1 INPUT DATA 1. TEAM REVCON A-7D: WING, fuselage and tail 2. 4. 1. 5.754 247.9 -23.3 3. 3.0 4. 0.0 0.0 0.0 1.0 5. -2.21 -2.5 0.0 1.0 6. -14.5 -2.5 0.0 1.0 7. -14.5 0.0 0.0 1.0 8. 5.0 9. -14.5 0.0 0.0 1.0 10. -14.5 -2.5 0.0 1.0 11. -31.89 -28.18 0.0 1.0 12. -33.57 -28.18 0.0 1.0 13. -22.26 -2.5 0.0 1.0 14. -22.26 0.0 0.0 1.0 15. 3.0 16. -22.26 0.0 0.0 1.0 17. -22.26 -2.5 0.0 1.0 18. -43.17 -2.5 0.0 1.0 19. -43.17 0.0 0.0 1.0 20. 3.0 21. -35.4 -2.5 0.0 1.0 22. -43.23 -9.07 0.0 1.0 23. -44.73 -9.07 0.0 1.0 24. -42.12 -2.5 0.0 1.0 25. BASIC LINEAR AERO 15. 15. 0.85 0.55 1 GEOMETRY DATA FIRST REFERENCE PLANFORM HAS 3 CURVES ROOT CHORD HEIGHT = 0.00000 VARIABLE SWEEP PIVOT POSITION X(S) = 0.00000 Y(S) = 0.00000 BREAK POINTS FOR THE REFERENCE PLANFORM POINT X Y SWEEP DIHEDRAL MOVE REF REF ANGLE ANGLE CODE 1 23.30000 0.00000 41.47667 0.00000 1 2 21.09000 -2.50000 90.00000 0.00000 1 3 8.80000 -2.50000 0.00000 0.00000 1 4 8.80000 0.00000 SECOND REFERENCE PLANFORM HAS 5 CURVES ROOT CHORD HEIGHT = 0.00000 VARIABLE SWEEP PIVOT POSITION X(S) = 0.00000 Y(S) = 0.00000 BREAK POINTS FOR THE REFERENCE PLANFORM POINT X Y SWEEP DIHEDRAL MOVE REF REF ANGLE ANGLE CODE 1 8.80000 0.00000 0.00000 0.00000 1 2 8.80000 -2.50000 34.10509 0.00000 1 3 -8.59000 -28.18000 90.00000 0.00000 1 4 -10.27000 -28.18000 23.76968 0.00000 1 5 1.04000 -2.50000 0.00000 0.00000 1 6 1.04000 0.00000 THIRD REFERENCE PLANFORM HAS 3 CURVES ROOT CHORD HEIGHT = 0.00000 VARIABLE SWEEP PIVOT POSITION X(S) = 0.00000 Y(S) = 0.00000 BREAK POINTS FOR THE REFERENCE PLANFORM POINT X Y SWEEP DIHEDRAL MOVE REF REF ANGLE ANGLE CODE 1 1.04000 0.00000 0.00000 0.00000 1 2 1.04000 -2.50000 90.00000 0.00000 1 3 -19.87000 -2.50000 0.00000 0.00000 1 4 -19.87000 0.00000 FOURTH REFERENCE PLANFORM HAS 3 CURVES ROOT CHORD HEIGHT = 0.00000 VARIABLE SWEEP PIVOT POSITION X(S) = 0.00000 Y(S) = 0.00000 BREAK POINTS FOR THE REFERENCE PLANFORM POINT X Y SWEEP DIHEDRAL MOVE REF REF ANGLE ANGLE CODE 1 -12.10000 -2.50000 50.00064 0.00000 1 2 -19.93000 -9.07000 90.00000 0.00000 1 3 -21.43000 -9.07000 21.66596 0.00000 1 4 -18.82000 -2.50000 CONFIGURATION:BASIC LINEAR AERO SCW = 15.00 VIC = 15.00 MACH = 0.85 CLDES = 0.50 SA(I), I=1,4 = 0.05 0.00 0.00 0.00 TWIST(J), J=1,4 = 0.00 0.00 0.00 0.00 PTEST = 0.00 QTEST = 0.00 ATPCOD = 0.00 OPTREP = 0.00 IOPTR0(J),J=1,4 = 0 0 0 0 1 GEOMETRY DATA CONFIGURATION : BASIC LINEAR AERO BREAK POINTS FOR THIS CONFIGURATION POINT X Y Z SWEEP DIHEDRAL MOVE ANGLE ANGLE CODE FIRST PLANFORM BREAK POINTS 1 23.30000 0.00000 0.00000 41.47667 0.00000 1 2 21.09000 -2.50000 0.00000 90.00000 0.00000 1 3 8.80000 -2.50000 0.00000 0.00000 0.00000 1 4 8.80000 0.00000 0.00000 SECOND PLANFORM BREAK POINTS 1 8.80000 0.00000 0.00000 0.00000 0.00000 1 2 8.80000 -2.50000 0.00000 34.10509 0.00000 1 3 4.35092 -9.07000 0.00000 34.10509 0.00000 1 4 -8.59000 -28.18000 0.00000 90.00000 0.00000 1 5 -10.27000 -28.18000 0.00000 23.76968 0.00000 1 6 1.04000 -2.50000 0.00000 0.00000 0.00000 1 7 1.04000 0.00000 0.00000 THIRD PLANFORM BREAK POINTS 1 1.04000 0.00000 0.00000 0.00000 0.00000 1 2 1.04000 -2.50000 0.00000 90.00000 0.00000 1 3 -19.87000 -2.50000 0.00000 0.00000 0.00000 1 4 -19.87000 0.00000 0.00000 FOURTH PLANFORM BREAK POINTS 1 -12.10000 -2.50000 0.00000 50.00064 0.00000 1 2 -19.93000 -9.07000 0.00000 90.00000 0.00000 1 3 -21.43000 -9.07000 0.00000 21.66596 0.00000 1 4 -18.82000 -2.50000 0.00000 HORSESHOE VORTEX SUMMARY TABLE 285 HORSESHOE VORTICES USED ON THE LEFT HALF OF THIS CONFIGURATION PLANFORM TOTAL SPANWISE 1 15 1 2 210 14 3 15 1 4 45 3 0 15 HORSESHOE VORTICES IN EACH CHORDWISE ROW 1 AERODYNAMIC DATA CONFIGURATION : BASIC LINEAR AERO STATIC LONGITUDINAL AERODYNAMIC COEFFICIENTS ARE COMPUTED X X Y Z S C/4 SWEEP DIHEDRAL LOCAL