enter name of input file: lamdes.inp Lamar Design Code mods by W.H. Mason Lamar program sample input - revised forward swept wing plan = 2.0 xmref = -8.0000 cref = 89.5000 tdklue = 1.0 case = 3.0 spnklu = 0.0 sref = 26640.0000 1st REFERENCE PLANFORM HAS 5 CURVES ROOT CHORD HEIGHT = -8.8000 POINT X Y SWEEP DIHEDRAL REF REF ANGLE ANGLE 1 76.9500 0.0000 0.00000 0.00000 2 76.9500 -34.0000 31.71155 0.00000 3 57.6100 -65.3000 90.00000 0.00000 4 33.6400 -65.3000 -6.18142 0.00000 5 30.2500 -34.0000 0.00000 0.00000 6 30.2500 0.0000 2nd REFERENCE PLANFORM HAS 5 CURVES ROOT CHORD HEIGHT = 0.0000 POINT X Y SWEEP DIHEDRAL REF REF ANGLE ANGLE 1 -17.9000 0.0000 0.00000 0.00000 2 -17.9000 -34.0000 -26.21138 0.00000 3 46.1000-164.0000 90.00000 0.00000 4 5.6000-164.0000 -45.29687 0.00000 5-139.9000 -20.0000 0.00000 0.00000 6-139.9000 0.0000 scw = 10.0 vic = 20.0 xitmax = 40.0 epsmax = 0.00060 CONFIGURATION NO. 1. delta ord shift for moment = -8.0000 CURVE 1 IS SWEPT 0.0000 DEGREES ON PLANFORM 1 CURVE 1 IS SWEPT 0.0000 DEGREES ON PLANFORM 2 BREAK POINTS FOR THIS CONFIGURATION POINT X Y Z SWEEP DIHEDRAL ANGLE ANGLE 1 76.9500 0.0000 -8.8000 0.0000 0.0000 2 76.9500 -20.0000 -8.8000 0.0000 0.0000 3 76.9500 -34.0000 -8.8000 31.7116 0.0000 4 57.6100 -65.3000 -8.8000 90.0000 0.0000 5 33.6400 -65.3000 -8.8000 -6.1814 0.0000 6 30.2500 -34.0000 -8.8000 0.0000 0.0000 7 30.2500 0.0000 -8.8000 SECOND PLANFORM BREAK POINTS 1 -17.9000 0.0000 0.0000 0.0000 0.0000 2 -17.9000 -34.0000 0.0000 -26.2114 0.0000 3 -2.4908 -65.3000 0.0000 -26.2114 0.0000 4 46.1000-164.0000 0.0000 90.0000 0.0000 5 5.6000-164.0000 0.0000 -45.2969 0.0000 6-139.9000 -20.0000 0.0000 0.0000 0.0000 7-139.9000 0.0000 0.0000 280 HORSESHOE VORTICES USED PLANFORM TOTAL SPANWISE 1 80 8 2 200 20 10. HORSESHOE VORTICES IN EACH CHORDWISE ROW xcfw = 0.00 xcft = 0.65 fkon = 0.00 ficam = 1.00 punch = 0.00 crbmnt = 0.000 cmb = -.10 iflag = 1 relax = 0.03 fioutw = 1.00 cd0 = 0.0000 firbm = 0.00 yrbm = 0.0000 zrbm = 0.0000 drag polar on canard (conv. sec) there are 1.0 polars on this surface 18.0 points this polar planform 1 qcl qcd 0.0000 0.0000 0.1000 0.0000 0.2500 0.0002 0.3000 0.0008 0.4000 0.0018 0.5000 0.0032 0.5500 0.0040 0.6000 0.0054 0.6500 0.0069 0.7000 0.0088 0.7500 0.0113 0.8000 0.0148 0.8500 0.0198 0.8800 0.0240 0.9150 0.0360 1.0000 0.0880 1.2000 0.2680 1.8000 0.9880 drag polar there are 1.0 polars on this surface 22.0 points this polar planform 2 qcl qcd 0.0000 0.0003 0.2000 0.0003 0.3000 0.0005 0.4000 0.0008 0.5000 0.0012 0.6000 0.0018 0.7000 0.0024 0.8000 0.0032 0.9000 0.0044 0.9500 0.0053 0.9700 0.0057 0.9900 0.0062 