vortex lattice aerodynamic computation program nasa-lrc no. a2794 by j.e. lamar and b.b. gloss modified for watfor77 with 72 column output YF-23 Flaps Down geometry data first reference planform has 6 curves center of gravity = 0.00000 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 37.80000 0.00000 73.89906 0.00000 1 2 22.73000 -4.35000 90.00000 0.00000 1 3 14.69000 -4.35000 39.96069 0.00000 1 4 0.11000 -21.75000 90.00000 0.00000 1 5 -3.24000 -21.75000 -40.15675 0.00000 1 6 -14.96000 -7.86000 0.00000 0.00000 1 7 -14.96000 0.00000 second reference planform has 8 curves center of gravity = 0.00000 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 -14.96000 0.00000 0.00000 0.00000 1 2 -14.96000 -7.86000 37.91007 43.00000 1 3 -22.00000 -16.90000 90.00000 0.00000 1 4 -24.51000 -16.90000 -38.87364 43.00000 1 5 -29.50000 -10.71000 41.02898 43.00000 1 6 -27.02000 -7.86000 -53.26718 0.00000 1 7 -28.36000 -6.86000 41.68077 0.00000 1 8 -25.68000 -3.85000 -42.43623 0.00000 1 9 -29.20000 0.00000 1 configuration no. 23. curve 1 is swept 73.89906 degrees on planform 1 curve 1 is swept 0.00000 degrees on planform 2 break points for this configuration point x y z sweep dihedral move angle angle code 1 37.80000 0.00000 0.00000 73.89906 0.00000 1 2 24.46218 -3.85000 0.00000 73.89906 0.00000 1 3 22.73000 -4.35000 0.00000 90.00000 0.00000 1 4 14.69000 -4.35000 0.00000 39.96069 0.00000 1 5 12.58679 -6.86000 0.00000 39.96069 0.00000 1 6 9.36076 -10.71000 0.00000 39.96069 0.00000 1 7 4.17397 -16.90000 0.00000 39.96069 0.00000 1 8 0.11000 -21.75000 0.00000 90.00000 0.00000 1 9 -3.24000 -21.75000 0.00000 -40.15676 0.00000 1 10 -14.96000 -7.86000 0.00000 0.00000 0.00000 1 11 -14.96000 0.00000 0.00000 second planform breakpoints 1 -14.96000 0.00000 0.00000 0.00000 0.00000 1 2 -14.96000 -4.35000 0.00000 0.00000 0.00000 1 3 -14.96000 -7.86000 0.00000 37.91007 43.00000 1 4 -22.00000 -16.90000 -8.42994 90.00000 0.00000 1 5 -24.51000 -16.90000 -8.42994 -38.87364 43.00000 1 6 -29.50000 -10.71000 -2.65767 41.02898 43.00000 1 7 -27.02000 -7.86000 0.00000 -53.26718 0.00000 1 8 -28.36000 -6.86000 0.00000 41.68077 0.00000 1 9 -25.68000 -3.85000 0.00000 -42.43624 0.00000 1 10 -29.20000 0.00000 0.00000 168 horseshoe vortices used on the left half of the configuration planform total spanwise 1 90 15 2 78 13 6. horseshoe vortices in each chordwise row 1 aerodynamic data configuration no. 23. static longitudinal aerodynamic coefficients are computed x x y z s c/4 3c/4 0.61276 0.21636 -20.91346 0.00000 0.83654 -0.18004 -0.57644 -20.91346 0.00000 0.83654 -0.97284 -1.36924 -20.91346 0.00000 0.83654 -1.76564 -2.16204 -20.91346 0.00000 0.83654 -2.55845 -2.95485 -20.91346 0.00000 0.83654 -3.35125 -3.74765 -20.91346 0.00000 0.83654 1.89745 1.26658 -19.24039 0.00000 0.83654 0.63571 0.00484 -19.24039 0.00000 0.83654 -0.62603 -1.25690 -19.24039 0.00000 0.83654 -1.88776 -2.51863 -19.24039 0.00000 0.83654 -3.14950 -3.78037 -19.24039 0.00000 0.83654 -4.41124 -5.04211 -19.24039 0.00000 0.83654 3.11717 2.26369 -17.65192 0.00000 0.75192 1.41021 0.55673 -17.65192 0.00000 0.75192 -0.29675 -1.15023 -17.65192 0.00000 0.75192 -2.00371 -2.85719 -17.65192 0.00000 0.75192 -3.71067 -4.56415 -17.65192 0.00000 0.75192 -5.41763 -6.27110 -17.65192 0.00000 0.75192 4.33688 3.26079 -16.06346 0.00000 0.83654 2.18470 1.10861 -16.06346 0.00000 0.83654 0.03253 -1.04356 -16.06346 0.00000 0.83654 -2.11965 -3.19574 -16.06346 0.00000 0.83654 -4.27183 -5.34792 -16.06346 0.00000 0.83654 -6.42401 -7.50010 -16.06346 0.00000 0.83654 5.62157 4.31101 -14.39038 0.00000 0.83654 3.00046 1.68990 -14.39038 0.00000 0.83654 0.37934 -0.93122 -14.39038 0.00000 0.83654 -2.24177 -3.55233 -14.39038 0.00000 0.83654 -4.86289 -6.17345 -14.39038 0.00000 0.83654 -7.48401 -8.79456 -14.39038 0.00000 0.83654 6.90626 5.36123 -12.71731 0.00000 0.83654 3.81621 2.27118 -12.71731 0.00000 0.83654 0.72616 -0.81887 -12.71731 0.00000 0.83654 -2.36390 -3.90892 -12.71731 0.00000 0.83654 -5.45395 -6.99897 -12.71731 0.00000 0.83654 -8.54400 -10.08903 -12.71731 0.00000 0.83654 7.99810 6.25380 -11.29539 0.00000 0.58538 4.50950 2.76521 -11.29539 0.00000 0.58538 1.02091 -0.72339 -11.29539 0.00000 0.58538 -2.46768 -4.21198 -11.29539 0.00000 0.58538 -5.95628 -7.70058 -11.29539 0.00000 0.58538 -9.44487 -11.18917 -11.29539 0.00000 0.58538 9.08994 7.14637 -9.87346 0.00000 0.83654 5.20280 3.25923 -9.87346 0.00000 0.83654 1.31566 -0.62790 -9.87346 0.00000 0.83654 -2.57147 -4.51504 -9.87346 0.00000 0.83654 -6.45861 -8.40218 -9.87346 0.00000 0.83654 -10.34575 -12.28931 -9.87346 0.00000 0.83654 10.18414 8.04087 -8.44846 0.00000 0.58846 5.89760 3.75432 -8.44846 0.00000 0.58846 1.61105 -0.53222 -8.44846 0.00000 0.58846 -2.67549 -4.81876 -8.44846 0.00000 0.58846 -6.96203 -9.10530 -8.44846 0.00000 0.58846 -11.24857 -13.39184 -8.44846 0.00000 0.58846 11.03750 8.77685 -7.36000 0.00000 0.50000 6.51620 4.25554 -7.36000 0.00000 0.50000 1.99489 -0.26576 -7.36000 0.00000 0.50000 -2.52641 -4.78706 -7.36000 0.00000 0.50000 -7.04772 -9.30837 -7.36000 0.00000 0.50000 -11.56902 -13.82967 -7.36000 0.00000 0.50000 12.11076 9.75678 -6.02346 0.00000 0.83654 7.40281 5.04883 -6.02346 0.00000 0.83654 2.69485 0.34087 -6.02346 0.00000 0.83654 -2.01311 -4.36709 -6.02346 0.00000 0.83654 -6.72107 -9.07505 -6.02346 0.00000 0.83654 -11.42903 -13.78301 -6.02346 0.00000 0.83654 13.11855 10.67694 -4.76846 0.00000 0.41846 8.23532 5.79371 -4.76846 0.00000 0.41846 3.35210 0.91049 -4.76846 0.00000 0.41846 -1.53113 -3.97274 -4.76846 0.00000 0.41846 -6.41435 -8.85597 -4.76846 0.00000 0.41846 -11.29758 -13.73919 -4.76846 0.00000 0.41846 21.98959 18.77658 -4.10000 0.00000 0.25000 15.56357 12.35056 -4.10000 0.00000 0.25000 9.13756 5.92455 -4.10000 0.00000 0.25000 2.71154 -0.50147 -4.10000 0.00000 0.25000 -3.71447 -6.92748 -4.10000 0.00000 