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This software and related documentation are proprietary to Electronic Data Systems Corporation. 2003 Electronic Data Systems Corporation. All Rights Reserved LIMITATIONS TO U.S. GOVERNM...
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UNIVERSITY OF TORONTO FACULTY OF APPLIED SCIENCE AND ENGINEERING EXAMINATION 1, OCTOBER 2002 MIE566F - DECISION ANALYSIS Examiner - Chi-Guhn Lee
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...MIE566
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Decision Analysis
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Special 10-77 Topic: Binary Vapor Cycles 10-82C Binary power cycle is a cycle which is actually a combination of two cycles; one in the high temperature region, and the other in the low temperature region. Its purpose is to increase thermal efficiency. 10-83C Consider the heat exchanger of a binary power cycle. The working fluid of the topping cycle (cycle A) enters the heat exchanger at state 1 and leaves at state 2. The working fluid of the bottoming cycle (cycle B) enters at state 3 and leaves at state 4. Neglecting any changes in kinetic and potential energies, and assuming the heat exchanger is well-insulated, the steady-flow energy balance relation yields & & & E in - E out = E system & & m h = m h e e 0 (steady) =0 & & E in = E out & & & & & & m A h2 + m B h4 = m A h1 + m B h3 or m A (h2 - h1 ) = m B (h3 - h4 ) i i Thus, & m A h3 - h4 = & mB h2 - h1 10-84C Steam is not an ideal fluid for vapor power cycles because its critical temperature is low, its saturation dome resembles an inverted V, and its condenser pressure is too low. 10-85C Because mercury has a high critical temperature, relatively low critical pressure, but a very low condenser pressure. It is also toxic, expensive, and has a low enthalpy of vaporization. 10-86C In binary vapor power cycles, both cycles are vapor cycles. In the combined gas-steam power cycle, one of the cycles is a gas cycle. 10-78 Review Problems 10-87 It is to be demonstrated that the thermal efficiency of a combined gas-steam power plant cc can be expressed as cc = g + s - gs where g = Wg / Qin and s = Ws / Qg,out are the thermal efficiencies of the gas and steam cycles, respectively, and the efficiency of a combined cycle is to be obtained. Analysis The thermal efficiencies of gas, steam, and combined cycles can be expressed as Wtotal Q = 1 - out Qin Qin Wg Qin = 1- Qg,out Qin cc = g = s = Ws Q = 1 - out Qg,out Qg,out where Qin is the heat supplied to the gas cycle, where Qout is the heat rejected by the steam cycle, and where Qg,out is the heat rejected from the gas cycle and supplied to the steam cycle. Using the relations above, the expression g + s - g s can be expressed as g,out + 1 - out g + s - g s = 1 - Qin Qg,out Q Q = 1- = 1- = cc Qg,out Qin Qout Qin +1- Qout Qg,out Qg,out Q - 1 - 1 - out Q Qin g,out Qg,out Q Q -1+ + out - out Qin Qg,out Qin Therefore, the proof is complete. Using the relation above, the thermal efficiency of the given combined cycle is determined to be cc = g + s - g s = 0.4 + 0.30 - 0.40 0.30 = 0.58 10-88 The thermal efficiency of a combined gas-steam power plant cc can be expressed in terms of the thermal efficiencies of the gas and the steam turbine cycles as cc = g + s - gs . It is to be shown that the value of cc is greater than either of g or s . Analysis By factoring out terms, the relation cc = g + s - gs can be expressed as cc = g + s - g s = g + s (1 - g ) > g 1 24 4 3 Positive since g <1 or cc = g + s - g s = s + g (1 - s ) > s 1 24 4 3 Positive since s <1 Thus we conclude that the combined cycle is more efficient than either of the gas turbine or steam turbine cycles alone. 10-79 10-89 A steam power plant operating on the ideal Rankine cycle with reheating is considered. The reheat pressures of the cycle are to be determined for the cases of single and double reheat. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis (a) Single Reheat: From the steam tables (Tables A-4, A-5, and A-6), P6 = 10 kPa h6 = h f + x6 h fg = 191.81 + (0.92 )(2392.1) = 2392.5 kJ/kg x6 = 0.92 s6 = s f + x6 s fg = 0.6492 + (0.92 )(7.4996) = 7.5488 kJ/kg K T5 = 600 C P5 = 2780 kPa s5 = s6 T 600 C SINGLE 25 MPa 2 10 kPa 1 6 s 1 3 5 T 600 C DOUBL 25 MPa 2 10 kPa 8 s 3 5 7 (b) Double Reheat : P3 = 25 MPa s = 6.3637 kJ/kg K T3 = 600 C 3 P4 = Px P = Px and 5 T5 = 600 C s 4 = s3 4 4 6 Any pressure Px selected between the limits of 25 MPa and 2.78 MPa will satisfy the requirements, and can be used for the double reheat pressure. 