ALPHA DELTA CP AT DESIRED C/4 3C/4 ANGLE ANGLE IN RADIANS CL = 0.50000 FIRST PLANFORM HORSESHOE VORTEX DESCRIPTIONS 21.97175 21.52525 -1.25000 0.00000 1.25000 40.99934 0.00000 0.00000 0.42507 21.07875 20.63225 -1.25000 0.00000 1.25000 39.01899 0.00000 0.00000 0.17044 20.18575 19.73925 -1.25000 0.00000 1.25000 36.92119 0.00000 0.00000 0.08717 19.29275 18.84625 -1.25000 0.00000 1.25000 34.70130 0.00000 0.00000 0.04777 18.39975 17.95325 -1.25000 0.00000 1.25000 32.35561 0.00000 0.00000 0.02826 17.50675 17.06025 -1.25000 0.00000 1.25000 29.88167 0.00000 0.00000 0.01858 16.61375 16.16725 -1.25000 0.00000 1.25000 27.27865 0.00000 0.00000 0.01409 15.72075 15.27425 -1.25000 0.00000 1.25000 24.54775 0.00000 0.00000 0.01263 14.82775 14.38125 -1.25000 0.00000 1.25000 21.69265 0.00000 0.00000 0.01326 13.93475 13.48825 -1.25000 0.00000 1.25000 18.71980 0.00000 0.00000 0.01581 13.04175 12.59525 -1.25000 0.00000 1.25000 15.63870 0.00000 0.00000 0.02070 12.14875 11.70225 -1.25000 0.00000 1.25000 12.46205 0.00000 0.00000 0.02917 11.25575 10.80925 -1.25000 0.00000 1.25000 9.20569 0.00000 0.00000 0.04387 10.36275 9.91625 -1.25000 0.00000 1.25000 5.88828 0.00000 0.00000 0.07052 9.46975 9.02325 -1.25000 0.00000 1.25000 2.53083 0.00000 0.00000 0.12251 SECOND PLANFORM HORSESHOE VORTEX DESCRIPTIONS -7.98561 -8.04902 -27.24067 0.00000 0.93933 33.94981 0.00000 0.00000 2.14950 -8.11244 -8.17585 -27.24067 0.00000 0.93933 33.32294 0.00000 0.00000 1.03419 -8.23926 -8.30268 -27.24067 0.00000 0.93933 32.68694 0.00000 0.00000 0.74021 -8.36609 -8.42950 -27.24067 0.00000 0.93933 32.04174 0.00000 0.00000 0.58297 -8.49292 -8.55633 -27.24067 0.00000 0.93933 31.38731 0.00000 0.00000 0.47677 -8.61974 -8.68316 -27.24067 0.00000 0.93933 30.72363 0.00000 0.00000 0.39634 -8.74657 -8.80998 -27.24067 0.00000 0.93933 30.05070 0.00000 0.00000 0.33158 -8.87339 -8.93681 -27.24067 0.00000 0.93933 29.36849 0.00000 0.00000 0.27781 -9.00022 -9.06363 -27.24067 0.00000 0.93933 28.67701 0.00000 0.00000 0.23234 -9.12705 -9.19046 -27.24067 0.00000 0.93933 27.97629 0.00000 0.00000 0.19332 -9.25387 -9.31729 -27.24067 0.00000 0.93933 27.26634 0.00000 0.00000 0.15932 -9.38070 -9.44411 -27.24067 0.00000 0.93933 26.54720 0.00000 0.00000 0.12913 -9.50753 -9.57094 -27.24067 0.00000 0.93933 25.81893 0.00000 0.00000 0.10151 -9.63435 -9.69777 -27.24067 0.00000 0.93933 25.08159 0.00000 0.00000 0.07492 -9.76118 -9.82459 -27.24067 0.00000 0.93933 24.33527 0.00000 0.00000 0.04638 -6.72083 -6.79907 -25.36200 0.00000 0.93933 33.94981 0.00000 0.00000 2.18430 -6.87731 -6.95555 -25.36200 0.00000 0.93933 33.32295 0.00000 0.00000 1.06374 -7.03379 -7.11203 -25.36200 0.00000 0.93933 32.68694 0.00000 0.00000 0.77287 -7.19026 -7.26850 -25.36200 0.00000 0.93933 32.04174 0.00000 0.00000 0.62012 -7.34674 -7.42498 -25.36200 0.00000 0.93933 31.38731 0.00000 0.00000 0.51896 -7.50322 -7.58146 -25.36200 0.00000 0.93933 30.72364 0.00000 0.00000 0.44358 -7.65970 -7.73794 -25.36200 0.00000 0.93933 30.05070 0.00000 0.00000 0.38334 -7.81618 -7.89442 -25.36200 0.00000 0.93933 29.36849 0.00000 0.00000 0.33285 -7.97266 -8.05090 -25.36200 0.00000 0.93933 28.67701 0.00000 0.00000 0.28900 -8.12914 -8.20738 -25.36200 0.00000 0.93933 27.97628 0.00000 0.00000 0.24973 -8.28562 -8.36386 -25.36200 0.00000 0.93933 27.26633 0.00000 0.00000 0.21357 -8.44210 -8.52034 -25.36200 0.00000 0.93933 26.54720 0.00000 0.00000 0.17931 -8.59858 -8.67682 -25.36200 0.00000 0.93933 25.81893 0.00000 0.00000 0.14568 -8.75506 -8.83330 -25.36200 0.00000 0.93933 25.08160 0.00000 0.00000 0.11083 -8.91154 -8.98978 -25.36200 0.00000 0.93933 24.33527 0.00000 0.00000 0.07049 -5.45604 -5.54911 -23.48334 0.00000 0.93933 33.94981 0.00000 0.00000 2.12805 -5.64218 -5.73524 -23.48334 0.00000 0.93933 