0.25000 -10.14049 -13.35350 -4.10000 0.00000 0.25000 25.59691 22.07023 -3.01346 0.00000 0.83654 18.54354 15.01685 -3.01346 0.00000 0.83654 11.49016 7.96347 -3.01346 0.00000 0.83654 4.43679 0.91010 -3.01346 0.00000 0.83654 -2.61659 -6.14328 -3.01346 0.00000 0.83654 -9.66997 -13.19666 -3.01346 0.00000 0.83654 31.98795 27.90552 -1.08846 0.00000 1.08846 23.82309 19.74066 -1.08846 0.00000 1.08846 15.65823 11.57580 -1.08846 0.00000 1.08846 7.49337 3.41094 -1.08846 0.00000 1.08846 -0.67149 -4.75393 -1.08846 0.00000 1.08846 -8.83636 -12.91879 -1.08846 0.00000 1.08846 second planform horseshoe vortex descriptions -21.66854 -21.95851 -16.28819 -7.85942 0.83654 -22.24848 -22.53845 -16.28819 -7.85942 0.83654 -22.82842 -23.11839 -16.28819 -7.85942 0.83654 -23.40836 -23.69833 -16.28819 -7.85942 0.83654 -23.98830 -24.27827 -16.28819 -7.85942 0.83654 -24.56824 -24.85822 -16.28819 -7.85942 0.83654 -20.79644 -21.24802 -15.06458 -6.71838 0.83654 -21.69960 -22.15118 -15.06458 -6.71838 0.83654 -22.60276 -23.05434 -15.06458 -6.71838 0.83654 -23.50591 -23.95749 -15.06458 -6.71838 0.83654 -24.40907 -24.86065 -15.06458 -6.71838 0.83654 -25.31223 -25.76381 -15.06458 -6.71838 0.83654 -19.92434 -20.53753 -13.84097 -5.57735 0.83654 -21.15072 -21.76390 -13.84097 -5.57735 0.83654 -22.37709 -22.99028 -13.84097 -5.57735 0.83654 -23.60347 -24.21665 -13.84097 -5.57735 0.83654 -24.82984 -25.44303 -13.84097 -5.57735 0.83654 -26.05622 -26.66940 -13.84097 -5.57735 0.83654 -19.05225 -19.82704 -12.61736 -4.43631 0.83654 -20.60184 -21.37664 -12.61736 -4.43631 0.83654 -22.15143 -22.92623 -12.61736 -4.43631 0.83654 -23.70102 -24.47582 -12.61736 -4.43631 0.83654 -25.25062 -26.02541 -12.61736 -4.43631 0.83654 -26.80021 -27.57500 -12.61736 -4.43631 0.83654 -18.15451 -19.09567 -11.35778 -3.26173 0.88572 -20.03682 -20.97798 -11.35778 -3.26173 0.88572 -21.91913 -22.86029 -11.35778 -3.26173 0.88572 -23.80145 -24.74260 -11.35778 -3.26173 0.88572 -25.68376 -26.62491 -11.35778 -3.26173 0.88572 -27.56607 -28.50722 -11.35778 -3.26173 0.88572 -17.21404 -18.23609 -10.09819 -2.08715 0.83654 -19.25814 -20.28019 -10.09819 -2.08715 0.83654 -21.30224 -22.32430 -10.09819 -2.08715 0.83654 -23.34634 -24.36839 -10.09819 -2.08715 0.83654 -25.39045 -26.41250 -10.09819 -2.08715 0.83654 -27.43455 -28.45660 -10.09819 -2.08715 0.83654 -16.09888 -17.11008 -8.67319 -0.75832 1.11190 -18.12127 -19.13247 -8.67319 -0.75832 1.11190 -20.14366 -21.15486 -8.67319 -0.75832 1.11190 -22.16605 -23.17725 -8.67319 -0.75832 1.11190 -24.18844 -25.19963 -8.67319 -0.75832 1.11190 -26.21083 -27.22202 -8.67319 -0.75832 1.11190 -15.49042 -16.55125 -7.36000 0.00000 0.50000 -17.61208 -18.67292 -7.36000 0.00000 0.50000 -19.73375 -20.79458 -7.36000 0.00000 0.50000 -21.85542 -22.91625 -7.36000 0.00000 0.50000 -23.97708 -25.03792 -7.36000 0.00000 0.50000 -26.09875 -27.15958 -7.36000 0.00000 0.50000 -15.48730 -16.54190 -6.02346 0.00000 0.83654 -17.59650 -18.65109 -6.02346 0.00000 0.83654 -19.70569 -20.76029 -6.02346 0.00000 0.83654 -21.81489 -22.86949 -6.02346 0.00000 0.83654 -23.92408 -24.97868 -6.02346 0.00000 0.83654 -26.03328 -27.08788 -6.02346 0.00000 0.83654 -15.44074 -16.40222 -4.76846 0.00000 0.41846 -17.36370 -18.32518 -4.76846 0.00000 0.41846 -19.28666 -20.24814 -4.76846 0.00000 0.41846 -21.20962 -22.17110 -4.76846 0.00000 0.41846 -23.13258 -24.09406 -4.76846 0.00000 0.41846 -25.05555 -26.01703 -4.76846 0.00000 0.41846 -15.41594 -16.32782 -4.10000 0.00000 0.25000 -17.23971 -18.15159 -4.10000 0.00000 0.25000 -19.06347 -19.97536 -4.10000 0.00000 0.25000 -20.88724 -21.79912 -4.10000 0.00000 0.25000 -22.71100 -23.62289 -4.10000 0.00000 0.25000 -24.53477 -25.44665 -4.10000 0.00000 0.25000 -15.43854 -16.39561 -3.01346 0.00000 0.83654 -17.35267 -18.30974 -3.01346 0.00000 0.83654 -19.26681 -20.22388 -3.01346 0.00000 0.83654 -21.18095 -22.13802 -3.01346 0.00000 0.83654 -23.09509 -24.05216 -3.01346 0.00000 0.83654 -25.00923 -25.96630 -3.01346 0.00000 0.83654 -15.51187 -16.61560 -1.08846 0.00000 1.08846 -17.71934 -18.82308 -1.08846 0.00000 1.08846 -19.92681 -21.03055 -1.08846 0.00000 1.08846 -22.13429 -23.23802 -1.08846 0.00000 1.08846 -24.34176 -25.44550 -1.08846 0.00000 1.08846 -26.54923 -27.65297 -1.08846 0.00000 1.08846 x c/4 dihedral local delta sweep angle alpha cp at angle in rad cl= 0.61276 37.51921 0.00000 0.00000 1.93466 -0.18004 25.99276 0.00000 0.00000 0.80132 -0.97284 11.71110 0.00000 0.00000 0.44417 -1.76564 -4.17472 0.00000 0.00000 0.26877 -2.55845 -19.45708 0.00000 0.00000 0.16716 -3.35125 -32.35670 0.00000 0.00000 0.09160 1.89745 37.51921 0.00000 0.00000 1.76990 0.63571 25.99275 0.00000 0.00000 0.76368 -0.62603 11.71110 0.00000 0.00000 0.45451 -1.88776 -4.17472 0.00000 0.00000 0.28471 -3.14950 -19.45708 0.00000 0.00000 0.17716 -4.41124 -32.35670 0.00000 0.00000 0.09637 3.11717 37.51921 0.00000 0.00000 1.61448 1.41021 25.99276 0.00000 0.00000 0.70163 -0.29675 11.71110 0.00000 0.00000 0.42928 -2.00371 -4.17472 0.00000 0.00000 0.27496 -3.71067 -19.45708 0.00000 0.00000 0.17320 -5.41763 -32.35670 0.00000 0.00000 0.09524 4.33688 37.51921 0.00000 0.00000 1.47893 2.18470 25.99276 0.00000 0.00000 0.65076 0.03253 11.71110 0.00000 0.00000 0.40415 -2.11965 -4.17472 0.00000 0.00000 0.26327 -4.27183 -19.45708 0.00000 0.00000 0.16857 -6.42401 -32.35670 0.00000 0.00000 0.09444 5.62157 37.51921 0.00000 0.00000 1.35651 3.00046 25.99275 0.00000 0.00000 0.60063 0.37934 11.71110 0.00000 0.00000 0.37829 -2.24177 -4.17472 0.00000 0.00000 0.25096 -4.86289 -19.45708 0.00000 0.00000 0.16475 -7.48401 -32.35670 0.00000 0.00000 0.09603 6.90626 37.51921 0.00000 0.00000 1.25084 3.81621 25.99275 0.00000 0.00000 0.55670 0.72616 11.71110 0.00000 0.00000 0.35540 -2.36390 -4.17472 0.00000 0.00000 0.24065 -5.45395 -19.45708 0.00000 0.00000 0.16334 -8.54400 -32.35670 0.00000 0.00000 0.10177 7.99810 