming and Extensions Fall 2007 Course Syllabus Instructor: Fernando Ordnez o GER - 203 (213) 821-2413 fordon@usc.edu Oce Hours
USC - ISE - 006
ISE 536 Fall 2008University of Southern California School of Engineering Daniel J. Epstein Department of Industrial and Systems EngineeringISE 536: Linear Programming and Extensions, Dr. Erim Kardes Fall, 2008 Location: OHE100D Time: M-W, 11-12:20
USC - ISE - 003
Elements of Stochastic Processes ISE 538, Spring 2007Contact Information: Instructor: Sheldon Ross Oce: GER 235A Number: (213) 821-1377 Oce Hours: tbd Email: smross@usc.edu TA:tbd Email: tbdTextbook: Introduction to Probability Models, ninth ed.,
USC - ISE - 003
UNIVERSITY OF SOUTHERN CALIFORNIASystems Engineering Theory & Practice ISE 541Jim Hines Spring 2007UNIVERSTY OF SOUTHERN CALIFORNIA COURSE OBJECTIVES AND REQUIREMENTS SYSTEMS ENGINEERING THEORY AND PRACTICE (ISE 541) Instructor: Jim Hines Phone
USC - ISE - 003
ISE 541 Systems Engineering Theory and Practice Spring / 2007 Scott Jackson Office Number: None Phone Number: 949-726-2003 Fax Number: 949-854-0519 Email Address: jackessone@cox.net Office Hours: 5:15 pm to 6:15 pm on Wednesdays in the DEN building f
USC - ISE - 006
UNIVERSITY OF SOUTHERN CALIFORNIASystems Engineering Theory & Practice SAE 541Jim Hines Fall 2008UNIVERSTY OF SOUTHERN CALIFORNIA COURSE OBJECTIVES AND REQUIREMENTS SYSTEMS ENGINEERING THEORY AND PRACTICE (ISE 541) Instructor: Jim Hines Phone:
USC - ISE - 006
UNIVERSITY OF SOUTHERN CALIFORNIASystems Engineering Theory & Practice SAE 541Jim Hines Spring 2009UNIVERSTY OF SOUTHERN CALIFORNIA COURSE OBJECTIVES AND REQUIREMENTS SYSTEMS ENGINEERING THEORY AND PRACTICE (SAE 541) Instructor: Jim Hines Phone
USC - ISE - 003
ISE 542 ADVANCED TOPICS IN SYSTEMS ENGINEERING (3) Fall semester, 2006 Syllabususc.syllabus. rev8/05Decision-based design, quantitative risk management, testing logic, graph theory applied to mathematical model management, mission systems engineer
USC - ISE - 005
ISE 542 ADVANCED TOPICS IN SYSTEMS ENGINEERING (3 units) Fall semester, 2007; Mondays, 6:30 9:10PM Syllabususc.syllabus. rev 8/07Decision-based design, quantitative risk management, testing logic, graph theory applied to mathematical model manage
USC - ISE - 005
ISE544 Fall 2007 Management of Engineering Teams Fall 2007 (rev. 07/10/07) Instructor: Office Hours: TA: Office Hours: Class time/place: Test Schedule: Geza Bottlik, E-mail: bottlik544@gezabottlik.com (email sent through DEN will go to 514) Wednesday
USC - ISE - 005
University Of Southern CaliforniaIndustrial and System Engineering ISE 544 Al Morelli E-mail: Morelli4@gmail.comManagement of Engineering TeamsFall Semester, 2007 Mondays, 6:30pm - 9:10pm 6:30 - 7:45pm - lecture 7:45 - 8:00pm - break 8:00 - 9:10p
USC - ISE - 006
University of Southern CaliforniaDaniel J. Epstein Department of Industrial and Systems EngineeringSyllabus ISE 544: Management of Engineering TeamsFall 2008 August 28 to December 11 Sections 31504D & 31704D Thursdays, 6:30 to 9:10 PM, RTH 105
USC - ISE - 006
University Of Southern CaliforniaIndustrial and System Engineering ISE 544 Professor Al Morelli E-mail: USCise544@gmail.com Office: GER 240 Office Hrs: T 5:30-6:30 pm (213 ) 740-4893 TA : Hamid Chabok Email: ISE544TA@gmail.comManagement of Enginee