33.32294 0.00000 0.00000 1.03837 -5.82831 -5.92137 -23.48334 0.00000 0.93933 32.68694 0.00000 0.00000 0.75604 -6.01444 -6.10751 -23.48334 0.00000 0.93933 32.04174 0.00000 0.00000 0.60814 -6.20057 -6.29364 -23.48334 0.00000 0.93933 31.38731 0.00000 0.00000 0.51062 -6.38670 -6.47977 -23.48334 0.00000 0.93933 30.72364 0.00000 0.00000 0.43841 -6.57284 -6.66590 -23.48334 0.00000 0.93933 30.05070 0.00000 0.00000 0.38104 -6.75897 -6.85204 -23.48334 0.00000 0.93933 29.36849 0.00000 0.00000 0.33311 -6.94510 -7.03817 -23.48334 0.00000 0.93933 28.67701 0.00000 0.00000 0.29145 -7.13123 -7.22430 -23.48334 0.00000 0.93933 27.97628 0.00000 0.00000 0.25398 -7.31737 -7.41043 -23.48334 0.00000 0.93933 27.26633 0.00000 0.00000 0.21918 -7.50350 -7.59656 -23.48334 0.00000 0.93933 26.54720 0.00000 0.00000 0.18579 -7.68963 -7.78270 -23.48334 0.00000 0.93933 25.81893 0.00000 0.00000 0.15245 -7.87576 -7.96883 -23.48334 0.00000 0.93933 25.08159 0.00000 0.00000 0.11716 -8.06189 -8.15496 -23.48334 0.00000 0.93933 24.33527 0.00000 0.00000 0.07527 -4.19126 -4.29915 -21.60467 0.00000 0.93933 33.94981 0.00000 0.00000 2.05789 -4.40705 -4.51494 -21.60467 0.00000 0.93933 33.32295 0.00000 0.00000 1.00453 -4.62283 -4.73072 -21.60467 0.00000 0.93933 32.68694 0.00000 0.00000 0.73159 -4.83862 -4.94651 -21.60467 0.00000 0.93933 32.04174 0.00000 0.00000 0.58866 -5.05440 -5.16229 -21.60467 0.00000 0.93933 31.38731 0.00000 0.00000 0.49464 -5.27019 -5.37808 -21.60467 0.00000 0.93933 30.72364 0.00000 0.00000 0.42528 -5.48597 -5.59386 -21.60467 0.00000 0.93933 30.05070 0.00000 0.00000 0.37033 -5.70176 -5.80965 -21.60467 0.00000 0.93933 29.36849 0.00000 0.00000 0.32446 -5.91754 -6.02543 -21.60467 0.00000 0.93933 28.67701 0.00000 0.00000 0.28458 -6.13333 -6.24122 -21.60467 0.00000 0.93933 27.97628 0.00000 0.00000 0.24865 -6.34911 -6.45700 -21.60467 0.00000 0.93933 27.26634 0.00000 0.00000 0.21519 -6.56490 -6.67279 -21.60467 0.00000 0.93933 26.54720 0.00000 0.00000 0.18295 -6.78068 -6.88857 -21.60467 0.00000 0.93933 25.81893 0.00000 0.00000 0.15059 -6.99647 -7.10436 -21.60467 0.00000 0.93933 25.08159 0.00000 0.00000 0.11611 -7.21225 -7.32014 -21.60467 0.00000 0.93933 24.33527 0.00000 0.00000 0.07485 -2.92648 -3.04920 -19.72600 0.00000 0.93933 33.94981 0.00000 0.00000 1.98565 -3.17192 -3.29463 -19.72600 0.00000 0.93933 33.32295 0.00000 0.00000 0.96931 -3.41735 -3.54007 -19.72600 0.00000 0.93933 32.68694 0.00000 0.00000 0.70585 -3.66279 -3.78551 -19.72600 0.00000 0.93933 32.04174 0.00000 0.00000 0.56793 -3.90823 -4.03095 -19.72600 0.00000 0.93933 31.38731 0.00000 0.00000 0.47741 -4.15367 -4.27639 -19.72600 0.00000 0.93933 30.72364 0.00000 0.00000 0.41080 -4.39911 -4.52182 -19.72600 0.00000 0.93933 30.05070 0.00000 0.00000 0.35808 -4.64454 -4.76726 -19.72600 0.00000 0.93933 29.36849 0.00000 0.00000 0.31408 -4.88998 -5.01270 -19.72600 0.00000 0.93933 28.67701 0.00000 0.00000 0.27579 -5.13542 -5.25814 -19.72600 0.00000 0.93933 27.97628 0.00000 0.00000 0.24126 -5.38086 -5.50358 -19.72600 0.00000 0.93933 27.26634 0.00000 0.00000 0.20906 -5.62629 -5.74901 -19.72600 0.00000 0.93933 26.54720 0.00000 0.00000 0.17798 -5.87173 -5.99445 -19.72600 0.00000 0.93933 25.81893 0.00000 0.00000 0.14670 -6.11717 -6.23989 -19.72600 0.00000 0.93933 25.08159 0.00000 0.00000 0.11327 -6.36261 -6.48533 -19.72600 0.00000 0.93933 24.33527 0.00000 0.00000 0.07313 -1.66169 -1.79924 -17.84734 0.00000 0.93933 33.94981 0.00000 0.00000 1.91354 -1.93679 -2.07433 -17.84734 0.00000 0.93933 33.32294 0.00000 0.00000 0.93410 -2.21188 -2.34942 -17.84734 0.00000 0.93933 32.68694 0.00000 0.00000 0.68012 -2.48697 -2.62451 -17.84734 0.00000 0.93933 32.04174 0.00000 0.00000 0.54728 -2.76206 -2.89960 -17.84734 0.00000 0.93933 31.38731 0.00000 0.00000 0.46028 -3.03715 -3.17469 -17.84734 0.00000 0.93933 30.72364 0.00000 0.00000 0.39634 -3.31224 -3.44978 -17.84734 0.00000 0.93933 30.05070 0.00000 0.00000 0.34574 -3.58733 -3.72488 -17.84734 0.00000 0.93933 29.36848 0.00000 0.00000 0.30350 -3.86242 -3.99997 -17.84734 0.00000 0.93933 28.67701 0.00000 0.00000 0.26672 -4.13751 -4.27506 -17.84734 0.00000 0.93933 27.97628 0.00000 0.00000 0.23351 -4.41260 -4.55015 -17.84734 0.00000 0.93933 27.26633 0.00000 0.00000 0.20251 -4.68769 -4.82524 -17.84734 0.00000 0.93933 26.54720 0.00000 0.00000 0.17255 -4.96278 -5.10033 -17.84734 0.00000 0.93933 25.81893 0.00000 0.00000 0.14235 -5.23787 -5.37542 -17.84734 0.00000 0.93933 25.08159 0.00000 0.00000 0.11000 -5.51297 -5.65051 -17.84734 0.00000 0.93933 24.33527 0.00000 0.00000 0.07108 -0.39691 -0.54928 -15.96867 0.00000 0.93933 33.94981 0.00000 0.00000 1.84149 -0.70166 -0.85403 -15.96867 0.00000 0.93933 33.32294 0.00000 0.00000 0.89902 -1.00640 -1.15877 -15.96867 0.00000 0.93933 32.68694 0.00000 0.00000 0.65464 -1.31114 -1.46351 -15.96867 0.00000 0.93933 32.04174 0.00000 0.00000 0.52698 -1.61589 -1.76826 -15.96867 0.00000 0.93933 31.38731 0.00000 0.00000 0.44352 -1.92063 -2.07300 -15.96867 0.00000 0.93933 30.72364 0.00000 0.00000 0.38223 -2.22537 -2.37775 -15.96867 0.00000 0.93933 30.05070 0.00000 0.00000 0.33370 -2.53012 -2.68249 -15.96867 0.00000 0.93933 29.36848 0.00000 0.00000 0.29316 -2.83486 -2.98723 -15.96867 0.00000 0.93933 28.67701 0.00000 0.00000 0.25783 -3.13960 -3.29198 -15.96867 0.00000 0.93933 27.97628 0.00000 0.00000 0.22590 -3.44435 -3.59672 -15.96867 0.00000 0.93933 27.26633 0.00000 0.00000 0.19606 -3.74909 -3.90146 -15.96867 0.00000 0.93933 26.54720 0.00000 0.00000 0.16717 -4.05384 -4.20621 -15.96867 0.00000 0.93933 25.81893 0.00000 0.00000 0.13801 -4.35858 -4.51095 -15.96867 0.00000 0.93933 25.08159 0.00000 0.00000 0.10671 -4.66332 -4.81569 -15.96867 0.00000 0.93933 24.33527 0.00000 0.00000 0.06900 0.86787 0.70067 -14.09000 0.00000 0.93933 33.94981 0.00000 0.00000 1.76857 0.53348 0.36628 -14.09000 0.00000 0.93933 33.32295 0.00000 0.00000 0.86376 0.19908 0.03188 -14.09000 0.00000 0.93933 32.68694 0.00000 0.00000 0.62929 -0.13532 -0.30251 -14.09000 0.00000 0.93933 32.04174 0.00000 0.00000 0.50702 -0.46971 -0.63691 -14.09000 0.00000 0.93933 31.38731 0.00000 0.00000 0.42719 -0.80411 -0.97131 -14.09000 0.00000 0.93933 30.72364 0.00000 0.00000 0.36856 -1.13851 -1.30570 -14.09000 0.00000 0.93933 30.05070 0.00000 0.00000 0.32211 -1.47290 -1.64010 -14.09000 0.00000 0.93933 29.36849 0.00000 0.00000 0.28325 -1.80730 -1.97450 -14.09000 0.00000 0.93933 28.67701 0.00000 0.00000 0.24935 -2.14170 -2.30889 -14.09000 0.00000 0.93933 27.97629 0.00000 0.00000 0.21866 -2.47609 -2.64329 -14.09000 0.00000 0.93933 27.26634 0.00000 0.00000 0.18993 -2.81049 -2.97769 -14.09000 0.00000 0.93933 26.54720 0.00000 0.00000 0.16207 -3.14489 -3.31208 -14.09000 0.00000 0.93933 25.81893 0.00000 0.00000 0.13389 -3.47928 -3.64648 -14.09000 0.00000 0.93933 25.08160 0.00000 0.00000 0.10360 -3.81368 -3.98088 -14.09000 0.00000 0.93933 24.33527 0.00000 0.00000 0.06703 2.13266 1.95063 -12.21134 0.00000 0.93933 33.94981 0.00000 0.00000 1.69329 1.76861 1.58658 -12.21134 0.00000 0.93933 33.32294 0.00000 0.00000 0.82775 1.40456 1.22253 -12.21134 0.00000 0.93933 32.68694 0.00000 0.00000 0.60381 1.04051 0.85848 -12.21134 0.00000 0.93933 32.04174 0.00000 0.00000 0.48730 0.67646 0.49443 -12.21134 0.00000 0.93933 31.38731 0.00000 0.00000 0.41130 0.31241 0.13038 -12.21134 0.00000 0.93933 30.72364 0.00000 0.00000 0.35545 -0.05164 -0.23367 -12.21134 0.00000 0.93933 30.05070 0.00000 0.00000 0.31115 -0.41569 -0.59772 -12.21134 0.00000 0.93933 29.36848 0.00000 0.00000 0.27402 -0.77974 -0.96176 -12.21134 0.00000 0.93933 