10-80 10-90E A geothermal power plant operating on the simple Rankine cycle using an organic fluid as the working fluid is considered. The exit temperature of the geothermal water from the vaporizer, the rate of heat rejection from the working fluid in the condenser, the mass flow rate of geothermal water at the preheater, and the thermal efficiency of the Level I cycle of this plant are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis (a) The exit temperature of geothermal water from the vaporizer is determined from the steadyflow energy balance on the geothermal water (brine), - 22,790,000 Btu/h = (384,286 lbm/h )(1.03 Btu/lbm F)(T2 - 325 F) T2 = 267.4 F & & Q brine = m brine c p (T2 - T1 ) (b) The rate of heat rejection from the working fluid to the air in the condenser is determined from the steady-flow energy balance on air, & & Qair = m air c p (T9 - T8 ) = (4,195,100 lbm/h )(0.24 Btu/lbm F)(84.5 - 55 F) = 29.7 MBtu/h (c) The mass flow rate of geothermal water at the preheater is determined from the steady-flow energy balance on the geothermal water, & - 11,140,000 Btu/h = m geo (1.03 Btu/lbm F)(154.0 - 211.8 F) & m geo = 187,120 lbm/h & & Qgeo = m geo c p (Tout - Tin ) (d) The rate of heat input is & & & Qin = Qvaporizer + Qreheater = 22,790,000 + 11140,000 , and = 33,930,000 Btu / h & Wnet = 1271 - 200 = 1071 kW Then, th = & 3412.14 Btu W net 1071 kW = 10.8% = & 33,930,000 Btu/h 1 kWh Qin 10-81 10-91 A steam power plant operates on the simple ideal Rankine cycle. The turbine inlet temperature, the net power output, the thermal efficiency, and the minimum mass flow rate of the cooling water required are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis (a) From the steam tables (Tables A-4, A-5, and A-6), h1 = h f @ 7.5 kPa = 168.75 kJ/kg v 1 = v f @ 7.5 kPa = 0.001008 m 3 /kg T1 = Tsat @ 7.5 kPa = 40.29 C wp,in = v 1 (P2 - P1 ) 1 kJ = 0.001008 m 3 /kg (6000 - 7.5 kPa ) 1 kPa m 3 = 6.04 kJ/kg T 3 ( ) 6 MPa 2 1 qin 7.5 kPa qout 4 s h2 = h1 + wp,in = 168.75 + 6.04 = 174.79 kJ/kg h4 = h g @ 7.5 kPa = 2574.0 kJ/kg s 4 = s g @ 7.5 kPa = 8.2501 kJ/kg P3 = 6 MPa s3 = s4 h3 = 4852.2 kJ/kg T = 1089.2 C 3 (b) qin = h3 - h2 = 4852.2 - 174.79 = 4677.4 kJ/kg qout = h4 - h1 = 2574.0 - 168.75 = 2405.3 kJ/kg wnet = qin - qout = 4677.4 - 2405.3 = 2272.1 kJ/kg and th = Thus, wnet 2272.1 kJ/kg = = 48.6% q in 4677.4 kJ/kg & & W net = th Qin = (0.4857 )(40,000 kJ/s ) = 19,428 kJ/s (c) The mass flow rate of the cooling water will be minimum when it is heated to the temperature of the steam in the condenser, which is 40.29 C, & & & Qout = Qin - Wnet = 40,000- 19,428 = 20,572 kJ/s & mcool = & 20,572 kJ/s Qout = = 194.6 kg/s (4.18 kJ/kg C)(40.29 - 15 C) cT 10-82 10-92 A steam power plant operating on an ideal Rankine cycle with two stages of reheat is considered. The thermal efficiency of the cycle and the mass flow rate of the steam are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis (a) From the steam tables (Tables A-4, A-5, and A-6), h1 = h f @ 5 kPa = 137.75 kJ/kg v1 = v f @ 5 kPa = 0.001005 m3/kg wp,in = v1 (P2 - P ) 1 1 kJ = 0.001005 m3/kg (15,000 - 5 kPa ) 1 kPa m3 = 15.07 kJ/kg 15 MPa 2 5 kPa T 5 MPa 1 MPa 3 4 5 6 7 ( ) h2 = h1 + wp,in = 137.75 + 15.07 = 152.82 kJ/kg P3 = 15 MPa h3 = 3310.8 kJ/kg T3 = 500 C s3 = 6.3480 kJ/kg K P4 = 5 MPa h4 = 3007.4 kJ/kg s4 = s3 P5 = 5 MPa h5 = 3434.7 kJ/kg T5 = 500 C s5 = 6.9781 kJ/kg K P6 = 1 MPa h6 = 2971.3 kJ/kg s6 = s5 1 8 s P7 = 1 MPa h7 = 3479.1 kJ/kg T7 = 500 C s7 = 7.7642 kJ/kg K s8 - s f 7.7642 - 0.4762 = = 0.9204 P8 = 5 kPa x8 = s fg 7.9176 s8 = s7 h8 = h f + x8h fg = 137.75 + (0.9204 )(2423.0 ) = 2367.9 kJ/kg Then, qin = (h3 - h2 ) + (h5 - h4 ) + (h7 - h6 ) = 3310.8 - 152.82 + 3434.7 - 3007.4 + 3479.1 - 2971.3 = 4093.1 kJ/kg qout = h8 - h1 = 2367.9 - 137.75 = 2230.2 kJ/kg wnet = qin - qout = 4093.1 - 2230.2 = 1862.9 kJ/kg Thus, th = (b) & m= wnet 1862.9 kJ/kg = = 45.5% 4093.1 kJ/kg q in & Wnet 120,000 kJ/s = = 64.4 kg/s wnet 1862.9 kJ/kg 10-83 10-93 An 150-MW steam power plant operating on a regenerative Rankine cycle with an open feedwater heater is considered. The mass flow rate of steam through the boiler, the thermal efficiency of the cycle, and the irreversibility associated with the regeneration process are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis 5 Boiler 6 y 4 Open fwh P II 3 Turbine 1-y 7 Condenser 2 4 T qin 10 MPa y 6 6s 7s 1-y 7 s 5 3 0.5 MPa 10 kPa 1 qout 2 PI 1 (a) From the steam tables (Tables A-4, A-5, and A-6), h1 = hf @ 10 kPa = 191.81 kJ/kg v1 = v f @ 10 kPa = 0.00101 m3/kg wpI,in = v1(P - P ) / p 2 1 1 kJ = 0.00101m3/kg (500-10 kPa) 1 kPa m3 /(0.95) = 0.52 kJ/kg ( ) h2 = h1 + wpI,in = 191.81+ 0.52 = 192.33 kJ/kg P = 0.5 MPa h3 = hf @ 0.5 MPa = 640.09 kJ/kg 3 v = v 3 sat.liquid f @ 0.5 MPa = 0.001093 m /kg 3 wpII,in = v 3 (P4 - P3 ) / p 1 kJ = 0.001093 m3/kg (10,000 - 500 kPa ) 1 kPa m3 / (0.95) = 10.93 kJ/kg ( ) h4 = h3 + wpII,in = 640.09 + 10.93 = 651.02 kJ/kg P5 = 10 MPa h5 = 3375.1 kJ/kg T5 = 500 C s 5 = 6.5995 kJ/kg K 6.5995 - 1.8604 = = 0.9554 4.9603 s fg P6 s = 0.5 MPa h6 s = h f + x 6 s h fg = 640.09 + (0.9554)(2108.0) s 6s = s5 = 2654.1 kJ/kg x6s = s6s - s f T = h5 - h6 h6 = h5 - T (h5 - h6 s ) h5 - h6 s = 3375.1 - (0.80)(3375.1 - 2654.1) = 2798.3 kJ/kg 10-84 6.5995 - 0.6492 = = 0.7934 7.4996 s fg P7 s = 10 kPa h7 s = h f + x 7 s h fg = 191.81 + (0.7934 )(2392.1) s7s = s5 = 2089.7 kJ/kg x7s = s7s - s f T = h5 - h7 h7 = h5 - T (h5 - h7 s ) h5 - h7 s = 3375.1 - (0.80)(3375.1 - 2089.7 ) = 2346.8 kJ/kg The fraction of steam extracted is determined from the steady-flow energy balance equation applied to the & & feedwater heaters. Noting that Q W ke pe 0 , & & & E in - E out = E system & & m h = m h i i 0 (steady) =0 & & Ein = E out e e & & & m6 h6 + m2 h2 = m3 h3 yh6 + (1 - y )h2 = 1(h3 ) & & where y is the fraction of steam extracted from the turbine ( = m6 / m3 ). Solving for y, y= h3 - h2 640.09 - 192.33 = = 0.1718 h6 - h2 2798.3 - 192.33 Then, qout = (1 - y )(h7 - h1 ) = (1 - 0.1718)(2346.8 - 191.81) = 1784.7 kJ/kg wnet = qin - qout = 2724.1 - 1784.7 = 939.4 kJ/kg qin = h5 - h4 = 3375.1 - 651.02 = 2724.1 kJ/kg and & m= & Wnet 150,000 kJ/s = = 159.7 kg/s wnet 939.4 kJ/kg q out 1784.7 kJ/kg = 1- = 34.5% q in 2724.1 kJ/kg (b) The thermal efficiency is determined from th = 1 - Also, P6 = 0.5 MPa s6 = 6.9453 kJ/kg K h6 = 2798.3 kJ/kg s3 = s f @ 0.5 MPa = 1.8604 kJ/kg K s2 = s1 = s f @ 10 kPa = 0.6492 kJ/kg K Then the irreversibility (or exergy destruction) associated with this regeneration process is 0 q iregen = T0 sgen = T0 me se - mi si + surr = T0 [s3 - ys6 - (1 - y )s2 ] TL = (303 K )[1.8604 - (0.1718)(6.9453) - (1 - 0.1718)(0.6492 )] = 39.25 kJ/kg 10-85 10-94 An 150-MW steam power plant operating on an ideal regenerative Rankine cycle with an open feedwater heater is considered. The mass flow rate of steam through the boiler, the thermal efficiency of the cycle, and the irreversibility associated with the regeneration process are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes negligible. are Analysis 5 Boiler 6 y 4 Open fwh P II 3 Turbine 1-y 7 Condenser 2 T qin 4 10 MPa y 6 1-y qout 7 s 5 3 0.5 MPa 10 kPa 2 PI 1 1 (a) From the steam tables (Tables A-4, A-5, and A-6), h1 = h f @ 10 kPa @ 10 kPa = 191.81 kJ/kg = 0.00101 m 3 /kg v1 = v f wpI,in = v 1 (P2 - P1 ) 1 kJ = 0.00101 m 3 /kg (500 - 10 kPa ) 1 kPa m 3 h2 = h1 + wpI,in = 191.81 + 0.50 = 192.30 kJ/kg ( ) = 0.50 kJ/kg P3 = 0.5 MPa sat.liquid h3 = h f @ 0.5 MPa = 640.09 kJ/kg v = v 3 f @ 0.5 MPa = 0.001093 m /kg 3 wpII,in = v 3 (P4 - P3 ) 1 kJ = 0.001093 m3/kg (10,000 - 500 kPa ) 1 kPa m3 = 10.38 kJ/kg h4 = h3 + wpII,in = 640.09 + 10.38 = 650.47 kJ/kg ( ) P5 = 10 MPa h5 = 3375.1 kJ/kg T5 = 500 C s5 = 6.5995 kJ/kg K s6 - s f 6.5995 - 1.8604 = = 0.9554 P6 = 0.5 MPa x6 = s fg 4.9603 s6 = s5 h6 = h f + x6 h fg = 640.09 + (0.9554)(2108.0 ) = 2654.1 kJ/kg s7 - s f 6.5995 - 0.6492 = = 0.7934 P7 = 10 kPa x7 = s fg 7.4996 s7 = s5 h7 = h f + x7 h fg = 191.81 + (0.7934)(2392.1) = 2089.7 kJ/kg 10-86 The fraction of steam extracted is determined from the steady-flow energy equation applied to the & & feedwater heaters. Noting that Q W ke pe 0 , & & & E in - E out = E system & & m h = m h i i e e 0 (steady) & & = 0 E in = E out & & & m6 h6 + m2 h2 = m3 h3 yh6 + (1 - y )h2 = 1(h3 ) & & where y is the fraction of steam extracted from the turbine ( = m6 / m3 ). Solving for y, y= h3 - h2 640.09 - 192.31 = = 0.1819 h6 - h2 2654.1 - 192.31 Then, qout = (1 - y )(h7 - h1 ) = (1 - 0.1819)(2089.7 - 191.81) = 1552.7 kJ/kg wnet = qin - qout = 2724.6 - 1552.7 = 1172.0 kJ/kg & Wnet 150,000 kJ/s = = 128.0 kg/s wnet 1171.9 kJ/kg qin = h5 - h4 = 3375.1 - 650.47 = 2724.6 kJ/kg and & m= (b) The thermal efficiency is determined from th = 1 - Also, q out 1552.7 kJ/kg = 1- = 43.0% q in 2724.7 kJ/kg s 6 = s 5 = 6.5995 kJ/kg K s3 = s f @ 0.5 MPa = 1.8604 kJ/kg K = 0.6492 kJ/kg K s 2 = s1 = s f @ 10 kPa Then the irreversibility (or exergy destruction) associated with this regeneration process is 0 q iregen = T0 sgen = T0 me se - mi si + surr = T0 [s3 - ys6 - (1 - y )s2 ] TL = (303 K )[1.8604 - (0.1819 )(6.5995) - (1 - 0.1819 )(0.6492)] = 39.0 kJ/kg 10-87 10-95 An ideal reheat-regenerative Rankine cycle with one open feedwater heater is considered. The fraction of steam extracted for regeneration and the thermal efficiency of the cycle are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis (a) From the steam tables (Tables A-4, A-5, and A-6), h1 = h f @ 15 kPa = 225.94 kJ/kg v1 = v f @ 15 kPa = 0.001014 m 3 /kg 5 wpI,in = v 1 (P2 - P1 ) 1 kJ = 0.001014 m 3 /kg (600 - 15 kPa ) 1 kPa m 3 = 0.59 kJ/kg ( ) Boiler 6 7 Turbine 1-y 9 Condens. 