vortex lattice aerodynamic computation program nasa-lrc no. a2794 by j.e. lamar and b.b. gloss modified for watfor77 with 72 column output 767 data - no engine geometry data first reference planform has 10 curves center of gravity = -26.64000 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 0.00000 0.00000 57.35474 0.00000 1 2 -1.24875 -0.80000 71.70327 0.00000 1 3 -6.38250 -2.49750 90.00000 0.00000 1 4 -19.42500 -2.49750 34.99202 6.00000 1 5 -24.28125 -9.43500 35.59078 6.00000 1 6 -34.41000 -23.58750 90.00000 0.00000 1 7 -36.35250 -23.58750 20.43283 6.00000 1 8 -31.08000 -9.43500 13.49572 6.00000 1 9 -29.41500 -2.49750 90.00000 0.00000 1 10 -47.73000 -2.49750 0.00000 0.00000 1 11 -47.73000 0.00000 second reference planform has 5 curves center of gravity = -26.64000 root chord height = -1.66500 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 -47.73000 0.00000 0.00000 0.00000 1 2 -47.73000 -2.49750 38.65980 6.00000 1 3 -53.28000 -9.43500 90.00000 0.00000 1 4 -54.94500 -9.43500 15.33328 6.00000 1 5 -52.58625 -0.83250 -61.38952 0.00000 1 6 -54.11250 0.00000 1 configuration no. 767. curve 1 is swept 57.35474 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 0.00000 0.00000 0.00000 57.35474 0.00000 1 2 -1.24875 -0.80000 0.00000 71.70327 0.00000 1 3 -1.34704 -0.83250 0.00000 71.70327 0.00000 1 4 -6.38250 -2.49750 0.00000 90.00000 0.00000 1 5 -19.42500 -2.49750 0.00000 34.99202 6.00000 1 6 -24.28125 -9.43500 -0.72916 35.59078 6.00000 1 7 -34.41000 -23.58750 -2.21665 90.00000 0.00000 1 8 -36.35250 -23.58750 -2.21665 20.43283 6.00000 1 9 -31.08000 -9.43500 -0.72916 13.49572 6.00000 1 10 -29.41500 -2.49750 0.00000 90.00000 0.00000 1 11 -47.73000 -2.49750 0.00000 0.00000 0.00000 1 12 -47.73000 0.00000 0.00000 second planform breakpoints 1 -47.73000 0.00000 -1.66500 0.00000 0.00000 1 2 -47.73000 -0.80000 -1.66500 0.00000 0.00000 1 3 -47.73000 -2.49750 -1.66500 38.65980 6.00000 1 4 -53.28000 -9.43500 -2.39416 90.00000 0.00000 1 5 -54.94500 -9.43500 -2.56916 15.33328 6.00000 1 6 -52.58625 -0.83250 -1.66500 -61.38952 0.00000 1 7 -54.11250 0.00000 -1.66500 180 horseshoe vortices used on the left half of the configuration planform total spanwise 1 126 21 2 54 9 6. horseshoe vortices in each chordwise row 1 aerodynamic data configuration no. 767. static longitudinal aerodynamic coefficients are computed x x y z s c/4 3c/4 -34.07758 -34.25630 -22.99815 -2.15471 0.59259 -34.43503 -34.61376 -22.99815 -2.15471 0.59259 -34.79249 -34.97121 -22.99815 -2.15471 0.59259 -35.14994 -35.32867 -22.99815 -2.15471 0.59259 -35.50740 -35.68612 -22.99815 -2.15471 0.59259 -35.86485 -36.04358 -22.99815 -2.15471 0.59259 -33.25086 -33.46329 -21.81947 -2.03082 0.59259 -33.67572 -33.88815 -21.81947 -2.03082 0.59259 -34.10058 -34.31302 -21.81947 -2.03082 0.59259 -34.52545 -34.73788 -21.81947 -2.03082 0.59259 -34.95031 -35.16274 -21.81947 -2.03082 0.59259 -35.37517 -35.58761 -21.81947 -2.03082 0.59259 -32.42414 -32.67027 -20.64077 -1.90693 0.59259 -32.91641 -33.16254 -20.64077 -1.90693 0.59259 -33.40868 -33.65482 -20.64077 -1.90693 0.59259 -33.90095 -34.14709 -20.64077 -1.90693 0.59259 -34.39322 -34.63936 -20.64077 -1.90693 0.59259 -34.88550 -35.13163 -20.64077 -1.90693 0.59259 -31.59742 -31.87726 -19.46209 -1.78305 0.59259 -32.15710 -32.43694 -19.46209 -1.78305 0.59259 -32.71678 -32.99662 -19.46209 -1.78305 0.59259 -33.27646 -33.55630 -19.46209 -1.78305 0.59259 -33.83614 -34.11598 -19.46209 -1.78305 0.59259 -34.39582 -34.67566 -19.46209 -1.78305 0.59259 -30.77070 -31.08424 -18.28339 -1.65916 0.59259 -31.39779 -31.71133 -18.28339 -1.65916 0.59259 -32.02488 -32.33842 -18.28339 -1.65916 0.59259 -32.65196 -32.96551 -18.28339 -1.65916 0.59259 -33.27905 -33.59260 -18.28339 -1.65916 0.59259 -33.90614 -34.21969 -18.28339 -1.65916 0.59259 -29.94398 -30.29123 -17.10471 -1.53528 0.59259 -30.63848 -30.98572 -17.10471 -1.53528 0.59259 -31.33297 -31.68022 -17.10471 -1.53528 0.59259 -32.02747 -32.37472 -17.10471 -1.53528 0.59259 -32.72197 -33.06922 -17.10471 -1.53528 0.59259 -33.41647 -33.76372 -17.10471 -1.53528 0.59259 -29.11726 -29.49821 -15.92601 -1.41139 0.59259 -29.87916 -30.26012 -15.92601 -1.41139 0.59259 -30.64107 -31.02202 -15.92601 -1.41139 0.59259 -31.40298 -31.78393 -15.92601 -1.41139 0.59259 -32.16488 -32.54584 -15.92601 -1.41139 0.59259 -32.92679 -33.30774 -15.92601 -1.41139 0.59259 -28.29054 -28.70519 -14.74732 -1.28751 0.59259 -29.11985 -29.53451 -14.74732 -1.28751 0.59259 -29.94917 -30.36383 -14.74732 -1.28751 0.59259 -30.77848 -31.19314 -14.74732 -1.28751 0.59259 -31.60780 -32.02246 -14.74732 -1.28751 0.59259 -32.43711 -32.85177 -14.74732 -1.28751 0.59259 -27.46381 -27.91218 -13.56863 -1.16362 0.59259 -28.36054 -28.80890 -13.56863 -1.16362 0.59259 -29.25726 -29.70563 -13.56863 -1.16362 0.59259 -30.15399 -30.60235 -13.56863 -1.16362 0.59259 -31.05071 -31.49908 -13.56863 -1.16362 0.59259 -31.94744 -32.39580 -13.56863 -1.16362 0.59259 -26.63709 -27.11916 -12.38994 -1.03974 0.59259 -27.60123 -28.08329 -12.38994 -1.03974 0.59259 -28.56536 -29.04743 -12.38994 -1.03974 0.59259 -29.52949 -30.01156 -12.38994 -1.03974 0.59259 -30.49363 -30.97569 -12.38994 -1.03974 0.59259 -31.45776 -31.93983 -12.38994 -1.03974 0.59259 -25.81037 -26.32614 -11.21125 -0.91585 0.59259 -26.84192 -27.35769 -11.21125 -0.91585 0.59259 -27.87346 -28.38923 -11.21125 -0.91585 0.59259 -28.90500 -29.42077 -11.21125 -0.91585 0.59259 -29.93654 -30.45231 -11.21125 -0.91585 0.59259 -30.96808 -31.48385 -11.21125 -0.91585 0.59259 -24.98077 -25.53036 -10.02845 -0.79154 0.59672 -26.07996 -26.62955 -10.02845 -0.79154 0.59672 -27.17914 -27.72874 -10.02845 -0.79154 0.59672 -28.27833 -28.82792 -10.02845 -0.79154 0.59672 -29.37752 -29.92711 -10.02845 -0.79154 0.59672 -30.47670 -31.02629 -10.02845 -0.79154 0.59672 -24.16329 -24.75244 -8.84566 -0.66722 0.59259 -25.34159 -25.93075 -8.84566 -0.66722 0.59259 -26.51990 -27.10906 -8.84566 -0.66722 0.59259 -27.69821 -28.28736 -8.84566 -0.66722 0.59259 -28.87652 -29.46567 -8.84566 -0.66722 0.59259 -30.05483 -30.64398 -8.84566 -0.66722 0.59259 -23.36079 -23.99513 -7.66696 -0.54333 0.59259 -24.62947 -25.26380 -7.66696 -0.54333 0.59259 -25.89814 -26.53248 -7.66696 -0.54333 0.59259 -27.16682 -27.80115 -7.66696 -0.54333 0.59259 -28.43549 -29.06983 -7.66696 -0.54333 0.59259 -29.70417 -30.33850 -7.66696 -0.54333 0.59259 -22.55830 -23.23782 -6.48827 -0.41945 0.59259 -23.91734 -24.59686 -6.48827 -0.41945 0.59259 -25.27638 -25.95590 -6.48827 -0.41945 0.59259 -26.63542 -27.31494 -6.48827 -0.41945 0.59259 -27.99446 -28.67398 -6.48827 -0.41945 0.59259 -29.35351 -30.03303 -6.48827 -0.41945 0.59259 -21.75581 -22.48051 -5.30958 -0.29556 0.59259 -23.20522 -23.92992 -5.30958 -0.29556 0.59259 -24.65462 -25.37933 -5.30958 -0.29556 0.59259 -26.10403 -26.82873 -5.30958 -0.29556 0.59259 -27.55344 -28.27814 -5.30958 -0.29556 0.59259 -29.00284 -29.72755 -5.30958 -0.29556 0.59259 -20.95332 -21.72320 -4.13089 -0.17168 0.59259 -22.49309 -23.26298 -4.13089 -0.17168 0.59259 -24.03286 -24.80275 -4.13089 -0.17168 0.59259 -25.57264 -26.34252 -4.13089 -0.17168 0.59259 -27.11241 -27.88230 -4.13089 -0.17168 0.59259 -28.65218 -29.42207 -4.13089 -0.17168 0.59259 -20.19666 -21.00915 -3.01952 -0.05487 0.52490 -21.82164 -22.63413 -3.01952 -0.05487 0.52490 -23.44662 -24.25911 -3.01952 -0.05487 0.52490 -25.07160 -25.88408 -3.01952 -0.05487 0.52490 -26.69657 -27.50906 -3.01952 -0.05487 0.52490 -28.32155 -29.13404 -3.01952 -0.05487 0.52490 -5.69249 -9.34792 -1.66500 0.00000 0.83250 -13.00336 -16.65879 -1.66500 0.00000 0.83250 -20.31423 -23.96967 -1.66500 0.00000 0.83250 -27.62510 -31.28054 -1.66500 0.00000 0.83250 -34.93597 -38.59141 -1.66500 0.00000 0.83250 -42.24684 -45.90228 -1.66500 0.00000 0.83250 -3.23257 -7.10191 -0.81625 0.00000 0.01625 -10.97125 -14.84059 -0.81625 0.00000 0.01625 -18.70993 -22.57928 -0.81625 0.00000 0.01625 -26.44862 -30.31796 -0.81625 0.00000 0.01625 -34.18730 -38.05665 -0.81625 0.00000 0.01625 -41.92599 -45.79533 -0.81625 0.00000 0.01625 -2.58711 -6.51258 -0.40000 0.00000 0.40000 -10.43805 -14.36351 -0.40000 0.00000 0.40000 -18.28898 -22.21445 -0.40000 0.00000 0.40000 -26.13992 -30.06539 -0.40000 0.00000 0.40000 -33.99086 -37.91633 -0.40000 0.00000 0.40000 -41.84179 -45.76726 -0.40000 0.00000 0.40000 second planform horseshoe