37.51921 0.00000 0.00000 1.17259 4.50950 25.99275 0.00000 0.00000 0.52388 1.02091 11.71110 0.00000 0.00000 0.33913 -2.46768 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-2.01311 21.00937 0.00000 0.00000 0.23344 -6.72107 13.73368 0.00000 0.00000 0.17482 -11.42903 5.97943 0.00000 0.00000 0.20034 13.11855 38.76506 0.00000 0.00000 0.88945 8.23532 33.55879 0.00000 0.00000 0.42661 3.35210 27.64136 0.00000 0.00000 0.33185 -1.53113 21.00937 0.00000 0.00000 0.23456 -6.41435 13.73368 0.00000 0.00000 0.15684 -11.29758 5.97943 0.00000 0.00000 0.21695 21.98959 73.23754 0.00000 0.00000 0.21302 15.56357 69.96743 0.00000 0.00000 0.38221 9.13756 65.21040 0.00000 0.00000 0.38601 2.71154 57.79776 0.00000 0.00000 0.29039 -3.71447 45.29755 0.00000 0.00000 0.25414 -10.14049 23.41484 0.00000 0.00000 0.19888 25.59691 73.23754 0.00000 0.00000 0.28844 18.54354 69.96743 0.00000 0.00000 0.19152 11.49016 65.21040 0.00000 0.00000 0.36631 4.43679 57.79776 0.00000 0.00000 0.30348 -2.61659 45.29755 0.00000 0.00000 0.23120 -9.66997 23.41484 0.00000 0.00000 0.20109 31.98795 73.23754 0.00000 0.00000 0.21732 23.82309 69.96743 0.00000 0.00000 0.16858 15.65823 65.21040 0.00000 0.00000 0.25630 7.49337 57.79776 0.00000 0.00000 0.30933 -0.67149 45.29755 0.00000 0.00000 0.23234 -8.83636 23.41482 0.00000 0.00000 0.19074 second planform horseshoe vortex descriptions -21.66854 35.47837 43.00000 0.17450 2.07234 -22.24848 24.15973 43.00000 0.17450 0.86344 -22.82842 10.44929 43.00000 0.17450 0.50181 -23.40836 -4.55831 43.00000 0.17450 0.31432 -23.98830 -18.97688 43.00000 0.17450 0.19781 -24.56824 -31.30072 43.00000 0.17450 0.10867 -20.79644 35.47836 43.00000 0.17450 1.86622 -21.69960 24.15975 43.00000 0.17450 0.79905 -22.60276 10.44927 43.00000 0.17450 0.48369 -23.50591 -4.55835 43.00000 0.17450 0.31020 -24.40907 -18.97688 43.00000 0.17450 0.19537 -25.31223 -31.30072 43.00000 0.17450 0.10614 -19.92434 35.47837 43.00000 0.17450 1.62276 -21.15072 24.15975 43.00000 0.17450 0.69665 -22.37709 10.44928 43.00000 0.17450 0.42654 -23.60347 -4.55832 43.00000 0.17450 0.27531 -24.82984 -18.97687 43.00000 0.17450 0.17295 -26.05622 -31.30070 43.00000 0.17450 0.09307 -19.05225 35.47837 43.00000 0.17450 1.39650 -20.60184 24.15974 43.00000 0.17450 0.60027 -22.15143 10.44929 43.00000 0.17450 0.36950 -23.70102 -4.55834 43.00000 0.17450 0.23890 -25.25062 -18.97689 43.00000 0.17450 0.14921 -26.80021 -31.30070 43.00000 0.17450 0.07915 -18.15451 35.47837 43.00000 0.17450 1.17860 -20.03682 24.15975 43.00000 0.17450 0.50846 -21.91913 10.44929 43.00000 0.17450 0.31541 -23.80145 -4.55835 43.00000 0.17450 0.20462 -25.68376 -18.97689 43.00000 0.17450 0.12671 -27.56607 -31.30071 43.00000 0.17450 0.06503 -17.21404 38.04567 43.00000 0.17450 1.01268 -19.25814 38.58307 43.00000 0.17450 0.44608 -21.30224 39.11254 43.00000 0.17450 0.28734 -23.34634 39.63417 43.00000 0.17450 0.19345 -25.39045 40.14806 43.00000 