2 PI 1 8 y h2 = h1 + wpI,in = 225.94 + 0.59 = 226.53 kJ/kg P3 = 0.6 MPa sat. liquid h3 = h f @ 0.6 MPa = 670.38 kJ/kg v = v 3 f @ 0.6 MPa = 0.001101 m /kg 3 4 Open fwh P II 3 wpII,in = v 3 (P4 - P3 ) 1 kJ = 0.001101 m3/kg (10,000 - 600 kPa ) 1 kPa m3 = 10.35 kJ/kg T ( ) h4 = h3 + wpII,in = 670.38 + 10.35 = 680.73 kJ/kg P5 = 10 MPa h5 = 3375.1 kJ/kg T5 = 500 C s5 = 6.5995 kJ/kg K P6 = 1.0 MPa h6 = 2783.8 kJ/kg s6 = s5 P7 = 1.0 MPa h7 = 3479.1 kJ/kg T7 = 500 C s7 = 7.7642 kJ/kg K P8 = 0.6 MPa h8 = 3310.2 kJ/kg s8 = s7 1 MPa 7 5 10 MPa 4 3 2 15 kPa 1 9 s 0.6 MPa 6 8 s9 - s f 7.7642 - 0.7549 = = 0.9665 P9 = 15 kPa x9 = s fg 7.2522 s9 = s7 h9 = h f + x9 h fg = 225.94 + (0.9665)(2372.3) = 2518.8 kJ/kg The fraction of steam extracted is determined from the steady-flow energy balance equation applied to the & & feedwater heaters. Noting that Q W ke pe 0 , & & & E in - E out = E system & & m h = m h i i e e 0 (steady) & & = 0 Ein = E out & & & m8 h8 + m 2 h2 = m3 h3 yh8 + (1 - y )h2 = 1(h3 ) & & where y is the fraction of steam extracted from the turbine ( = m8 / m3 ). Solving for y, y= h3 - h2 670.38 - 226.53 = = 0.144 h8 - h2 3310.2 - 226.53 (b) The thermal efficiency is determined from q in = (h5 - h4 ) + (h7 - h6 ) = (3375.1 - 680.73) + (3479.1 - 2783.8) = 3389.7 kJ/kg q out = (1 - y )(h9 - h1 ) = (1 - 0.1440)(2518.8 - 225.94 ) = 1962.7 kJ/kg q out 1962.7 kJ/kg = 1- = 42.1% 3389.7 kJ/kg q in and th = 1 - 10-88 10-96 A nonideal reheat-regenerative Rankine cycle with one open feedwater heater is considered. The fraction of steam extracted for regeneration and the thermal efficiency of the cycle are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis 5 Boiler 6 7 Turbine 1-y 9 Condenser 2 T 5 4 3 7 8 y 6 6s 8s 8 y 1-y 4 Open fwh P II 3 2 PI 1 1 9s 9 s (a) From the steam tables (Tables A-4, A-5, and A-6), h1 = h f @ 15 kPa = 225.94 kJ/kg v 1 = v f @ 15 kPa = 0.001014 m 3 /kg w pI ,in = v 1 (P2 - P1 ) 1 kJ = 0.001014 m 3 /kg (600 - 15 kPa ) 1 kPa m 3 = 0.59 kJ/kg h3 = h f @ 0.6 MPa = 670.38 kJ/kg v = v 3 f @ 0.6 MPa = 0.001101 m /kg 3 ( ) h2 = h1 + w pI ,in = 225.94 + 0.59 = 226.54 kJ/kg P3 = 0.6 MPa sat. liquid wpII,in = v 3 (P4 - P3 ) 1 kJ = 0.001101 m3/kg (10,000 - 600 kPa ) 1 kPa m3 = 10.35 kJ/kg ( ) h4 = h3 + wpII,in = 670.38 + 10.35 = 680.73 kJ/kg P5 = 10 MPa h5 = 3375.1 kJ/kg T5 = 500 C s5 = 6.5995 kJ/kg K P6 s = 1.0 MPa h6 s = 2783.8 kJ/kg s6 s = s5 T = h5 - h6 h6 = h5 - T (h5 - h6 s ) h5 - h6 s = 3375.1 - (0.84 )(3375.1 - 2783.8) = 2878.4 kJ/kg 10-89 P7 = 1.0 MPa h7 = 3479.1 kJ/kg T7 = 500 C s7 = 7.7642 kJ/kg K P8 s = 0.6 MPa h8 s = 3310.2 kJ/kg s8 s = s7 T = h7 - h8 h8 = h7 - T (h7 - h8 s ) = 3479.1 - (0.84 )(3479.1 - 3310.2 ) h7 - h8 s = 3337.2 kJ/kg s 9 s - s f 7.7642 - 0.7549 = = 0.9665 P9 s = 15 kPa x9 s = s fg 7.2522 s9s = s7 h9 s = h f + x9 s h fg = 225.94 + (0.9665)(2372.3) = 2518.8 kJ/kg T = h7 - h9 h9 = h7 - T (h7 - h9 s ) = 3479.1 - (0.84)(3479.1 - 2518.8) h7 - h9 s = 2672.5 kJ/kg The fraction of steam extracted is determined from the steady-flow energy balance equation applied to the & & feedwater heaters. Noting that Q W ke pe 0 , & & & E in - E out = E system & & m h = m h i i 0 (steady) =0 & & E in = E out e e & & & m8 h8 + m2 h2 = m3 h3 yh8 + (1 - y )h2 = 1(h3 ) & & where y is the fraction of steam extracted from the turbine ( = m8 / m3 ). Solving for y, y= h3 - h2 670.38 - 226.53 = = 0.1427 h8 - h2 3335.3 - 226.53 (b) The thermal efficiency is determined from qin = (h5 - h4 ) + (h7 - h6 ) = (3375.1 - 680.73) + (3479.1 - 2878.4 ) = 3295.1 kJ/kg qout = (1 - y )(h9 - h1 ) = (1 - 0.1427 )(2672.5 - 225.94 ) = 2097.2 kJ/kg and th = 1 - q out 2097.2 kJ/kg = 1- = 36.4% q in 3295.1 kJ/kg 10-90 10-97 A steam power plant operates on an ideal reheat-regenerative Rankine cycle with one reheater and two feedwater heaters, one open and one closed. The fraction of steam extracted from the turbine for the open feedwater heater, the thermal efficiency of the cycle, and the net power output are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis 8 Boiler 9 10 11 y 5 Closed fwh 4 6 P