vortex descriptions -52.89081 -53.05538 -8.84566 -2.33222 0.59259 -53.21996 -53.38453 -8.84566 -2.33222 0.59259 -53.54910 -53.71368 -8.84566 -2.33222 0.59259 -53.87825 -54.04282 -8.84566 -2.33222 0.59259 -54.20740 -54.37197 -8.84566 -2.33222 0.59259 -54.53654 -54.70112 -8.84566 -2.33222 0.59259 -51.97368 -52.18990 -7.66696 -2.20833 0.59259 -52.40612 -52.62234 -7.66696 -2.20833 0.59259 -52.83856 -53.05478 -7.66696 -2.20833 0.59259 -53.27100 -53.48722 -7.66696 -2.20833 0.59259 -53.70345 -53.91967 -7.66696 -2.20833 0.59259 -54.13589 -54.35211 -7.66696 -2.20833 0.59259 -51.05655 -51.32442 -6.48827 -2.08445 0.59259 -51.59229 -51.86015 -6.48827 -2.08445 0.59259 -52.12802 -52.39589 -6.48827 -2.08445 0.59259 -52.66376 -52.93163 -6.48827 -2.08445 0.59259 -53.19949 -53.46736 -6.48827 -2.08445 0.59259 -53.73523 -54.00309 -6.48827 -2.08445 0.59259 -50.13942 -50.45894 -5.30958 -1.96056 0.59259 -50.77845 -51.09797 -5.30958 -1.96056 0.59259 -51.41748 -51.73699 -5.30958 -1.96056 0.59259 -52.05651 -52.37602 -5.30958 -1.96056 0.59259 -52.69554 -53.01505 -5.30958 -1.96056 0.59259 -53.33457 -53.65408 -5.30958 -1.96056 0.59259 -49.22229 -49.59345 -4.13089 -1.83668 0.59259 -49.96461 -50.33578 -4.13089 -1.83668 0.59259 -50.70694 -51.07810 -4.13089 -1.83668 0.59259 -51.44926 -51.82042 -4.13089 -1.83668 0.59259 -52.19158 -52.56274 -4.13089 -1.83668 0.59259 -52.93391 -53.30507 -4.13089 -1.83668 0.59259 -48.35755 -48.77741 -3.01952 -1.71987 0.52490 -49.19726 -49.61712 -3.01952 -1.71987 0.52490 -50.03698 -50.45684 -3.01952 -1.71987 0.52490 -50.87670 -51.29655 -3.01952 -1.71987 0.52490 -51.71641 -52.13627 -3.01952 -1.71987 0.52490 -52.55613 -52.97599 -3.01952 -1.71987 0.52490 -47.94185 -48.36556 -1.66500 -1.66500 0.83250 -48.78927 -49.21298 -1.66500 -1.66500 0.83250 -49.63669 -50.06040 -1.66500 -1.66500 0.83250 -50.48411 -50.90782 -1.66500 -1.66500 0.83250 -51.33153 -51.75524 -1.66500 -1.66500 0.83250 -52.17895 -52.60266 -1.66500 -1.66500 0.83250 -47.93358 -48.34076 -0.81625 -1.66500 0.01625 -48.74793 -49.15509 -0.81625 -1.66500 0.01625 -49.56226 -49.96944 -0.81625 -1.66500 0.01625 -50.37661 -50.78378 -0.81625 -1.66500 0.01625 -51.19094 -51.59812 -0.81625 -1.66500 0.01625 -52.00529 -52.41246 -0.81625 -1.66500 0.01625 -47.96538 -48.43615 -0.40000 -1.66500 0.40000 -48.90691 -49.37767 -0.40000 -1.66500 0.40000 -49.84843 -50.31920 -0.40000 -1.66500 0.40000 -50.78996 -51.26073 -0.40000 -1.66500 0.40000 -51.73149 -52.20226 -0.40000 -1.66500 0.40000 -52.67302 -53.14378 -0.40000 -1.66500 0.40000 x c/4 dihedral local delta sweep angle alpha cp at angle in rad cl= -34.07758 35.04539 6.00000 0.00000 3.04883 -34.43503 32.78961 6.00000 0.00000 1.23676 -34.79249 30.41335 6.00000 0.00000 0.67195 -35.14994 27.91555 6.00000 0.00000 0.38815 -35.50740 25.29686 6.00000 0.00000 0.22502 -35.86485 22.56001 6.00000 0.00000 0.11547 -33.25086 35.04539 6.00000 0.00000 3.21330 -33.67572 32.78961 6.00000 0.00000 1.43675 -34.10058 30.41335 6.00000 0.00000 0.90693 -34.52545 27.91555 6.00000 0.00000 0.59833 -34.95031 25.29686 6.00000 0.00000 0.38024 -35.37517 22.56001 6.00000 0.00000 0.20657 -32.42414 35.04539 6.00000 0.00000 3.17813 -32.91641 32.78961 6.00000 0.00000 1.44949 -33.40868 30.41335 6.00000 0.00000 0.94958 -33.90095 27.91555 6.00000 0.00000 0.65841 -34.39322 25.29686 6.00000 0.00000 0.44198 -34.88550 22.56002 6.00000 0.00000 0.25239 -31.59742 35.04539 6.00000 0.00000 3.09981 -32.15710 32.78961 6.00000 0.00000 1.42301 -32.71678 30.41335 6.00000 0.00000 0.94510 -33.27646 27.91555 6.00000 0.00000 0.66796 -33.83614 25.29686 6.00000 0.00000 0.45930 -34.39582 22.56001 6.00000 0.00000 0.26922 -30.77070 35.04539 6.00000 0.00000 3.00996 -31.39779 32.78961 6.00000 0.00000 1.38565 -32.02488 30.41335 6.00000 0.00000 0.92648 -32.65196 27.91555 6.00000 0.00000 0.66076 -33.27905 25.29686 6.00000 0.00000 0.45969 -33.90614 22.56002 6.00000 0.00000 0.27309 -29.94398 35.04539 6.00000 0.00000 2.91747 -30.63848 32.78961 6.00000 0.00000 1.34541 -31.33297 30.41335 6.00000 0.00000 0.90328 -32.02747 27.91555 6.00000 0.00000 0.64762 -32.72197 25.29686 6.00000 0.00000 0.45352 -33.41647 22.56001 6.00000 0.00000 0.27147 -29.11726 35.04539 6.00000 0.00000 2.82498 -29.87916 32.78961 6.00000 0.00000 1.30490 -30.64107 30.41335 6.00000 0.00000 0.87890 -31.40298 27.91555 6.00000 0.00000 0.63251 -32.16488 25.29686 6.00000 0.00000 0.44487 -32.92679 22.56001 6.00000 0.00000 0.26758 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22.56001 6.00000 0.00000 0.25200 -24.98077 35.04539 6.00000 0.00000 2.35781 -26.07996 32.78961 6.00000 0.00000 1.10855 -27.17914 30.41335 6.00000 0.00000 0.76541 -28.27833 27.91555 6.00000 0.00000 0.56680 -29.37752 25.29686 6.00000 0.00000 0.41056 -30.47670 22.56001 6.00000 0.00000 0.25369 -24.16329 34.24834 6.00000 0.00000 2.25427 -25.34159 31.13897 6.00000 0.00000 1.05860 -26.51990 27.81165 6.00000 0.00000 0.73571 -27.69821 24.26744 6.00000 0.00000 0.55112 -28.87652 20.51417 6.00000 0.00000 0.40447 -30.05483 16.56774 6.00000 0.00000 0.25301 -23.36079 34.24834 6.00000 0.00000 2.14499 -24.62947 31.13897 6.00000 0.00000 1.00166 -25.89814 27.81165 6.00000 0.00000 0.69779 -27.16682 24.26744 6.00000 0.00000 0.53018 -28.43549 20.51417 6.00000 0.00000 0.39648 -29.70417 16.56774 6.00000 0.00000 0.25005 -22.55830 34.24834 6.00000 0.00000 2.04237 -23.91734 31.13897 6.00000 0.00000 0.94356 -25.27638 27.81165 6.00000 0.00000 0.65461 -26.63542 24.26744 6.00000 0.00000 0.50718 -27.99446 20.51417 6.00000 0.00000 0.39437 -29.35351 16.56774 6.00000 0.00000 0.25620 -21.75581 34.24834 6.00000 0.00000 1.95107 -23.20522 31.13897 6.00000 0.00000 0.88652 -24.65462 27.81165 6.00000 0.00000 0.59876 -26.10403 24.26744 6.00000 0.00000 0.47388 -27.55344 20.51417 6.00000 0.00000 0.39663 -29.00284 16.56774 6.00000 0.00000 0.28016 -20.95332 34.24834 6.00000 0.00000 1.86472 -22.49309 31.13897 6.00000 0.00000 0.85396 -24.03286 27.81165 6.00000 0.00000 0.51797 -25.57264 24.26744 6.00000 0.00000 0.41436 -27.11241 20.51417 6.00000 0.00000 0.39254 -28.65218 16.56774 6.00000 0.00000 0.34639 -20.19666 34.24834 6.00000 0.00000 1.72780 -21.82164 31.13897 6.00000 0.00000 0.95903 -23.44662 27.81165 6.00000 0.00000 0.38061 -25.07160 24.26744 6.00000 0.00000 0.29779 -26.69657 20.51417 6.00000 0.00000 0.34041 -28.32155 16.56774 6.00000 0.00000 0.52706 -5.69249 70.96396 0.00000 0.00000 0.19446 -13.00336 67.33119 0.00000 0.00000 0.04080 -20.31423 62.11901 0.00000 0.00000 0.45943 -27.62510 54.19222 0.00000 0.00000 0.29682 -34.93597 41.41512 0.00000 0.00000 0.03866 -42.24684 20.70848 0.00000 0.00000 0.01778 -3.23257 70.96396 0.00000 0.00000 0.19127 -10.97125 67.33119 0.00000 0.00000 0.04375 -18.70993 62.11901 0.00000 0.00000 0.40800 -26.44862 54.19222 0.00000 0.00000 0.29449 -34.18730 41.41511 0.00000 0.00000 0.04240 -41.92599 20.70847 0.00000 0.00000 0.01840 -2.58711 56.23750 0.00000 0.00000 0.19545 -10.43805 51.01918 0.00000 0.00000 0.04794 -18.28898 44.29199 0.00000 0.00000 0.37810 -26.13992 35.58107 0.00000 0.00000 0.30330 -33.99086 24.47853 0.00000 0.00000 0.04724 -41.84179 11.04069 0.00000 0.00000 0.01962 second planform horseshoe vortex descriptions -52.89081 37.88617 6.00000 0.00000 1.38331 -53.21996 34.62340 6.00000 0.00000 0.59329 -53.54910 31.08251 6.00000 0.00000 0.34042 -53.87825 27.25699 6.00000 0.00000 0.20285 -54.20740 23.14932 6.00000 0.00000 0.11995 -54.53654 18.77389 6.00000 0.00000 0.06264 -51.97368 37.88617 6.00000 0.00000 1.31110 -52.40612 34.62340 6.00000 0.00000 0.60121 -52.83856 31.08252 6.00000 0.00000 0.38985 -53.27100 27.25698 6.00000 0.00000 0.26418 -53.70345 23.14930 6.00000 0.00000 0.17180 -54.13589 18.77389 6.00000 0.00000 0.09512 -51.05655 37.88617 6.00000 0.00000 1.18282 -51.59229 34.62341 6.00000 0.00000 0.55123 -52.12802 31.08251 6.00000 0.00000 0.36996 -52.66376 27.25698 6.00000 0.00000 0.26242 -53.19949 23.14931 6.00000 0.00000 0.17960 -53.73523 18.77388 6.00000 0.00000 0.10417 -50.13942 37.88617 6.00000 0.00000 1.04736 -50.77845 34.62341 6.00000 0.00000 0.49471 -51.41748 31.08251 6.00000 0.00000 0.33947 -52.05651 27.25698 6.00000 0.00000 0.24689 -52.69554 23.14931 6.00000 0.00000 0.17373 -53.33457 18.77388 6.00000 0.00000 0.10359 -49.22229 37.88617 6.00000 0.00000 0.89728 -49.96461 34.62340 6.00000 0.00000 0.43642 -50.70694 31.08251 6.00000 0.00000 