1.0000 0.0065 1.0200 0.0073 1.0400 0.0082 1.0600 0.0093 1.0800 0.0109 1.1000 0.0128 1.1250 0.0240 1.1300 0.0360 1.2000 0.2040 2.0000 2.1240 LM = 70 IL = 71 JM = 72 IM = 73 TSPAN =-164.000 TSPANA = -65.300 BOTL = 164.000 BOL = 65.300 SNN = 1.6400 DELTYB = 3.2800 NMA(KBOT) = 50 KBOT = 2 NMA(KBIT) = 20 KBIT = 1 induced drag cd = 0.06815 pressure drag cdpt = 0.01665 induced drag cd = 0.06818 pressure drag cdpt = 0.01441 induced drag cd = 0.06827 pressure drag cdpt = 0.01255 induced drag cd = 0.06839 pressure drag cdpt = 0.01139 induced drag cd = 0.06850 pressure drag cdpt = 0.01053 induced drag cd = 0.06863 pressure drag cdpt = 0.00976 induced drag cd = 0.06876 pressure drag cdpt = 0.00915 induced drag cd = 0.06885 pressure drag cdpt = 0.00886 induced drag cd = 0.06893 pressure drag cdpt = 0.00868 induced drag cd = 0.06898 pressure drag cdpt = 0.00856 induced drag cd = 0.06902 pressure drag cdpt = 0.00847 induced drag cd = 0.06905 pressure drag cdpt = 0.00841 induced drag cd = 0.06907 pressure drag cdpt = 0.00836 induced drag cd = 0.06909 pressure drag cdpt = 0.00832 induced drag cd = 0.06911 pressure drag cdpt = 0.00829 induced drag cd = 0.06913 pressure drag cdpt = 0.00826 induced drag cd = 0.06915 pressure drag cdpt = 0.00823 induced drag cd = 0.06916 pressure drag cdpt = 0.00821 induced drag cd = 0.06917 pressure drag cdpt = 0.00819 induced drag cd = 0.06918 pressure drag cdpt = 0.00817 induced drag cd = 0.06919 pressure drag cdpt = 0.00816 induced drag cd = 0.06920 pressure drag cdpt = 0.00815 induced drag cd = 0.06921 pressure drag cdpt = 0.00814 induced drag cd = 0.06921 pressure drag cdpt = 0.00813 induced drag cd = 0.06922 pressure drag cdpt = 0.00812 induced drag cd = 0.06923 pressure drag cdpt = 0.00811 induced drag cd = 0.06923 pressure drag cdpt = 0.00810 induced drag cd = 0.06924 pressure drag cdpt = 0.00810 induced drag cd = 0.06924 pressure drag cdpt = 0.00809 induced drag cd = 0.06924 pressure drag cdpt = 0.00809 induced drag cd = 0.06925 pressure drag cdpt = 0.00808 pressure drag iteration has converged k eps cl cdi cdp cdi+cdp 1 28.66362 0.90000 0.06815 0.01665 0.08480 2 0.05789 0.90000 0.06818 0.01441 0.08260 3 0.05278 0.90000 0.06827 0.01255 0.08082 4 0.04274 0.90000 0.06839 0.01139 0.07978 5 0.03408 0.90000 0.06850 0.01053 0.07903 6 0.03155 0.90000 0.06863 0.00976 0.07839 7 0.02773 0.90000 0.06876 0.00915 0.07791 8 0.02043 0.90000 0.06885 0.00886 0.07772 9 0.01549 0.90000 0.06893 0.00868 0.07761 10 0.01218 0.90000 0.06898 0.00856 0.07754 11 0.00994 0.90000 0.06902 0.00847 0.07749 12 0.00847 0.90000 0.06905 0.00841 0.07746 13 0.00724 0.90000 