II 3 Open fwh I 2 PI 12 z High-P Turbine Low-P Turbine 13 1-y-z 2 T 15 MPa 6 0.6 MPa 9 1 MPa 8 5 4 3 10 y 11 Condenser 1 1 z 12 0.2 MPa 7 1-y-z 5 kPa 13 s 7 (a) From the steam tables (Tables A-4, A-5, and A-6), h1 = h f @ 5 kPa @ 5 kPa = 137.75 kJ/kg = 0.001005 m 3 /kg v1 = v f wpI,in = v 1 (P2 - P1 ) 1 kJ = 0.001005 m 3 /kg (200 - 5 kPa ) 1 kPa m 3 = 0.20 kJ/kg ( ) h2 = h1 + wpI,in = 137.75 + 0.20 = 137.95 kJ/kg P3 = 0.2 MPa h3 = h f @ 0.2 MPa = 504.71 kJ/kg 3 sat.liquid v 3 = v f @ 0.2 MPa = 0.001061 m /kg wpII,in = v 3 (P4 - P3 ) 1 kJ = 0.001061 m3/kg (15,000 - 200 kPa ) 1 kPa m3 = 15.70 kJ/kg h4 = h3 + wpII,in = 504.71 + 15.70 = 520.41 kJ/kg ( ) P6 = 0.6 MPa h6 = h7 = h f @ 0.6 MPa = 670.38 kJ/kg 3 sat.liquid v 6 = v f @ 0.6 MPa = 0.001101 m /kg T6 = T5 h5 = h6 + v 6 (P5 - P6 ) 1 kJ = 670.38 + 0.001101 m 3 /kg (15,000 - 600 kPa ) 1 kPa m 3 = 686.23 kJ/kg ( ) P8 = 15 MPa T8 = 600 C h8 = 3583.1 kJ/kg s = 6.6796 kJ/kg K 8 P9 = 1.0 MPa h9 = 2820.8 kJ/kg s 9 = s8 P10 = 1.0 MPa h10 = 3479.1 kJ/kg T10 = 500 C s10 = 7.7642 kJ/kg K 10-91 P = 0.6 MPa 11 h11 = 3310.2 kJ/kg s11 = s10 P = 0.2 MPa 12 h12 = 3000.9 kJ/kg s12 = s10 x13 = s13 - s f s fg = 7.7642 - 0.4762 7.9176 = 0.9205 P = 5 kPa 13 h13 = h f + x13h fg s13 = s10 = 137.75 + (0.9205)(2423.0 ) = 2368.1 kJ/kg The fraction of steam extracted is determined from the steady-flow energy balance equation applied to the & & feedwater heaters. Noting that Q W ke pe 0 , & & & E in - E out = E system & & m h = m h i i 0 (steady) =0 & & Ein = E out e e & & m11 (h11 - h6 ) = m5 (h5 - h4 ) y (h11 - h6 ) = (h5 - h4 ) & & where y is the fraction of steam extracted from the turbine ( = m11 / m5 ). Solving for y, y= h5 - h4 686.23 - 520.41 = = 0.06287 h11 - h6 3310.2 - 670.38 & & & E in - E out = E system & & m h = m h i i 0 (steady) For the open FWH, =0 & & E in = E out e e & & & & m 7 h7 + m 2 h2 + m12 h12 = m3 h3 yh7 + (1 - y - z )h2 + zh12 = (1)h3 & & where z is the fraction of steam extracted from the turbine ( = m12 / m5 ) at the second stage. Solving for z, z= (h3 - h2 ) - y(h7 - h2 ) h12 - h2 = 504.71 - 137.95 - (0.06287 )(670.38 - 137.95) = 0.1165 3000.0 - 137.95 (b) q in = (h8 - h5 ) + (h10 - h9 ) = (3583.1 - 686.23) + (3479.1 - 2820.8) = 3555.3 kJ/kg q out = (1 - y - z )(h13 - h1 ) = (1 - 0.06287 - 0.1165)(2368.0 - 137.75) = 1830.4 kJ/kg wnet = q in - q out = 3555.3 - 1830.4 = 1724.9 kJ/kg and th = 1 - (c) q out 1830.4 kJ/kg = 1- = 48.5% 3555.3 kJ/kg q in & & Wnet = mwnet = (42 kg/s )(1724.9 kJ/kg ) = 72,447 kW 10-92 10-98 A cogeneration power plant is modified with reheat and that produces 3 MW of power and supplies 7 MW of process heat. The rate of heat input in the boiler and the fraction of steam extracted for process heating are to be determined. Assumptions 1 Steady operating conditions exist. 2 Kinetic and potential energy changes are negligible. Analysis (a) From the steam tables (Tables A-4, A-5, and A-6), 6 Turbine h1 = h f @ 15 kPa = 225.94 kJ/kg Boiler 7 h2 h1 h3 = h f @ 120 C = 503.81 kJ/kg P6 = 8 MPa h6 = 3399.5 kJ/kg T6 = 500 C s6 = 6.7266 kJ/kg K P7 = 1 MPa h7 = 2843.7 kJ/kg s7 = s6 8 5 Process heater 3 P II 4 2 PI 9 Condenser 1 P8 = 1 MPa h8 = 3479.1 kJ/kg T8 = 500 C s8 = 7.7642 kJ/kg K T s9 - s f 7.7642 - 0.7549 = = 0.9665 x9 = s fg 7.2522 P9 = 15 kPa h9 = h f + x9 h fg = 225.94 + (0.9665)(2372.3) s9 = s8 = 2518.8 kJ/kg 6 8 MPa 5 1 MPa 4 3 7 8 The mass flow rate through the process heater is & Qprocess 7,000 kJ/s & = = 2.992 kg/s m3 = h7 - h3 (2843.7 - 503.81) kJ/kg Also, or, 2 15 kPa 1 9 s & & & & & WT = m6 (h6 - h7 ) + m9 (h8 - h9 ) = m6 (h6 - h7 ) + (m6 - 2.993)(h8 - h9 ) & & 3000 kJ/s = m6 (3399.5 - 2843.7 ) + (m6 - 2.992 )(3479.1 - 2518.8) & m6 = 3.873 kg/s & & & m9 = m6 - m3 = 3.873 - 2.992 = 0.881 kg/s in out It yields and Mixing chamber: & & E -E & = E system 0 (steady) =0 & & & m4 h4 = m2 h2 + m3h3 & & m h = m h i i & & E in = E out e e or, Then, h4 h5 = & & m2 h2 + m3h3 (0.881)(225.94 ) + (2.992)(503.81) = = 440.60 kJ/kg & m4 3.873 & & & Qin = m6 (h6 - h5 ) + m8 (h8 - h7 ) = (3.873 kg/s )(3399.5 - 440.60 kJ/kg ) + (0.881 kg/s )(3479.1 - 2843.7 kJ/kg ) = 12,020 kW (b) The fraction of steam extracted for process heating is & m3 2.992 kg/s = = 77.3% y= & m total 3.873 kg/s
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UMass (Amherst) >> MIE >> 273 (Spring, 2008)
10-93 10-99 A combined gas-steam power plant is considered. The topping cycle is an ideal gas-turbine cycle and the bottoming cycle is an ideal reheat Rankine cycle. The mass flow rate of air in the gas-turbine cycle, the rate of total heat input, a...