0.30804 -51.44926 27.25698 6.00000 0.00000 0.22937 -52.19158 23.14931 6.00000 0.00000 0.16493 -52.93391 18.77389 6.00000 0.00000 0.10033 -48.35755 37.88618 6.00000 0.00000 0.71317 -49.19726 34.62341 6.00000 0.00000 0.38118 -50.03698 31.08252 6.00000 0.00000 0.28020 -50.87670 27.25699 6.00000 0.00000 0.21393 -51.71641 23.14931 6.00000 0.00000 0.15684 -52.55613 18.77389 6.00000 0.00000 0.09702 -47.94185 0.65456 0.00000 0.00000 0.66794 -48.78927 3.26939 0.00000 0.00000 0.33041 -49.63669 5.87067 0.00000 0.00000 0.24913 -50.48411 8.44790 0.00000 0.00000 0.19629 -51.33153 10.99117 0.00000 0.00000 0.14752 -52.17895 13.49136 0.00000 0.00000 0.09374 -47.93358 -4.36827 0.00000 0.00000 0.71054 -48.74793 -20.90406 0.00000 0.00000 0.34862 -49.56226 -34.50851 0.00000 0.00000 0.25996 -50.37661 -44.80035 0.00000 0.00000 0.19952 -51.19094 -52.40178 0.00000 0.00000 0.13979 -52.00529 -58.06152 0.00000 0.00000 0.07768 -47.96538 -4.36828 0.00000 0.00000 0.63031 -48.90691 -20.90408 0.00000 0.00000 0.30764 -49.84843 -34.50850 0.00000 0.00000 0.22753 -50.78996 -44.80035 0.00000 0.00000 0.16973 -51.73149 -52.40179 0.00000 0.00000 0.10848 -52.67302 -58.06153 0.00000 0.00000 0.04742 ref. chord c average true area reference area 5.95500 11.43268 539.33685 283.29999 b/2 ref. ar true ar mach number 23.58750 7.85556 4.12633 0.80000 complete configuration lift induced drag(far field solution) cl computed alpha cl(wb) cdi at cl(wb) cdi/(cl(wb)**2) -0.1000 -0.8605 -0.0908 0.0003 0.0412 0.1000 0.8605 0.0908 0.0003 0.0412 0.2000 1.7210 0.1816 0.0014 0.0412 0.3000 2.5815 0.2723 0.0031 0.0412 0.4000 3.4420 0.3631 0.0054 0.0412 0.5000 4.3025 0.4539 0.0085 0.0412 0.6000 5.1630 0.5447 0.0122 0.0412 0.7000 6.0235 0.6355 0.0166 0.0412 0.8000 6.8840 0.7262 0.0217 0.0412 0.9000 7.7445 0.8170 0.0275 0.0412 1.0000 8.6050 0.9078 0.0339 0.0412 complete configuration characteristics cl alpha cl(twist) alpha y cp cm/cl cmo per rad per deg at cl=0 6.65845 0.11621 0.00000 0.00000 -0.39957 -0.31637 0.00000 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 0.000 0 press 1 -0.975 0.338 1.804 0.188 0.000 0.000 0.000 0.178 -34.406 2 -0.925 0.477 2.139 0.223 0.000 0.000 0.000 0.251 -33.730 3 -0.875 0.568 2.199 0.258 0.000 0.000 0.000 0.298 -33.018 4 -0.825 0.640 2.178 0.294 0.000 0.000 0.000 0.336 -32.290 5 -0.775 0.701 2.131 0.329 0.000 0.000 0.000 0.368 -31.557 6 -0.725 0.756 2.075 0.364 0.000 0.000 0.000 0.397 -30.822 7 -0.675 0.806 2.016 0.400 0.000 0.000 0.000 0.423 -30.086 8 -0.625 0.852 1.957 0.435 0.000 0.000 0.000 0.447 -29.350 9 -0.575 0.894 1.899 0.471 0.000 0.000 0.000 0.469 -28.616 10 -0.525 0.932 1.842 0.506 0.000 0.000 0.000 0.490 -27.886 11 -0.475 0.967 1.787 0.541 0.000 0.000 0.000 0.508 -27.160 12 -0.425 1.000 1.733 0.577 0.000 