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F14 Data - Run 1 AOA Lift Force-8.33625-5.32440-1.81287...

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Run 1: Time AOA Q Temp C Pressure Normal Axial Side Pitch Roll Yaw AOA Lift Force Drag Force Side Force L aero ref M aero ref N aero ref CFl CFd CFs Cm Cl Cn 14:47.6 -6 2.99155 23.86284 27.46266 -8.42392 0.39723 -0.13199 -0.32825 -0.47132 -0.04899 -6.00000 -8.33625 1.27559 -0.13199 -0.47132 1.42392 -0.02153 -2.38783 0.365379 -0.03781 0.916556 -0.0477 -0.00218 15:20.1 -4 3.01141 23.92482 27.46112 -5.37236 0.49995 -0.11532 0.01598 -0.39506 -0.01408 -4.00000 -5.32440 0.87349 -0.11532 -0.39506 1.13343 0.00991 -1.51506 0.248552 -0.03282 0.724758 -0.03972 0.000996 15:52.8 -2 3.01000 23.92325 27.45853 -1.83630 0.63923 -0.06602 0.33025 -0.08257 -0.00340 -2.00000 -1.81287 0.70292 -0.06602 -0.08257 0.71220 0.01033 -0.5161 0.200111 -0.01879 0.455624 -0.00831 0.001039 16:24.8 0 3.01232 23.97607 27.45856 1.70068 0.68020 -0.00893 0.55736 0.20269 -0.01847 0.00000 1.70068 0.68020 -0.00893 0.20269 0.20362 -0.01662 0.483784 0.193493 -0.00254 0.130164 0.020374 -0.00167 16:57.9 2 2.99846 23.87405 27.45825 5.22652 0.61290 0.05047 0.83811 0.64978 -0.00585 2.00000 5.20195 0.79493 0.05047 0.64978 -0.24901 -0.01635 1.486609 0.227176 0.014424 -0.15991 0.065616 -0.00165 17:30.9 4 2.98994 23.89711 27.45979 8.49346 0.41423 0.14093 1.04335 0.97535 0.03726 4.00000 8.44388 1.00569 0.14093 0.97535 -0.72329 0.00795 2.419959 0.288225 0.040388 -0.46582 0.098774 0.000805 18:04.1 6 2.98657 23.89900 27.46037 11.71052 0.10715 0.23565 1.26974 1.26270 0.08289 6.00000 11.63516 1.33065 0.23565 1.26270 -1.16605 0.03387 3.338331 0.381787 0.067611 -0.75182 0.128017 0.003434 18:37.4 8 2.98059 23.91910 27.46016 14.92125 -0.22138 0.29796 1.46296 1.35469 0.22234 8.00000 14.80685 1.85741 0.29796 1.35469 -1.64066 0.16036 4.256855 0.533991 0.08566 -1.05995 0.13762 0.016291 19:10.8 10 2.97811 23.96265 27.45788 17.87721 -0.42137 0.38178 1.72373 1.40956 0.30647 10.00000 17.67879 2.68937 0.38178 1.40956 -1.99473 0.22706 5.086754 0.773819 0.109849 -1.28977 0.143313 0.023086 19:43.7 12 3.01872 23.92648 27.45697 20.17760 -0.08360 0.67951 1.98858 0.63365 -0.03766 12.00000 19.75405 4.11338 0.67951 0.63365 -2.20836 -0.17900 5.607416 1.167631 0.192886 -1.40869 0.063558 -0.01795 20:17.1 14 3.01254 24.00294 27.45707 22.59901 -0.12570 0.75411 2.31318 0.52258 -0.11063 14.00000 21.95814 5.34523 0.75411 0.52258 -2.38742 -0.26748 6.245859 1.520417 0.214502 -1.52604 0.052525 -0.02688 20:50.9 16 2.98704 23.95858 27.45806 25.38884 -0.17663 0.86208 2.54713 0.53119 -0.02898 16.00000 24.45400 6.82832 0.86208 0.53119 -2.73375 -0.20830 7.01516 1.958851 0.247306 -1.76233 0.053846 -0.02111 21:24.8 18 3.00688 23.98277 27.45641 28.50803 -0.09547 0.92030 3.11386 0.52777 -0.01880 18.00000 27.14225 8.71867 0.92030 0.52777 -2.81581 -0.21022 7.734986 2.484641 0.262265 -1.80325 0.053146 -0.02117 21:59.2 20 2.97478 23.91136 27.45782 31.05237 -0.06589 0.73291 3.30542 0.54639 0.15211 20.00000 29.20222 10.55862 0.73291 0.54639 -3.15348 -0.00033 8.411817 3.041453 0.211116 -2.04128 0.055614 -3E-005 Run 2: Time AOA Q Temp C Pressure Normal Axial Side Pitch Roll Yaw AOA Lift Force Drag Force Side Force L aero ref M aero ref N aero ref CFl
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