0.17450 0.12395 -27.43455 40.65429 43.00000 0.17450 0.06535 -16.09888 38.04567 43.00000 0.17450 0.83667 -18.12127 38.58307 43.00000 0.17450 0.39566 -20.14366 39.11254 43.00000 0.17450 0.27313 -22.16605 39.63417 43.00000 0.17450 0.19673 -24.18844 40.14806 43.00000 0.17450 0.13605 -26.21083 40.65429 43.00000 0.17450 0.07985 -15.49042 -3.19570 0.00000 0.00000 0.56637 -17.61208 -15.59796 0.00000 0.00000 0.42340 -19.73375 -26.67953 0.00000 0.00000 0.31785 -21.85542 -35.97340 0.00000 0.00000 0.23703 -23.97708 -43.50610 0.00000 0.00000 0.16547 -26.09875 -49.53985 0.00000 0.00000 0.09394 -15.48730 2.12462 0.00000 0.00000 0.38372 -17.59650 10.50852 0.00000 0.00000 0.33354 -19.70569 18.46350 0.00000 0.00000 0.27610 -21.81489 25.74715 0.00000 0.00000 0.21449 -23.92408 32.23863 0.00000 0.00000 0.15167 -26.03328 37.92108 0.00000 0.00000 0.08438 -15.44074 2.12462 0.00000 0.00000 0.34990 -17.36370 10.50851 0.00000 0.00000 0.29853 -19.28666 18.46349 0.00000 0.00000 0.25906 -21.20962 25.74714 0.00000 0.00000 0.21134 -23.13258 32.23862 0.00000 0.00000 0.15849 -25.05555 37.92108 0.00000 0.00000 0.09723 -15.41594 2.12462 0.00000 0.00000 0.35024 -17.23971 10.50852 0.00000 0.00000 0.28116 -19.06347 18.46350 0.00000 0.00000 0.24782 -20.88724 25.74714 0.00000 0.00000 0.20712 -22.71100 32.23864 0.00000 0.00000 0.16006 -24.53477 37.92108 0.00000 0.00000 0.10421 -15.43854 -2.18164 0.00000 0.00000 0.32319 -17.35267 -10.78430 0.00000 0.00000 0.24905 -19.26681 -18.92465 0.00000 0.00000 0.22019 -21.18095 -26.34637 0.00000 0.00000 0.18542 -23.09509 -32.92787 0.00000 0.00000 0.14319 -25.00923 -38.65982 0.00000 0.00000 0.09029 -15.51187 -2.18164 0.00000 0.00000 0.29260 -17.71934 -10.78430 0.00000 0.00000 0.22016 -19.92681 -18.92465 0.00000 0.00000 0.19116 -22.13429 -26.34637 0.00000 0.00000 0.15602 -24.34176 -32.92787 0.00000 0.00000 0.11287 -26.54923 -38.65981 0.00000 0.00000 0.06313 ref. chord c average true area reference area 26.89170 31.36179 1364.23767 950.00000 b/2 ref. ar true ar mach number 21.75000 1.99184 1.38704 0.30000 complete configuration lift induced drag(far field solution) cl computed alpha cl(wb) cdi at cl(wb) cdi/(cl(wb)**2) 0.5300 7.6834 0.3851 0.0238 0.1608 complete configuration characteristics cl alpha cl(twist) alpha y cp cm/cl cmo per rad per deg at cl=0 3.11731 0.05441 0.11197 -2.05798 -0.42053 0.06834 -0.07080 additional loading with cl based on s(true) -at cl des- load add. basic span x loc dueto load load load of stat 2y/b sl cl c twist at cl at cl at cl local coef ratio ratio = = desir cent of 0.112 0 press 1 -0.962 0.310 2.045 0.152 0.003 0.024 -0.021 0.094 -0.162 2 -0.885 0.471 1.950 0.241 0.006 0.037 -0.031 0.143 0.575 3 -0.812 0.588 1.802 0.327 0.008 0.046 -0.038 0.179 1.273 4 -0.739 0.687 1.669 0.412 0.010 0.054 -0.044 0.210 1.949 5 -0.662 0.775 1.545 0.501 0.012 0.060 -0.048 0.238 2.630 6 -0.585 0.850 1.438 0.591 0.016 0.066 -0.051 0.263 