USC - ISE - 002
SYLLABUSISE545: Technology Development and ImplementationThe 1st Summer Term (six-week session), 2006 Stephen Lu, Ph.D. David Packard Chair in Manufacturing Engineering; Professor of Aerospace and Mechanical Engineering, Computer Science, and Indu
USC - ISE - 003
SYLLABUS:ISE 550TITLE: ENGINEERING MANAGEMENT OF GOVERNMENT-FUNDED PROGRAMS. LECTURER: Mr. Kenneth Cureton TIME: Wednesdays, 6:30-9:10 p.m. ROOM: OHE 100D- DEN Studio "F" (Webcasted Course) OFFICE: GER 205, Wednesdays, 5:30-6:30 p.m. (213) 740-53
USC - ISE - 003
INVENTION & TECHNOLOGY DEVELOPMENT ISE 555Instructor: B. Khoshnevis Industrial & Systems Engineering University of Southern CaliforniaAbout the Course Great engineering systems, processes and products are usually based largely on the exercise of
USC - ISE - 005
INVENTION & TECHNOLOGY DEVELOPMENT ISE 555Instructor: B. KhoshnevisAbout the Course Great engineering systems, processes and products are usually based largely on the exercise of inventive thinking and not on routine procedures for engineering an
USC - ISE - 006
INVENTION & TECHNOLOGY DEVELOPMENT ISE 555Instructor: B. KhoshnevisAbout the Course Great engineering systems, processes and products are usually based largely on the exercise of inventive thinking and not on routine procedures for engineering an
USC - ISE - 003
-1ECONOMIC ANALYSIS OF ENGINEERING PROJECTS (ISE 561)Fridays, 5:30 8:10 pm, Room OHB 100B Professor: Office: Phone: Fax: e-mail: Virgil Adumitroaie GER 205 (Fridays, 4:25-5:25 pm) (213) 740-5383 (213) 740-1120 adumitro@usc.edu Teaching Assistant: O
USC - ISE - 005
-1ECONOMIC ANALYSIS OF ENGINEERING PROJECTS (ISE 561)Monday, 6:30 9:10 pm, Room RTH109 Professor: Office: Phone: Fax: e-mail: Virgil Adumitroaie GER 205 (Monday, 5:25-6:25 pm) (213) 740-5383 (213) 740-1120 adumitro@usc.edu Teaching Assistant: Offic
USC - ISE - 003
Value and Decision Analysis, ISE 562 Spring 2007 Dr. SmithContents Contact Info My Office Hours Importance of this course Course Description Suggestions for success Course Prerequisite Course Goals Text Course Requirements and Grading Schedule Acad
USC - ISE - 006
Value and Decision Theory (ISE 562) Richard S. John, Ph.D. Fall Semester, 2008 Class meets: Instructor: Office: Phone: Office Hrs. e-mail TA: e-mail: OHE 136; Tues and Thur, 5:00 PM - 6:20 PM Richard John, Ph.D. SGM 621 213-740-4011 or 310-227-6186 T
USC - ISE - 003
Syllabus ISE 563: FINANCIAL ENGINEERINGContact Information: Instructor: Sheldon Ross Oce: GER 235A Oce Hours: TBD Phone: (213) 821-1377 Email: smross@usc.edu TA: TBD TA Oce: GER 309 TA Oce Hours: TBD TA Phone: (213) 740-4893 TA Email: TBDTextbook
USC - ISE - 001
ISE 564: Fall 20031ISE 564: PERFORMANCE ANALYSISInstructor: Dr. M. Rahimi TA: Greg Placencia Office: GER 202-B Tel: (213)740-4883 Tel: 213-740-4016 E-mail: placenci@usc.edu Fax: 213-740-1120 Office hours: 12:00 2:00 pm E-mail: mrahimi@rcf.usc.e
USC - ISE - 005
ISE 599 (566) FINANCIAL ACCOUNTING ANALYSIS FOR ENGINEERING COURSE SYLLABUS SPRING 2007Instructor: Dana Sherman, Esq. (BA, JD, MBA, MBT, MPA) PO Box 570775 Tarzana, CA 91357-0775 818-881-3738 (tel) 818-881-5580 (fax) 818-640-7567 (cell) danasher@usc