UMass (Amherst) >> MIE >> 273 (Spring, 2008)
11-1 Chapter 11 REFRIGERATION CYCLES The Reversed Carnot Cycle 11-1C Because the compression process involves the compression of a liquid-vapor mixture which requires a compressor that will handle two phases, and the expansion process involves the e...
UMass (Amherst) >> MIE >> 273 (Spring, 2008)
11-36 Gas Refrigeration Cycles 11-49C The ideal gas refrigeration cycle is identical to the Brayton cycle, except it operates in the reversed direction. 11-50C The reversed Stirling cycle is identical to the Stirling cycle, except it operates in the...
UMass (Amherst) >> MIE >> 273 (Spring, 2008)
12-1 Chapter 12 THERMODYNAMIC PROPERTY RELATIONS Partial Derivatives and Associated Relations 12-1C z dz x dx (z)y (z)x y dy dz = (z ) x + (z ) y y x dx x +dx dy y + dy y x 12-2C For functions that depend on one variable, they are identical...
UMass (Amherst) >> MIE >> 273 (Spring, 2008)
12-29 12-58E The enthalpy of nitrogen at 400 R and 2000 psia is to be determined using data from the ideal-gas nitrogen table and the generalized enthalpy departure chart. Analysis (a) From the ideal gas table of nitrogen (Table A-18E) we read h = 2...
UMass (Amherst) >> MIE >> 273 (Spring, 2008)
13-1 Chapter 13 GAS MIXTURES Composition of Gas Mixtures 13-1C It is the average or the equivalent gas constant of the gas mixture. No. 13-2C No. We can do this only when each gas has the same mole fraction. 13-3C It is the average or the equivalent...
UMass (Amherst) >> MIE >> 273 (Spring, 2008)
13-35 13-64 Heat is transferred to a gas mixture contained in a piston cylinder device discussed in previous problem. The total entropy change and the exergy destruction are to be determined for two cases. Analysis The entropy generated during this ...
UMass (Amherst) >> MIE >> 273 (Spring, 2008)
14-1 Chapter 14 GAS-VAPOR MIXTURES AND AIR CONDITIONING Dry and Atmospheric Air, Specific and Relative Humidity 14-1C Yes; by cooling the air at constant pressure. 14-2C Yes. 14-3C Specific humidity will decrease but relative humidity will increase....
UMass (Amherst) >> MIE >> 273 (Spring, 2008)
14-20 14-69E Air enters a heating section at a specified pressure, temperature, velocity, and relative humidity. The exit temperature of air, the exit relative humidity, and the exit velocity are to be determined. Assumptions 1 This is a steady-flow...
UMass (Amherst) >> MIE >> 273 (Spring, 2008)
14-45 Adiabatic Mixing of Airstreams 14-100C This will occur when the straight line connecting the states of the two streams on the psychrometric chart crosses the saturation line. 14-101C Yes. 14-102 Two airstreams are mixed steadily. The specific...
UMass (Amherst) >> MIE >> 273 (Spring, 2008)
14-58 Review Problems 14-115 Air is compressed by a compressor and then cooled to the ambient temperature at high pressure. It is to be determined if there will be any condensation in the compressed air lines. Assumptions The air and the water vapo...
UMass (Amherst) >> MIE >> 273 (Spring, 2008)
15-1 Chapter 15 CHEMICAL REACTIONS Fuels and Combustion 15-1C Gasoline is C8H18, diesel fuel is C12H26, and natural gas is CH4. 15-2C Nitrogen, in general, does not react with other chemical species during a combustion process but its presence affec...
UMass (Amherst) >> MIE >> 273 (Spring, 2008)
15-24 First Law Analysis of Reacting Systems 15-46C In this case U + Wb = H, and the conservation of energy relation reduces to the form of the steady-flow energy relation. 15-47C The heat transfer will be the same for all cases. The excess oxygen a...
UMass (Amherst) >> MIE >> 273 (Spring, 2008)
15-43 Adiabatic Flame Temperature 15-68C For the case of stoichiometric amount of pure oxygen since we have the same amount of chemical energy released but a smaller amount of mass to absorb it. 15-69C Under the conditions of complete combustion wit...
UMass (Amherst) >> MIE >> 273 (Spring, 2008)
15-64 Review Problems 15-88 A sample of a certain fluid is burned in a bomb calorimeter. The heating value of the fuel is to be determined. Properties The specific heat of water is 4.18 kJ/kg.C (Table A-3). Analysis We take the water as the system,...
UMass (Amherst) >> MIE >> 273 (Spring, 2008)
15-83 15-102 A mixture of 40% by volume methane, CH4, and 60% by volume propane, C3H8, is burned completely with theoretical air. The amount of water formed during combustion process that will be condensed is to be determined. 40% CH4 Assumptions 1 ...
UMass (Amherst) >> MIE >> 273 (Spring, 2008)
16-1 Chapter 16 CHEMICAL AND PHASE EQUILIBRIUM The Kp and Equilibrium Composition of Ideal Gases 16-1C Because when a reacting system involves heat transfer, the increase-in-entropy principle relation requires a knowledge of heat transfer between th...