0.06907 0.00836 0.07743 14 0.00616 0.90000 0.06909 0.00832 0.07741 15 0.00519 0.90000 0.06911 0.00829 0.07740 16 0.00442 0.90000 0.06913 0.00826 0.07739 17 0.00371 0.90000 0.06915 0.00823 0.07738 18 0.00310 0.90000 0.06916 0.00821 0.07737 19 0.00263 0.90000 0.06917 0.00819 0.07736 20 0.00221 0.90000 0.06918 0.00817 0.07736 21 0.00183 0.90000 0.06919 0.00816 0.07735 22 0.00154 0.90000 0.06920 0.00815 0.07735 23 0.00131 0.90000 0.06921 0.00814 0.07734 24 0.00112 0.90000 0.06921 0.00813 0.07734 25 0.00095 0.90000 0.06922 0.00812 0.07734 26 0.00084 0.90000 0.06923 0.00811 0.07734 27 0.00076 0.90000 0.06923 0.00810 0.07733 28 0.00069 0.90000 0.06924 0.00810 0.07733 29 0.00064 0.90000 0.06924 0.00809 0.07733 30 0.00061 0.90000 0.06924 0.00809 0.07733 31 0.00057 0.90000 0.06925 0.00808 0.07733 induced + pressure drag was minimized on this run ref. chord = 89.500 c average = 81.2195 true area = 32771.566 ref. area = 26640.000 b/2 = 164.0000 ref ar = 4.0384 true ar = 3.2828 Mach number = 0.9000 first planform cl = 0.17126 cm = 0.11493 cb = -0.01502 second planform cl = 0.72874 cm = -0.21493 cb = -0.18341 1st planform CL = 0.1713 CDP = 0.0042 CM = 0.1150 CB = -0.0151 2nd planform CL = 0.7292 CDP = 0.0038 CM = -0.2149 CB = 0.0000 no root bending moment constraint CL DES = 0.90000 CL COMPUTED = 0.9005 CM = -0.0999 CD I = 0.06925 E = 0.9230 CDPRESS = 0.00804 CDTOTAL = 0.07729 first planform Y CL*C/CAVE C/CAVE CL CD -61.2000 0.21189 0.33178 0.63862 0.00651 -53.0000 0.33566 0.40510 0.82857 0.01765 -44.8000 0.41311 0.47842 0.86348 0.02166 -37.3500 0.46740 0.54503 0.85757 0.02082 -29.9000 0.49499 0.57498 0.86088 0.02129 -22.9000 0.50260 0.57498 0.87411 0.02317 -15.9000 0.50504 0.57498 0.87835 0.02377 -5.9000 0.50631 0.57498 0.88056 0.02419 second planform -159.9000 0.33879 0.52480 0.64556 0.00208 -151.7000 0.53136 0.57711 0.92072 0.00478 -143.5000 0.64513 0.62942 1.02495 0.00752 -135.3000 0.72403 0.68173 1.06206 0.00946 -127.1000 0.78509 0.73404 1.06954 0.01006 -118.9000 0.83563 0.78635 1.06267 0.00951 -110.7000 0.87760 0.83866 1.04644 0.00855 -102.5000 0.91055 0.89096 1.02198 0.00739 -94.3000 0.93428 0.94327 0.99047 0.00622 -86.1000 0.94681 0.99558 0.95101 0.00530 -77.9000 0.94347 1.04789 0.90036 0.00443 -69.5500 0.90911 1.10116 0.82559 0.00354 -61.2000 0.82859 1.15442 0.71775 0.00258 -53.0000 0.74419 1.20673 0.61670 0.00189 -44.8000 0.67721 1.25904 0.53788 0.00145 -37.3500 0.63142 1.30656 0.48327 0.00117 -29.9000 0.60043 1.37894 0.43543 0.00096 -22.9000 0.58289 1.46602 0.39760 0.00079 -15.9000 0.57323 1.50210 0.38162 0.00074 -5.9000 0.56730 1.50210 0.37767 0.00073 