28.67701 0.00000 0.00000 0.24155 -1.14379 -1.32581 -12.21134 0.00000 0.93933 27.97628 0.00000 0.00000 0.21209 -1.50784 -1.68986 -12.21134 0.00000 0.93933 27.26633 0.00000 0.00000 0.18443 -1.87189 -2.05391 -12.21134 0.00000 0.93933 26.54720 0.00000 0.00000 0.15753 -2.23594 -2.41796 -12.21134 0.00000 0.93933 25.81893 0.00000 0.00000 0.13025 -2.59999 -2.78201 -12.21134 0.00000 0.93933 25.08160 0.00000 0.00000 0.10085 -2.96404 -3.14606 -12.21134 0.00000 0.93933 24.33527 0.00000 0.00000 0.06529 3.50628 3.30815 -10.17100 0.00000 1.10100 33.94981 0.00000 0.00000 1.60414 3.11003 2.91190 -10.17100 0.00000 1.10100 33.32295 0.00000 0.00000 0.78564 2.71377 2.51565 -10.17100 0.00000 1.10100 32.68694 0.00000 0.00000 0.57475 2.31752 2.11939 -10.17100 0.00000 1.10100 32.04174 0.00000 0.00000 0.46531 1.92127 1.72314 -10.17100 0.00000 1.10100 31.38731 0.00000 0.00000 0.39396 1.52501 1.32688 -10.17100 0.00000 1.10100 30.72364 0.00000 0.00000 0.34147 1.12876 0.93063 -10.17100 0.00000 1.10100 30.05070 0.00000 0.00000 0.29975 0.73250 0.53438 -10.17100 0.00000 1.10100 29.36849 0.00000 0.00000 0.26468 0.33625 0.13812 -10.17100 0.00000 1.10100 28.67701 0.00000 0.00000 0.23388 -0.06001 -0.25813 -10.17100 0.00000 1.10100 27.97629 0.00000 0.00000 0.20580 -0.45626 -0.65439 -10.17100 0.00000 1.10100 27.26634 0.00000 0.00000 0.17931 -0.85251 -1.05064 -10.17100 0.00000 1.10100 26.54720 0.00000 0.00000 0.15342 -1.24877 -1.44690 -10.17100 0.00000 1.10100 25.81893 0.00000 0.00000 0.12704 -1.64502 -1.84315 -10.17100 0.00000 1.10100 25.08160 0.00000 0.00000 0.09851 -2.04128 -2.23940 -10.17100 0.00000 1.10100 24.33527 0.00000 0.00000 0.06386 4.87991 4.66568 -8.13067 0.00000 0.93933 33.94981 0.00000 0.00000 1.50945 4.45145 4.23722 -8.13067 0.00000 0.93933 33.32294 0.00000 0.00000 0.74057 4.02299 3.80876 -8.13067 0.00000 0.93933 32.68694 0.00000 0.00000 0.54339 3.59453 3.38030 -8.13067 0.00000 0.93933 32.04174 0.00000 0.00000 0.44177 3.16607 2.95184 -8.13067 0.00000 0.93933 31.38731 0.00000 0.00000 0.37583 2.73761 2.52338 -8.13067 0.00000 0.93933 30.72364 0.00000 0.00000 0.32743 2.30915 2.09492 -8.13067 0.00000 0.93933 30.05070 0.00000 0.00000 0.28891 1.88069 1.66646 -8.13067 0.00000 0.93933 29.36849 0.00000 0.00000 0.25640 1.45224 1.23801 -8.13067 0.00000 0.93933 28.67701 0.00000 0.00000 0.22764 1.02378 0.80955 -8.13067 0.00000 0.93933 27.97628 0.00000 0.00000 0.20117 0.59532 0.38109 -8.13067 0.00000 0.93933 27.26633 0.00000 0.00000 0.17591 0.16686 -0.04737 -8.13067 0.00000 0.93933 26.54720 0.00000 0.00000 0.15093 -0.26160 -0.47583 -8.13067 0.00000 0.93933 25.81893 0.00000 0.00000 0.12522 -0.69006 -0.90429 -8.13067 0.00000 0.93933 25.08160 0.00000 0.00000 0.09720 -1.11852 -1.33275 -8.13067 0.00000 0.93933 24.33527 0.00000 0.00000 0.06305 6.14469 5.91563 -6.25200 0.00000 0.93933 33.94981 0.00000 0.00000 1.41363 5.68658 5.45752 -6.25200 0.00000 0.93933 33.32295 0.00000 0.00000 0.69446 5.22847 4.99941 -6.25200 0.00000 0.93933 32.68694 0.00000 0.00000 0.51158 4.77035 4.54130 -6.25200 0.00000 0.93933 32.04174 0.00000 0.00000 0.41822 4.31224 4.08319 -6.25200 0.00000 0.93933 31.38731 0.00000 0.00000 0.35813 3.85413 3.62508 -6.25200 0.00000 0.93933 30.72364 0.00000 0.00000 0.31430 3.39602 3.16696 -6.25200 0.00000 0.93933 30.05070 0.00000 0.00000 0.27955 2.93791 2.70885 -6.25200 0.00000 0.93933 29.36849 0.00000 0.00000 0.25022 2.47980 2.25074 -6.25200 0.00000 0.93933 28.67701 0.00000 0.00000 0.22415 2.02168 1.79263 -6.25200 0.00000 0.93933 27.97628 0.00000 0.00000 0.19990 1.56357 1.33452 -6.25200 0.00000 0.93933 27.26634 0.00000 0.00000 0.17638 1.10546 0.87640 -6.25200 0.00000 0.93933 26.54720 0.00000 0.00000 0.15258 0.64735 0.41829 -6.25200 0.00000 0.93933 25.81893 0.00000 0.00000 0.12741 0.18924 -0.03982 -6.25200 0.00000 0.93933 25.08159 0.00000 0.00000 0.09927 -0.26887 -0.49793 -6.25200 0.00000 0.93933 24.33527 0.00000 0.00000 0.06447 7.72387 7.47631 -3.90633 0.00000 1.40633 33.94981 0.00000 0.00000 1.30264 7.22874 6.98117 -3.90633 0.00000 1.40633 33.32294 0.00000 0.00000 0.63037 6.73360 6.48603 -3.90633 0.00000 1.40633 32.68694 0.00000 0.00000 0.46311 6.23847 5.99090 -3.90633 0.00000 1.40633 32.04174 0.00000 0.00000 0.38059 5.74333 5.49576 -3.90633 0.00000 1.40633 31.38731 0.00000 0.00000 0.32921 5.24820 5.00063 -3.90633 0.00000 1.40633 30.72364 0.00000 0.00000 0.29264 4.75306 4.50549 -3.90633 0.00000 1.40633 30.05070 0.00000 0.00000 0.26404 4.25792 4.01036 -3.90633 0.00000 1.40633 29.36849 0.00000 0.00000 0.23999 3.76279 3.51522 -3.90633 0.00000 1.40633 28.67701 0.00000 0.00000 0.21856 3.26765 3.02008 -3.90633 0.00000 1.40633 27.97628 0.00000 0.00000 0.19848 2.77252 2.52495 -3.90633 0.00000 1.40633 27.26634 0.00000 0.00000 0.17879 2.27738 2.02981 -3.90633 0.00000 1.40633 26.54720 0.00000 0.00000 0.15853 1.78224 1.53468 -3.90633 0.00000 1.40633 25.81893 0.00000 0.00000 0.13644 1.28711 1.03954 -3.90633 0.00000 1.40633 25.08160 0.00000 0.00000 0.11030 0.79197 0.54440 -3.90633 0.00000 1.40633 24.33527 0.00000 0.00000 0.07456 8.67067 8.41200 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.21603 8.15333 7.89467 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.23457 7.63600 7.37733 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.24810 7.11867 6.86000 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.24972 6.60133 6.34267 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.24447 6.08400 5.82533 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.23551 5.56667 5.30800 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.22452 5.04933 4.79067 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.21235 4.53200 4.27333 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.19941 4.01467 3.75600 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.18581 3.49733 3.23867 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.17156 2.98000 2.72133 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.15650 2.46267 2.20400 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.14035 1.94533 1.68667 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.12244 1.42800 1.16933 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.09960 THIRD PLANFORM HORSESHOE VORTEX DESCRIPTIONS 0.69150 -0.00550 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.07660 -0.70250 -1.39950 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.05309 -2.09650 -2.79350 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.03578 -3.49050 -4.18750 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.02550 -4.88450 -5.58150 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.01926 -6.27850 -6.97550 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.01564 -7.67250 -8.36950 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.01422 -9.06650 -9.76350 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.01566 -10.46050 -11.15750 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.02296 -11.85450 -12.55150 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.04666 -13.24850 -13.94550 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.07699 -14.64250 -15.33950 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.07952 -16.03650 -16.73350 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.06996 -17.43050 -18.12750 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.05404 -18.82450 -19.52150 -1.25000 0.00000 1.25000 0.00000 0.00000 0.00000 0.03215 FOURTH PLANFORM HORSESHOE VORTEX DESCRIPTIONS -18.84796 -18.92284 -8.13067 0.00000 0.93933 49.68510 0.00000 0.00000 