UMass (Amherst) >> MIE >> 273 (Spring, 2008)
16-17 16-29E A mixture of CO, O2, and N2 is heated to a high temperature at a constant pressure. The equilibrium composition is to be determined. Assumptions 1 The equilibrium composition consists of CO2, CO, O2, and N2. 2 The constituents of the mi...
UMass (Amherst) >> MIE >> 273 (Spring, 2008)
16-43 16-52 The KP value of the combustion process H2 + 1/2O2 H2O is to be determined at a specified temperature using hR data and KP value . Assumptions Both the reactants and products are ideal gases. Analysis The hR and KP data are related to ea...
UMass (Amherst) >> MIE >> 273 (Spring, 2008)
16-60 16-83 A mixture of H2 and O2 in a tank is ignited. The equilibrium composition of the product gases and the amount of heat transfer from the combustion chamber are to be determined. Assumptions 1 The equilibrium composition consists of H2O, H2...
UMass (Amherst) >> MIE >> 273 (Spring, 2008)
17-1 Chapter 17 COMPRESSIBLE FLOW Stagnation Properties 17-1C The temperature of the air will rise as it approaches the nozzle because of the stagnation process. 17-2C Stagnation enthalpy combines the ordinary enthalpy and the kinetic energy of a fl...
UMass (Amherst) >> MIE >> 273 (Spring, 2008)
17-64 Review Problems 17-118 A leak develops in an automobile tire as a result of an accident. The initial mass flow rate of air through the leak is to be determined. Assumptions 1 Air is an ideal gas with constant specific heats. 2 Flow of air thro...
Naval Academy >> SOC >> SOC 244 (Spring, 2008)
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Naval Academy >> SOC >> SOC 244 (Spring, 2008)
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UIllinois >> NRES >> 475 (Spring, 2008)
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UIllinois >> IB >> 420 (Spring, 2008)
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UIllinois >> IB >> 420 (Spring, 2008)
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UIllinois >> IB >> 420 (Spring, 2008)
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RIT >> COLA >> 0510-210 (Fall, 2006)
? , Article 2 ,. Napoleon Chagnon\'s War of Discovery He Wrote a Bestseller in the \'60s About One of the Last Undiscovered Peoples on Earth. Yet His Brash Style and Opinions Have Sabotaged His Research. Now He Is Forbidden to Visit the Jungle to Fi...
CofC >> CHEM >> 112 (Spring, 2008)
Chem 112 - Test 3 Spring 2008 Name \' 1. If 0.10 moles of KF dissolves in enough water to make 500 mL k3 f H+ a. What ions are found? I - solution then (20 pts) I L b. If any of the ions are acids andlo ases identify them, and provide Ka or Kb ...
UCSB >> MCDB >> 1B (Spring, 2008)
Name _ TA _ MCDB 1B Midterm Examination I February 14, 2007 Scantron Instructions: 1. Use a #2 pencil to complete the form. 2. Write your name and fill in the appropriate bubbles. 3. Write your perm. number in the ID number box and fill in the bubb...
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MCDB 1B MT 1; Yellow Key Quest Answer # 1 B 2 C 3 C 4 C 5 D 6 E 7 B 8 C 9 D 10 C 11 D 12 E 13 E 14 C 15 B 16 C 17 B 18 B 19 B 20 D 21 E 22 E 23 A 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 D E A A C E A D E B C E E B A ...
UCSB >> PHYS >> 6a (Winter, 2007)
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UCSB >> PHYS >> 6a (Winter, 2007)
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UCSB >> PHYS >> 6a (Winter, 2007)
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UCSB >> PHYS >> 6a (Winter, 2007)
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UCSB >> PHYS >> 6a (Winter, 2007)
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UCSB >> PHYS >> 6a (Winter, 2007)
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UCSB >> PHYS >> 6a (Winter, 2007)
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UCSB >> PHYS >> 6a (Winter, 2007)
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UCSB >> PHYS >> 6a (Winter, 2007)
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UCSB >> PHYS >> 6a (Winter, 2007)
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UCSB >> PHYS >> 6a (Winter, 2007)
PracticeMidterm2Physics6AWinter2008 1. Inthefigurebelow,whatisthetensioninropeA? a. 127Nb.146N c.253N d.317N 2. Apersonwithw=600NisridingonaFerrisWheelwithR=20m.The FerrisWheelisrotatingwithacircularspeedofvc=12m/s.Whatisthe normalforcethatthesea...
UCSB >> PHYS >> 6a (Winter, 2007)
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UCSB >> CHEM >> 6a (Winter, 2007)
Chem 6A AN INTRODUCTION TO ORGANIC LAB TECHNIQUES, COLLIGATIVE PROPERTIES, & SPECTROSCOPY A guide to teaching assistants and their students Modus Operandi (1-4) 1. TA responsibilities. Safety: For safety, TAs permit a maximum of eighteen students ...
UCSB >> CHEM >> 6a (Winter, 2007)
Experiment 2: separation of water and ethanol (Simple and Fractional Distillation) Mohrig, Chapter 11 Distillation is undoubtedly the most important purification technique for organic liquids (bp < 300 C). It involves heating a liquid to its boiling ...
UCSB >> CHEM >> 6a (Winter, 2007)
Experiment 3: Acid, Base, Neutral Separation (LiquidLiquid Extraction, Drying, recrystallization) Mohrig, Chapter 89 This experiment is designed to 1) demonstrate that immiscible solvents, such as water and ether, form separate layers on the basis of...
UCSB >> CHEM >> 6a (Winter, 2007)
Experiment 4: Isolation and Characterization of the Natural Product Caffeine (Solid-Liquid Extraction, Sublimation) Mohrig, Chapter 12 Lecture Ideas Describe the story of taxol and how it was isolated from the Yew tree (needles) and then semi-synthe...
UCSB >> CHEM >> 6a (Winter, 2007)
Experiment 5 Photochemical Isomerization of an Olefin: cis-1,2-Dibenzoylethylene: (TLC) Mohrig, Chapter 15 In this experiment, the technique of thin layer chromatography (TLC) along with destructive and non-destructive visualization techniques will b...
UCSB >> CHEM >> 6a (Winter, 2007)
Experiment 7: Carbonyl Reduction: Sodium Borohydride Reduction of 4-tert-Butylcyclohexanone. Mohrig, Chapter 18. See slides and Mohrig Chapters for a discussion of MS, IR & NMR Aldehydes and ketones play a central role in organic chemistry and many r...