mean camber lines to obtain the spanload (subsonic linear theory) y= -61.2000 y/(b/2) = -0.3732 chord= 26.9474 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0750 0.1295 0.1750 0.0672 0.2750 0.0194 0.3750 -0.0200 0.4750 -0.0522 0.5750 -0.0775 0.6750 -0.0960 0.7750 -0.1077 0.8750 -0.1122 0.9750 -0.1081 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0299 0.0000 -0.8067 0.0000 0.0250 -0.0332 0.6737 -0.8944 -0.0040 0.0500 -0.0365 1.3474 -0.9831 -0.0080 0.0750 -0.0398 2.0211 -1.0717 -0.0121 0.1000 -0.0429 2.6947 -1.1558 -0.0159 0.1250 -0.0457 3.3684 -1.2310 -0.0195 0.1500 -0.0480 4.0421 -1.2945 -0.0226 0.1750 -0.0499 4.7158 -1.3456 -0.0252 0.2000 -0.0514 5.3895 -1.3857 -0.0275 0.2250 -0.0526 6.0632 -1.4166 -0.0294 0.2500 -0.0534 6.7368 -1.4399 -0.0310 0.2750 -0.0540 7.4105 -1.4563 -0.0323 0.3000 -0.0544 8.0842 -1.4660 -0.0334 0.3250 -0.0545 8.7579 -1.4689 -0.0343 0.3500 -0.0544 9.4316 -1.4651 -0.0349 0.3750 -0.0540 10.1053 -1.4548 -0.0353 0.4000 -0.0534 10.7790 -1.4383 -0.0354 0.4250 -0.0525 11.4526 -1.4160 -0.0353 0.4500 -0.0515 12.1263 -1.3884 -0.0351 0.4750 -0.0503 12.8000 -1.3556 -0.0346 0.5000 -0.0489 13.4737 -1.3181 -0.0339 0.5250 -0.0474 14.1474 -1.2760 -0.0331 0.5500 -0.0456 14.8211 -1.2297 -0.0322 0.5750 -0.0438 15.4948 -1.1794 -0.0310 0.6000 -0.0418 16.1684 -1.1254 -0.0298 0.6250 -0.0396 16.8421 -1.0679 -0.0284 0.6500 -0.0374 17.5158 -1.0074 -0.0269 0.6750 -0.0350 18.1895 -0.9440 -0.0253 0.7000 -0.0326 18.8632 -0.8781 -0.0236 0.7250 -0.0301 19.5369 -0.8100 -0.0218 0.7500 -0.0275 20.2105 -0.7400 -0.0200 0.7750 -0.0248 20.8842 -0.6682 -0.0181 0.8000 -0.0221 21.5579 -0.5950 -0.0161 0.8250 -0.0193 22.2316 -0.5205 -0.0141 0.8500 -0.0165 22.9053 -0.4452 -0.0120 0.8750 -0.0137 23.5790 -0.3696 -0.0100 0.9000 -0.0109 24.2527 -0.2942 -0.0079 0.9250 -0.0081 24.9263 -0.2196 -0.0059 0.9500 -0.0054 25.6000 -0.1458 -0.0039 0.9750 -0.0027 26.2737 -0.0728 -0.0020 1.0000 0.0000 26.9474 0.0000 0.0000 y= -53.0000 y/(b/2) = -0.3232 chord= 32.9022 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0750 0.0783 0.1750 -0.0034 0.2750 -0.0572 0.3750 -0.0982 0.4750 -0.1306 0.5750 -0.1557 0.6750 -0.1740 0.7750 -0.1854 0.8750 -0.1898 0.9750 -0.1845 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.1036 0.0000 -3.4093 0.0000 0.0250 -0.1056 0.8226 -3.4745 -0.0046 0.0500 -0.1076 1.6451 -3.5414 -0.0092 0.0750 -0.1097 2.4677 -3.6080 -0.0138 0.1000 -0.1115 3.2902 -3.6674 -0.0182 0.1250 -0.1128 4.1128 -3.7122 -0.0222 0.1500 -0.1136 4.9353 -3.7381 -0.0255 0.1750 -0.1138 5.7579 -3.7444 -0.0283 0.2000 -0.1135 6.5804 -3.7339 -0.0306 0.2250 -0.1128 7.4030 -3.7102 -0.0325 