3.257 7 -0.519 0.909 1.362 0.667 0.019 0.071 -0.052 0.284 3.709 8 -0.454 0.963 1.295 0.744 0.023 0.075 -0.052 0.303 4.081 9 -0.388 1.011 1.233 0.820 0.028 0.079 -0.051 0.322 4.316 10 -0.338 1.046 1.209 0.865 0.031 0.082 -0.050 0.336 4.526 11 -0.277 1.075 1.193 0.901 0.033 0.084 -0.051 0.346 5.045 12 -0.219 1.092 1.168 0.934 0.034 0.085 -0.052 0.351 5.530 13 -0.189 1.100 0.895 1.229 0.033 0.086 -0.053 0.353 6.950 14 -0.139 1.109 0.822 1.349 0.033 0.086 -0.053 0.356 8.812 15 -0.050 1.117 0.715 1.562 0.033 0.087 -0.054 0.358 11.245 contribution of the second planform to span load distribution 16 -0.749 0.116 1.047 0.111 0.041 0.009 0.032 0.075 -22.261 17 -0.693 0.164 0.948 0.173 0.061 0.013 0.048 0.108 -21.759 18 -0.636 0.189 0.806 0.235 0.073 0.015 0.059 0.129 -21.242 19 -0.580 0.200 0.676 0.296 0.082 0.016 0.066 0.140 -20.719 20 -0.522 0.200 0.555 0.360 0.086 0.016 0.070 0.144 -20.183 21 -0.464 0.187 0.479 0.391 0.084 0.015 0.070 0.139 -19.541 22 -0.399 0.164 0.423 0.387 0.076 0.013 0.063 0.124 -18.709 23 -0.338 0.174 0.429 0.406 0.071 0.014 0.058 0.122 -18.903 24 -0.277 0.148 0.366 0.404 0.054 0.012 0.043 0.097 -19.224 25 -0.219 0.133 0.363 0.368 0.045 0.010 0.035 0.084 -19.037 26 -0.189 0.128 0.366 0.349 0.041 0.010 0.031 0.079 -18.872 27 -0.139 0.124 0.339 0.366 0.038 0.010 0.028 0.074 -19.025 28 -0.050 0.126 0.297 0.422 0.036 0.010 0.027 0.073 -19.428 induced drag,leading edge thrust , 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 1 -0.96154 39.96069 0.00412 0.00085 0.00111 2 -0.88462 39.96069 0.00182 0.00507 0.00661 3 -0.81158 39.96069 0.00042 0.00821 0.01071 4 -0.73855 39.96069 0.00101 0.00912 0.01190 5 -0.66163 39.96069 0.00187 0.00962 0.01255 6 -0.58470 39.96069 0.00286 0.00985 0.01285 7 -0.51933 39.96069 0.00392 0.00978 0.01276 8 -0.45395 39.96069 0.00499 0.00967 0.01261 9 -0.38844 39.96069 0.00581 0.00975 0.01272 10 -0.33839 39.96069 0.00675 0.00940 0.01226 11 -0.27694 39.96069 0.00795 0.00872 0.01138 12 -0.21924 39.96069 0.00884 0.00813 0.01389 13 -0.18851 73.89906 0.00974 0.00733 0.02002 14 -0.13855 73.89906 0.01161 0.00557 0.02009 15 -0.05004 73.89906 0.02071 -0.00342 -0.01233 contribution of the second planform to the chord or drag force 16 -0.74888 37.91007 0.00645 0.00292 0.00370 17 -0.69262 37.91007 0.00477 0.00715 0.00906 18 -0.63637 37.91007 0.00430 0.00984 0.01247 19 -0.58011 37.91007 0.00588 0.00953 0.01208 20 -0.52220 37.91007 0.00755 0.00832 0.01054 21 -0.46428 37.91007 0.00901 0.00640 0.00812 22 -0.39877 37.91007 0.00956 0.00324 0.00400 23 -0.33839 0.00000 0.00665 0.00124 0.00128 24 -0.27694 0.00000 0.00449 0.00034 0.00034 25 -0.21924 0.00000 0.00408 0.00003 0.00003 26 -0.18851 0.00000 0.00389 -0.00001 -0.00001 27 -0.13855 0.00000 0.00361 0.00002 0.00002 28 -0.05004 0.00000 0.00331 0.00022 0.00022 total coefficients cdii/cl**2= 0.15439 ct= 0.04177 cs= 0.05673 1 end of file encountered after configuration 23.