UCSB >> CHEM >> 6a (Winter, 2007)
Experiment 6: Butene Synthesis by E1 dehydration of 2butanol (GC): Mohrig, Chapter 16-17 In this experiment, the non destructive technique of gas chromatography will be used to monitor the progress of a reaction over time. In gas chromatography, the ...
UCSB >> CHEM >> 6a (Winter, 2007)
Experiment 8: Williamson Ether Synthesis of Phenacetin. (IR, NMR, MS) Mohrig, Chapter 19-20 Lecture Ideas Again, discuss but don\'t quiz on the mechanisms. Many 109a students have still not covered SN2 reactions at this point in the lecture series. A...
UCSB >> CHEM >> 6a (Winter, 2007)
Experiment 9: An Unusual SN2 Displacement of a primary alcohol: Synthesis of n-Butyl Bromide Mohrig, Chapter 20 As was demonstrated by the previous phenacetin synthesis, substitutions reactions are useful. The synthesis of n-butyl bromide, which is c...
UCSB >> CHEM >> 6a (Winter, 2007)
NMR Spectroscopy Nuclear Magnetic Resonance Spectroscopy 1. Background Over the past fifty years nuclear magnetic resonance spectroscopy, commonly referred to as nmr, has become the preeminent technique for determining the structure of organic compo...
UCSB >> CHEM >> 6a (Winter, 2007)
NMR Topics Supplemental NMR Topics Spin Properties of Nuclei Nuclear spin may be related to the nucleon composition of a nucleus in the following manner: Odd mass nuclei (i.e. those having an odd number of nucleons) have fractional spins. Examples a...
UCSB >> CHEM >> 6a (Winter, 2007)
Group -X -R (alkyl) -Cl -Br -I -OH/OR -OPh -OC(=O)R -C(=O)H -C(=O)R -C(=O)Ph -C(=O)OH -C(=O)OR -CN -NH2 -NO2 CH3-X 0.8 3.0 2.7 2.2 3.2 3.8 3.6 2.2 2.1 2.4 2.1 1.8 2.2 2.5 4.1 RCH2-X 1.2 3.4 3.4 3.2 3.4 4.0 4.1 2.4 2.4 2.7 2.3 2.0 2.4 2.7 4.2 RR...
UCSB >> CHEM >> 6a (Winter, 2007)
Chem 6A Spectra All compounds from Experiment 1-9 Updated August 8, 2005 University of California at Santa Barbara! 07/05 2 Experiment 1 Chem 6a UCSB 07/05 3 Chem 6a UCSB 07/05 4 Chem 6a UCSB 07/05 5 Chem 6a UCSB 07/05 6 Chem 6a ...
UCSB >> MCDB >> 1A (Fall, 2007)
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UCSB >> MCDB >> 1A (Fall, 2007)
The Eukaryotic Genome and its Expression (Chapt 14) Table 14.1 A Comparison of Prokaryotic and Eukaryotic Genes and Genomes Eukaryotic genomes are larger than those of prokaryotes. Much of eukaryotic DNA is noncoding. Eukaryotes have multiple chr...
UCSB >> MCDB >> 1A (Fall, 2007)
Molecular Biology and Medicine Chpt. 17 Figure 17.3 Genetic Diseases of Membrane Proteins: Cystic Fibrosis Genetic Basis of Disease Genetic Markers RFLP mapping Human Genome Project Genetic Screening Gene Therapy Co E In 125 125 Co E ...
UCSB >> MCDB >> 1B (Winter, 2007)
Key Concepts General: Mechanisms and driving forces for transport (macro vs microscopic pumps, active vs. passive contributions, electrochemical gradients as sources of potential energy) Structure/function relationships of tissues, cell types, etc. R...
UCSB >> MCDB >> 1B (Winter, 2007)
Review of seedling growth controls Etiolated growth (regulation by light, brassinosteroids) Phototropism (regulation by light, auxin: D L transport and effects on growth) Wild-type Organ initiation (regulation by auxin) Recurring themes: Multiple...
UCSB >> MCDB >> 1B (Winter, 2007)
MCDB 1B: Physiology, Part II Dr. Ruth Finkelstein Study materials available online contain: -syllabus and contact information -anticipated figures for lectures -list of key concepts and vocabulary terms -old exam Other study resources: -textbook -o...
UCSB >> MCDB >> 1B (Winter, 2007)
Review from Monday\'s lecture: Key concepts: Macro- vs. microscopic pumps Active vs. passive contributions Structure/function relationships of tissues, cell types Regulatory mechanisms First example = circulatory system Structural organization, direct...
UCSB >> MCDB >> 1B (Winter, 2007)
Review: Purpose of excretory system = filtration and maintain osmotic balance (osmoregulation) Requirements and mechanisms vary depending on environment (osmoconformers vs. osmoregulators, need to conserve solutes vs water) Nitrogenous wastes must be...
UCSB >> MCDB >> 1B (Winter, 2007)
Summary of specialized zones of the renal tubules -proximal convoluted tubule: major site of salt, nutrient and water reabsorption, pH regulation, secretion of wastes -loop of Henle: creates external concentration gradient in medulla by countercurren...
UCSB >> MCDB >> 1B (Winter, 2007)
Xylem is major site of water and mineral movement Vascular system: water and mineral movement Site of movement (xylem) Driving force for movement = water potential gradient Path of water movement through plant Control of stomatal aperture Key co...
UCSB >> MCDB >> 1B (Winter, 2007)
Summary of path and driving force of water and mineral movement Water and minerals move in transpiration stream: roots -> leaves -> air Massive water flux (Ex. 15m tall tree transpires 220 liters/hr) Driving force for movement is water potential (...
UCSB >> MCDB >> 1B (Winter, 2007)
Photosynthesis 6 CO2 + 12 H2O + light C6H12O6 + 6 H2O + 6 O2 Chloroplasts are photosynthetic organelles thylakoid membranes are site of light reactions stroma is site of dark reactions Requirements: light, pigments, access to CO2 \"Light reactions\" ...
UCSB >> MCDB >> 1B (Winter, 2007)
Review Light reactions occur in thylakoids Light energy absorbed by pigments in antenna complexes Antenna complexes act as energetic funnel toward reaction center Absorption spectra reflect chemical structure of pigments Light energy converted to che...
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