0.86575 -18.99772 -19.07259 -8.13067 0.00000 0.93933 48.38087 0.00000 0.00000 0.43123 -19.14747 -19.22235 -8.13067 0.00000 0.93933 47.00623 0.00000 0.00000 0.32066 -19.29723 -19.37210 -8.13067 0.00000 0.93933 45.55699 0.00000 0.00000 0.26339 -19.44698 -19.52186 -8.13067 0.00000 0.93933 44.02897 0.00000 0.00000 0.22546 -19.59674 -19.67161 -8.13067 0.00000 0.93933 42.41788 0.00000 0.00000 0.19663 -19.74649 -19.82137 -8.13067 0.00000 0.93933 40.71958 0.00000 0.00000 0.17257 -19.89624 -19.97112 -8.13067 0.00000 0.93933 38.92997 0.00000 0.00000 0.15119 -20.04600 -20.12087 -8.13067 0.00000 0.93933 37.04530 0.00000 0.00000 0.13152 -20.19575 -20.27063 -8.13067 0.00000 0.93933 35.06218 0.00000 0.00000 0.11317 -20.34551 -20.42038 -8.13067 0.00000 0.93933 32.97786 0.00000 0.00000 0.09597 -20.49526 -20.57014 -8.13067 0.00000 0.93933 30.79029 0.00000 0.00000 0.07968 -20.64502 -20.71989 -8.13067 0.00000 0.93933 28.49853 0.00000 0.00000 0.06394 -20.79477 -20.86965 -8.13067 0.00000 0.93933 26.10274 0.00000 0.00000 0.04805 -20.94452 -21.01940 -8.13067 0.00000 0.93933 23.60468 0.00000 0.00000 0.03021 -16.63388 -16.75851 -6.25200 0.00000 0.93933 49.68511 0.00000 0.00000 0.70595 -16.88314 -17.00777 -6.25200 0.00000 0.93933 48.38088 0.00000 0.00000 0.35331 -17.13241 -17.25704 -6.25200 0.00000 0.93933 47.00623 0.00000 0.00000 0.26392 -17.38167 -17.50630 -6.25200 0.00000 0.93933 45.55700 0.00000 0.00000 0.21765 -17.63093 -17.75557 -6.25200 0.00000 0.93933 44.02897 0.00000 0.00000 0.18696 -17.88020 -18.00483 -6.25200 0.00000 0.93933 42.41790 0.00000 0.00000 0.16378 -18.12946 -18.25410 -6.25200 0.00000 0.93933 40.71958 0.00000 0.00000 0.14501 -18.37873 -18.50336 -6.25200 0.00000 0.93933 38.92997 0.00000 0.00000 0.12907 -18.62799 -18.75262 -6.25200 0.00000 0.93933 37.04529 0.00000 0.00000 0.11495 -18.87725 -19.00189 -6.25200 0.00000 0.93933 35.06218 0.00000 0.00000 0.10192 -19.12652 -19.25115 -6.25200 0.00000 0.93933 32.97785 0.00000 0.00000 0.08939 -19.37578 -19.50041 -6.25200 0.00000 0.93933 30.79030 0.00000 0.00000 0.07688 -19.62505 -19.74968 -6.25200 0.00000 0.93933 28.49852 0.00000 0.00000 0.06386 -19.87431 -19.99894 -6.25200 0.00000 0.93933 26.10274 0.00000 0.00000 0.04955 -20.12357 -20.24821 -6.25200 0.00000 0.93933 23.60466 0.00000 0.00000 0.03210 -13.86942 -14.05617 -3.90633 0.00000 1.40633 49.68511 0.00000 0.00000 0.54648 -14.24293 -14.42968 -3.90633 0.00000 1.40633 48.38089 0.00000 0.00000 0.27285 -14.61644 -14.80319 -3.90633 0.00000 1.40633 47.00623 0.00000 0.00000 0.20444 -14.98995 -15.17670 -3.90633 0.00000 1.40633 45.55700 0.00000 0.00000 0.16963 -15.36346 -15.55021 -3.90633 0.00000 1.40633 44.02897 0.00000 0.00000 0.14720 -15.73697 -15.92372 -3.90633 0.00000 1.40633 42.41790 0.00000 0.00000 0.13105 -16.11048 -16.29723 -3.90633 0.00000 1.40633 40.71958 0.00000 0.00000 0.11824 -16.48398 -16.67074 -3.90633 0.00000 1.40633 38.92998 0.00000 0.00000 0.10718 -16.85749 -17.04425 -3.90633 0.00000 1.40633 37.04530 0.00000 0.00000 0.09739 -17.23100 -17.41776 -3.90633 0.00000 1.40633 35.06219 0.00000 0.00000 0.08847 -17.60451 -17.79127 -3.90633 0.00000 1.40633 32.97786 0.00000 0.00000 0.07954 -17.97802 -18.16478 -3.90633 0.00000 1.40633 30.79030 0.00000 0.00000 0.07004 -18.35153 -18.53828 -3.90633 0.00000 1.40633 28.49852 0.00000 0.00000 0.05980 -18.72504 -18.91179 -3.90633 0.00000 1.40633 26.10275 0.00000 0.00000 0.04792 -19.09855 -19.28530 -3.90633 0.00000 1.40633 23.60466 0.00000 0.00000 0.03196 REF. CHORD C AVERAGE TRUE AREA REFERENCE AREA B/2 REF. AR TRUE AR MACH NUMBER 5.75400 8.99130 506.74951 247.89999 28.18000 12.81343 6.26828 0.85000 1 COMPLETE CONFIGURATION WING-BODY CHARACTERISTICS LIFT INDUCED DRAG (FAR FIELD SOLUTION) DESIRED CL COMPUTED ALPHA CL(WB) CDI AT