0.2500 -0.1117 8.2256 -3.6761 -0.0340 0.2750 -0.1104 9.0481 -3.6333 -0.0353 0.3000 -0.1089 9.8707 -3.5819 -0.0363 0.3250 -0.1070 10.6932 -3.5220 -0.0371 0.3500 -0.1050 11.5158 -3.4534 -0.0376 0.3750 -0.1026 12.3383 -3.3766 -0.0379 0.4000 -0.1001 13.1609 -3.2920 -0.0379 0.4250 -0.0973 13.9834 -3.2003 -0.0377 0.4500 -0.0943 14.8060 -3.1020 -0.0373 0.4750 -0.0911 15.6285 -2.9975 -0.0367 0.5000 -0.0878 16.4511 -2.8872 -0.0359 0.5250 -0.0842 17.2737 -2.7715 -0.0350 0.5500 -0.0806 18.0962 -2.6505 -0.0339 0.5750 -0.0767 18.9188 -2.5247 -0.0327 0.6000 -0.0728 19.7413 -2.3945 -0.0313 0.6250 -0.0687 20.5639 -2.2601 -0.0298 0.6500 -0.0645 21.3864 -2.1219 -0.0282 0.6750 -0.0602 22.2090 -1.9804 -0.0265 0.7000 -0.0558 23.0315 -1.8358 -0.0247 0.7250 -0.0513 23.8541 -1.6886 -0.0228 0.7500 -0.0468 24.6766 -1.5391 -0.0209 0.7750 -0.0422 25.4992 -1.3875 -0.0189 0.8000 -0.0375 26.3218 -1.2341 -0.0168 0.8250 -0.0328 27.1443 -1.0792 -0.0147 0.8500 -0.0281 27.9669 -0.9233 -0.0125 0.8750 -0.0233 28.7894 -0.7671 -0.0104 0.9000 -0.0186 29.6120 -0.6114 -0.0082 0.9250 -0.0139 30.4345 -0.4569 -0.0061 0.9500 -0.0092 31.2571 -0.3038 -0.0041 0.9750 -0.0046 32.0796 -0.1517 -0.0020 1.0000 0.0000 32.9022 0.0000 0.0000 y= -44.8000 y/(b/2) = -0.2732 chord= 38.8570 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0750 0.0351 0.1750 -0.0472 0.2750 -0.0965 0.3750 -0.1310 0.4750 -0.1566 0.5750 -0.1756 0.6750 -0.1889 0.7750 -0.1968 0.8750 -0.1987 0.9750 -0.1920 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.1293 0.0000 -5.0240 0.0000 0.0250 -0.1302 0.9714 -5.0590 -0.0041 0.0500 -0.1312 1.9429 -5.0961 -0.0083 0.0750 -0.1321 2.9143 -5.1328 -0.0125 0.1000 -0.1328 3.8857 -5.1609 -0.0165 0.1250 -0.1331 4.8571 -5.1713 -0.0200 0.1500 -0.1328 5.8286 -5.1593 -0.0229 0.1750 -0.1319 6.8000 -5.1241 -0.0252 0.2000 -0.1305 7.7714 -5.0694 -0.0270 0.2250 -0.1287 8.7428 -5.0000 -0.0285 0.2500 -0.1266 9.7143 -4.9195 -0.0296 0.2750 -0.1243 10.6857 -4.8300 -0.0306 0.3000 -0.1218 11.6571 -4.7320 -0.0313 0.3250 -0.1190 12.6285 -4.6253 -0.0318 0.3500 -0.1161 13.6000 -4.5100 -0.0320 0.3750 -0.1129 14.5714 -4.3866 -0.0321 0.4000 -0.1095 15.5428 -4.2557 -0.0319 0.4250 -0.1060 16.5142 -4.1180 -0.0316 0.4500 -0.1023 17.4857 -3.9742 -0.0312 0.4750 -0.0984 18.4571 -3.8247 -0.0305 0.5000 -0.0944 19.4285 -3.6700 -0.0298 0.5250 -0.0903 20.3999 -3.5103 -0.0289 0.5500 -0.0861 21.3714 -3.3460 -0.0279 0.5750 -0.0818 22.3428 -3.1774 -0.0268 0.6000 -0.0773 23.3142 -3.0049 -0.0256 0.6250 -0.0728 24.2856 -2.8288 -0.0243 0.6500 -0.0682 25.2571 -2.6495 -0.0229 0.6750 -0.0635 26.2285 -2.4673 -0.0215 0.7000 -0.0587 27.1999 -2.2826 -0.0200 0.7250 -0.0539 28.1713 -2.0957 -0.0184 0.7500 -0.0491 29.1428 -1.9070 -0.0168 0.7750 -0.0442 30.1142 -1.7166 -0.0151 0.8000 -0.0392 31.0856 -1.5247 -0.0134 0.8250 -0.0343 32.0570 -1.3318 -0.0116 0.8500 -0.0293 33.0285 -1.1382 -0.0099 0.8750 -0.0243 33.9999 -0.9447 -0.0082 0.9000 -0.0194 34.9713 -0.7524 -0.0064 0.9250 -0.0145 35.9427 -0.5619 -0.0048 0.9500 -0.0096 36.9142 -0.3735 -0.0031 0.9750 -0.0048 37.8856 -0.1865 -0.0016 1.0000 0.0000 38.8570 0.0000 0.0000 y= -37.3500 y/(b/2) = -0.2277 chord= 44.2672 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0750 -0.0422 0.1750 -0.1199 0.2750 -0.1619 0.3750 -0.1883 0.4750 -0.2063 0.5750 -0.2190 0.6750 -0.2275 0.7750 -0.2321 0.8750 -0.2322 0.9750 -0.2247 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.1810 0.0000 -8.0115 0.0000 0.0250 -0.1799 1.1067 -7.9658 -0.0035 0.0500 -0.1790 2.2134 -7.9224 -0.0070 0.0750 -0.1780 3.3200 -7.8786 -0.0106 0.1000 -0.1768 4.4267 -7.8253 -0.0139 0.1250 -0.1751 5.5334 -7.7529 -0.0168 0.1500 -0.1730 6.6401 -7.6562 -0.0191 0.1750 -0.1702 7.7468 -7.5349 -0.0209 0.2000 -0.1670 8.8534 -7.3930 -0.0222 0.2250 -0.1635 9.9601 -7.2364 -0.0232 0.2500 -0.1597 11.0668 -7.0692 -0.0240 0.2750 -0.1557 12.1735 -6.8938 -0.0245 0.3000 -0.1516 13.2802 -6.7109 -0.0249 0.3250 -0.1473 14.3868 -6.5203 -0.0251 0.3500 -0.1428 15.4935 -6.3223 -0.0252 0.3750 -0.1382 16.6002 -6.1172 -0.0251 0.4000 -0.1334 17.7069 -5.9057 -0.0248 0.4250 -0.1285 18.8136 -5.6887 -0.0244 0.4500 -0.1235 19.9202 -5.4668 -0.0240 0.4750 -0.1184 21.0269 -5.2405 -0.0234 0.5000 -0.1132 22.1336 -5.0102 -0.0227 0.5250 -0.1079 23.2403 -4.7761 -0.0219 0.5500 -0.1025 24.3470 -4.5385 -0.0211 0.5750 -0.0971 25.4537 -4.2977 -0.0202 0.6000 -0.0916 26.5603 -4.0539 -0.0192 0.6250 -0.0860 27.6670 -3.8075 -0.0181 0.6500 -0.0804 28.7737 -3.5587 -0.0170 0.6750 -0.0747 29.8804 -3.3079 -0.0159 0.7000 -0.0690 30.9871 -3.0553 -0.0147 0.7250 -0.0633 32.0937 -2.8013 -0.0135 0.7500 -0.0575 33.2004 -2.5460 -0.0123 0.7750 -0.0517 34.3071 -2.2897 -0.0110 0.8000 -0.0459 35.4138 -2.0323 -0.0097 0.8250 -0.0401 36.5205 -1.7743 -0.0084 0.8500 -0.0342 37.6271 -1.5161 -0.0071 0.8750 -0.0284 38.7338 -1.2585 -0.0058 0.9000 -0.0226 39.8405 -1.0025 -0.0045 0.9250 -0.0169 40.9472 -0.7489 -0.0033 0.9500 -0.0112 42.0539 -0.4979 -0.0022 0.9750 -0.0056 43.1605 -0.2487 -0.0011 1.0000 0.0000 44.2672 0.0000 0.0000 y= -29.9000 y/(b/2) = -0.1823 chord= 46.7000 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0750 -0.0403 0.1750 -0.1078 0.2750 -0.1474 0.3750 -0.1733 0.4750 -0.1911 0.5750 -0.2034 0.6750 -0.2112 0.7750 -0.2150 0.8750 -0.2143 0.9750 -0.2061 