0.000 0.000 0.525 -26.440 13 -0.375 1.032 1.668 0.618 0.000 0.000 0.000 0.542 -25.747 14 -0.325 1.061 1.593 0.666 0.000 0.000 0.000 0.557 -25.085 15 -0.275 1.086 1.522 0.713 0.000 0.000 0.000 0.570 -24.437 16 -0.225 1.107 1.455 0.761 0.000 0.000 0.000 0.582 -23.807 17 -0.175 1.126 1.393 0.808 0.000 0.000 0.000 0.591 -23.210 18 -0.128 1.145 1.343 0.853 0.000 0.000 0.000 0.602 -22.735 19 -0.071 1.276 0.333 3.837 0.000 0.000 0.000 0.670 -20.299 20 -0.035 1.286 0.317 4.061 0.000 0.000 0.000 0.676 -18.774 21 -0.017 1.296 0.315 4.120 0.000 0.000 0.000 0.681 -18.430 contribution of the second planform to span load distribution 22 -0.375 0.148 0.857 0.173 0.000 0.000 0.000 0.078 -53.217 23 -0.325 0.204 0.899 0.227 0.000 0.000 0.000 0.107 -52.483 24 -0.275 0.236 0.841 0.281 0.000 0.000 0.000 0.124 -51.727 25 -0.225 0.256 0.763 0.335 0.000 0.000 0.000 0.134 -50.970 26 -0.175 0.264 0.678 0.390 0.000 0.000 0.000 0.139 -50.231 27 -0.128 0.258 0.585 0.441 0.000 0.000 0.000 0.135 -49.586 28 -0.071 0.238 0.535 0.445 0.000 0.000 0.000 0.125 -49.187 29 -0.035 0.235 0.551 0.427 0.000 0.000 0.000 0.124 -49.066 30 -0.017 0.234 0.473 0.494 0.000 0.000 0.000 0.123 -49.192 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 -0.97501 35.59078 -0.00162 0.00481 0.00591 2 -0.92504 35.59078 -0.00140 0.00595 0.00732 3 -0.87507 35.59078 -0.00123 0.00665 0.00817 4 -0.82510 35.59078 -0.00102 0.00713 0.00877 5 -0.77513 35.59078 -0.00079 0.00749 0.00921 6 -0.72516 35.59078 -0.00052 0.00775 0.00953 7 -0.67519 35.59078 -0.00023 0.00793 0.00976 8 -0.62522 35.59078 0.00008 0.00806 0.00991 9 -0.57525 35.59078 0.00042 0.00812 0.00999 10 -0.52528 35.59078 0.00078 0.00812 0.00999 11 -0.47530 35.59078 0.00119 0.00806 0.00991 12 -0.42516 35.59078 0.00163 0.00793 0.00973 13 -0.37501 34.99202 0.00208 0.00778 0.00951 14 -0.32504 34.99202 0.00250 0.00763 0.00931 15 -0.27507 34.99202 0.00288 0.00750 0.00915 16 -0.22510 34.99202 0.00306 0.00752 0.00918 17 -0.17513 34.99202 0.00148 0.00928 0.01133 18 -0.12801 34.99202 0.00784 0.00324 0.00429 19 -0.07059 71.70327 0.00391 0.00826 0.02611 20 -0.03461 71.70327 0.01695 -0.00464 -0.00943 21 -0.01696 57.35474 0.02334 -0.01096 -0.02686 contribution of the second planform to the chord or drag force 22 -0.37501 38.65980 0.00059 0.00089 0.00114 23 -0.32504 38.65980 0.00089 0.00103 0.00132 24 -0.27507 38.65980 0.00119 0.00105 0.00135 25 -0.22510 38.65980 0.00145 0.00098 0.00125 26 -0.17513 38.65980 0.00170 0.00080 0.00103 27 -0.12801 38.65980 0.00190 0.00055 0.00068 28 -0.07059 0.00000 0.00204 0.00023 0.00023 29 -0.03461 0.00000 0.00202 0.00023 0.00023 30 -0.01696 0.00000 0.00200 0.00023 0.00023 total coefficients cdii/cl**2= 0.04190 ct= 0.10779 cs= 0.13793 1 end of file encountered after configuration 767.