CL(WB) CDI/(CL(WB)**2) (1/PI*AR REF) = 0.02484) 0.50000 3.30886 0.42606 0.00550 0.03030 COMPLETE CONFIGURATION CHARACTERISTICS CL ALPHA CL(TWIST) ALPHA AT CL=0 Y CP CM/CL CMO PER RADIAN PER DEGREE 8.65793 0.15111 0.00000 0.00000 -0.39906 -0.08683 0.00000 FIRST PLANFORM 0.34926 0.00610 0.00000 0.00000 -0.04436 SECOND PLANFORM 7.37763 0.12876 0.00000 0.00000 -0.44815 THIRD PLANFORM 0.31063 0.00542 0.00000 0.00000 -0.04436 FOURTH PLANFORM 0.62041 0.01083 0.00000 0.00000 -0.19256 ADDITIONAL LOADING WITH CL BASED ON S(TRUE) -AT CL DES- LOAD DUE ADD. LOAD AT BASIC LOAD SPAN LOAD AT X LOCATION OF STATION 2Y/B SL COEF CL RATIO C RATIO TO TWIST CL= 0.00000 AT CL=0 DESIRED CL LOCAL CENT PR FIRST PLANFORM SPAN LOAD DISTRIBUTION 1 -0.04436 0.45471 0.30522 1.48978 0.00000 0.00000 0.00000 0.11122 18.14280 SECOND PLANFORM SPAN LOAD DISTRIBUTION 2 -0.96667 0.39942 1.88781 0.21158 0.00000 0.00000 0.00000 0.09770 -8.38003 3 -0.90000 0.53921 2.06553 0.26105 0.00000 0.00000 0.00000 0.13189 -7.26257 4 -0.83333 0.63383 2.04119 0.31052 0.00000 0.00000 0.00000 0.15503 -6.11434 5 -0.76667 0.71335 1.98157 0.35999 0.00000 0.00000 0.00000 0.17448 -4.95924 6 -0.70000 0.78414 1.91506 0.40946 0.00000 0.00000 0.00000 0.19180 -3.80249 7 -0.63333 0.84802 1.84783 0.45893 0.00000 0.00000 0.00000 0.20742 -2.64565 8 -0.56667 0.90559 1.78127 0.50840 0.00000 0.00000 0.00000 0.22151 -1.48960 9 -0.50000 0.95705 1.71554 0.55787 0.00000 0.00000 0.00000 0.23409 -0.33530 10 -0.43333 1.00247 1.65061 0.60734 0.00000 0.00000 0.00000 0.24520 0.81551 11 -0.36093 1.04350 1.57851 0.66106 0.00000 0.00000 0.00000 0.25524 2.05793 12 -0.28853 1.07636 1.50584 0.71479 0.00000 0.00000 0.00000 0.26327 3.28846 13 -0.22186 1.10072 1.44025 0.76426 0.00000 0.00000 0.00000 0.26924 4.39680 14 -0.13862 1.12079 1.35685 0.82602 0.00000 0.00000 0.00000 0.27414 5.74222 15 -0.04436 0.69180 0.80157 0.86306 0.00000 0.00000 0.00000 0.16921 5.53178 THIRD PLANFORM SPAN LOAD DISTRIBUTION 16 -0.04436 0.40442 0.17390 2.32558 0.00000 0.00000 0.00000 0.09892 -9.77780 FOURTH PLANFORM SPAN LOAD DISTRIBUTION 17 -0.28853 0.21718 0.86930 0.24983 0.00000 0.00000 0.00000 0.05312 -19.39089 18 -0.22186 0.30537 0.73434 0.41584 0.00000 0.00000 0.00000 0.07469 -17.58777 19 -0.13862 0.36891 0.59204 0.62312 0.00000 0.00000 0.00000 0.09024 -15.38664 INDUCED DRAG, LEADING EDGE THRUST AND SUCTION COEFFICIENT CHARACTERISTICS COMPUTED AT THE DESIRED CL FROM A NEAR FIELD SOLUTION SECTION COEFFICIENTS L. E. SWEEP STATION 2Y/B ANGLE CDII C/2B CT C/2B CS C/2B CONTRIBUTION OF THE FIRST PLANFORM TO THE CHORD OR DRAG FORCE 1 -0.04436 41.47667 0.00052 -0.00001 -0.00001 CONTRIBUTION OF THE SECOND PLANFORM TO THE CHORD OR DRAG FORCE 2 -0.96667 34.10510 -0.00016 0.00061 0.00074 3 -0.90000 34.10510 -0.00014 0.00075 0.00090 4 -0.83333 34.10510 -0.00012 0.00084 0.00101 5 -0.76667 34.10510 -0.00010 0.00090 0.00109 6 -0.70000 34.10510 -0.00007 0.00095 0.00115 7 -0.63333 34.10510 -0.00003 0.00099 0.00119 8 -0.56667 34.10510 0.00001 0.00101 0.00122 9 -0.50000 34.10510 0.00007 0.00101 0.00122 10 -0.43333 34.10510 0.00013 0.00100 0.00121 11 -0.36093 34.10510 0.00021 0.00096 0.00116 12 -0.28853 34.10510 0.00032 0.00089 0.00107 13 -0.22186 34.10510 0.00056 0.00068 0.00082 14 -0.13862 34.10510 -0.00002 0.00119 0.00132 15 -0.04436 0.00000 0.00120 -0.00039 -0.00037 CONTRIBUTION OF THE THIRD PLANFORM TO THE CHORD OR DRAG FORCE 16 -0.04436 0.00000 0.00084 -0.00038 -0.00038 CONTRIBUTION OF THE FOURTH PLANFORM TO THE CHORD OR DRAG FORCE 17 -0.28853 50.00064 0.00011 0.00015 0.00023 18 -0.22186 50.00064 0.00024 0.00010 0.00015 19 -0.13862 50.00064 -0.00007 0.00048 0.00074 TOTAL COEFFICIENTS CDII/CL**2 = 0.02642 CT= 0.02162 CS= 0.02666 1 END OF FILE ENCOUNTERED AFTER CONFIGURATION BASIC LINEAR AERO