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

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Run 1: Time AOA Q Temp C Pres ure Normal Axial Side Pitch Rol 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 3.01 41 23.92482 27.461 2 -5.37236 0.49995 -0.1 532 0.01598 -0.39506 -0.01408 -4.00000 -5.32440 0.87349 -0.1 532 -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 0.2001 1 -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 0.8381 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 23.8971 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 1 .71052 0.10715 0.23565 1.26974 1.26270 0.08289 6.00000 1 .63516 1.33065 0.23565 1.26270 -1.16605 0.03387 3.338331 0.381787 0.06761 -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
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