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.1670 0.0000 -7.7974 0.0000 0.0250 -0.1660 1.1675 -7.7512 -0.0032 0.0500 -0.1650 2.3350 -7.7071 -0.0064 0.0750 -0.1641 3.5025 -7.6626 -0.0096 0.1000 -0.1629 4.6700 -7.6095 -0.0127 0.1250 -0.1614 5.8375 -7.5392 -0.0153 0.1500 -0.1595 7.0050 -7.4466 -0.0175 0.1750 -0.1570 8.1725 -7.3312 -0.0192 0.2000 -0.1541 9.3400 -7.1967 -0.0205 0.2250 -0.1509 10.5075 -7.0479 -0.0215 0.2500 -0.1475 11.6750 -6.8884 -0.0223 0.2750 -0.1439 12.8425 -6.7203 -0.0229 0.3000 -0.1401 14.0100 -6.5443 -0.0233 0.3250 -0.1362 15.1775 -6.3604 -0.0235 0.3500 -0.1321 16.3450 -6.1687 -0.0236 0.3750 -0.1278 17.5125 -5.9698 -0.0235 0.4000 -0.1234 18.6800 -5.7643 -0.0233 0.4250 -0.1189 19.8475 -5.5530 -0.0229 0.4500 -0.1143 21.0150 -5.3366 -0.0224 0.4750 -0.1095 22.1825 -5.1156 -0.0219 0.5000 -0.1047 23.3500 -4.8905 -0.0212 0.5250 -0.0998 24.5175 -4.6614 -0.0205 0.5500 -0.0948 25.6850 -4.4287 -0.0197 0.5750 -0.0898 26.8525 -4.1928 -0.0188 0.6000 -0.0847 28.0200 -3.9540 -0.0179 0.6250 -0.0795 29.1875 -3.7125 -0.0169 0.6500 -0.0743 30.3550 -3.4688 -0.0158 0.6750 -0.0690 31.5225 -3.2231 -0.0148 0.7000 -0.0637 32.6900 -2.9757 -0.0136 0.7250 -0.0584 33.8575 -2.7271 -0.0125 0.7500 -0.0530 35.0250 -2.4773 -0.0113 0.7750 -0.0477 36.1925 -2.2267 -0.0101 0.8000 -0.0423 37.3600 -1.9753 -0.0089 0.8250 -0.0369 38.5275 -1.7234 -0.0077 0.8500 -0.0315 39.6950 -1.4715 -0.0065 0.8750 -0.0261 40.8625 -1.2204 -0.0053 0.9000 -0.0208 42.0300 -0.9714 -0.0041 0.9250 -0.0155 43.1975 -0.7252 -0.0030 0.9500 -0.0103 44.3650 -0.4818 -0.0020 0.9750 -0.0052 45.5325 -0.2406 -0.0010 1.0000 0.0000 46.7000 0.0000 0.0000 y= -22.9000 y/(b/2) = -0.1396 chord= 46.7000 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0750 -0.0070 0.1750 -0.0691 0.2750 -0.1089 0.3750 -0.1368 0.4750 -0.1569 0.5750 -0.1712 0.6750 -0.1806 0.7750 -0.1853 0.8750 -0.1848 0.9750 -0.1764 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.1336 0.0000 -6.2379 0.0000 0.0250 -0.1334 1.1675 -6.2305 -0.0032 0.0500 -0.1333 2.3350 -6.2252 -0.0064 0.0750 -0.1332 3.5025 -6.2194 -0.0096 0.1000 -0.1329 4.6700 -6.2059 -0.0127 0.1250 -0.1323 5.8375 -6.1765 -0.0154 0.1500 -0.1312 7.0050 -6.1267 -0.0177 0.1750 -0.1297 8.1725 -6.0558 -0.0195 0.2000 -0.1278 9.3400 -5.9667 -0.0209 0.2250 -0.1256 10.5075 -5.8637 -0.0220 0.2500 -0.1231 11.6750 -5.7499 -0.0229 0.2750 -0.1205 12.8425 -5.6270 -0.0237 0.3000 -0.1177 14.0100 -5.4956 -0.0242 0.3250 -0.1147 15.1775 -5.3558 -0.0245 0.3500 -0.1115 16.3450 -5.2076 -0.0247 0.3750 -0.1082 17.5125 -5.0516 -0.0247 0.4000 -0.1047 18.6800 -4.8884 -0.0245 0.4250 -0.1010 19.8475 -4.7188 -0.0242 0.4500 -0.0973 21.0150 -4.5434 -0.0238 0.4750 -0.0934 22.1825 -4.3626 -0.0233 0.5000 -0.0894 23.3500 -4.1770 -0.0227 0.5250 -0.0854 24.5175 -3.9869 -0.0219 0.5500 -0.0812 25.6850 -3.7926 -0.0211 0.5750 -0.0770 26.8525 -3.5944 -0.0202 0.6000 -0.0727 28.0200 -3.3929 -0.0192 0.6250 -0.0683 29.1875 -3.1882 -0.0182 0.6500 -0.0638 30.3550 -2.9807 -0.0171 0.6750 -0.0593 31.5225 -2.7709 -0.0159 0.7000 -0.0548 32.6900 -2.5592 -0.0147 0.7250 -0.0502 33.8575 -2.3458 -0.0135 0.7500 -0.0456 35.0250 -2.1311 -0.0122 0.7750 -0.0410 36.1925 -1.9153 -0.0110 0.8000 -0.0364 37.3600 -1.6986 -0.0097 0.8250 -0.0317 38.5275 -1.4812 -0.0083 0.8500 -0.0271 39.6950 -1.2637 -0.0070 0.8750 -0.0224 40.8625 -1.0471 -0.0057 0.9000 -0.0178 42.0300 -0.8326 -0.0045 0.9250 -0.0133 43.1975 -0.6209 -0.0033 0.9500 -0.0088 44.3650 -0.4123 -0.0022 0.9750 -0.0044 45.5325 -0.2058 -0.0011 1.0000 0.0000 46.7000 0.0000 0.0000 y= -15.9000 y/(b/2) = -0.0970 chord= 46.7000 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0750 0.0051 0.1750 -0.0530 0.2750 -0.0903 0.3750 -0.1168 0.4750 -0.1360 0.5750 -0.1497 0.6750 -0.1586 0.7750 -0.1629 0.8750 -0.1621 0.9750 -0.1534 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.1139 0.0000 -5.3197 0.0000 0.0250 -0.1141 1.1675 -5.3263 -0.0030 0.0500 -0.1142 2.3350 -5.3348 -0.0060 0.0750 -0.1144 3.5025 -5.3429 -0.0090 0.1000 -0.1144 4.6700 -5.3438 -0.0119 0.1250 -0.1141 5.8375 -5.3298 -0.0145 0.1500 -0.1134 7.0050 -5.2968 -0.0166 0.1750 -0.1123 8.1725 -5.2441 -0.0183 0.2000 -0.1108 9.3400 -5.1745 -0.0197 0.2250 -0.1090 10.5075 -5.0918 -0.0207 0.2500 -0.1070 11.6750 -4.9989 -0.0216 0.2750 -0.1049 12.8425 -4.8976 -0.0223 0.3000 -0.1025 14.0100 -4.7882 -0.0228 0.3250 -0.1000 15.1775 -4.6707 -0.0231 0.3500 -0.0973 16.3450 -4.5454 -0.0233 0.3750 -0.0945 17.5125 -4.4127 -0.0233 0.4000 -0.0915 18.6800 -4.2730 -0.0232 0.4250 -0.0884 19.8475 -4.1272 -0.0229 0.4500 -0.0851 21.0150 -3.9759 -0.0225 0.4750 -0.0818 22.1825 -3.8194 -0.0220 0.5000 -0.0783 23.3500 -3.6583 -0.0214 0.5250 -0.0748 24.5175 -3.4929 -0.0207 0.5500 -0.0712 25.6850 -3.3234 -0.0199 0.5750 -0.0675 26.8525 -3.1503 -0.0190 0.6000 -0.0637 28.0200 -2.9739 -0.0181 0.6250 -0.0598 29.1875 -2.7946 -0.0171 0.6500 -0.0559 30.3550 -2.6126 -0.0161 0.6750 -0.0520 31.5225 -2.4284 -0.0150 0.7000 -0.0480 32.6900 -2.2423 -0.0138 0.7250 -0.0440 33.8575 -2.0548 -0.0127 0.7500 -0.0400 35.0250 -1.8660 -0.0115 0.7750 -0.0359 36.1925 -1.6763 -0.0103 0.8000 -0.0318 37.3600 -1.4857 -0.0090 0.8250 -0.0277 38.5275 -1.2946 -0.0078 0.8500 -0.0236 39.6950 -1.1035 -0.0065 0.8750 -0.0196 40.8625 -0.9134 -0.0053 0.9000 -0.0155 42.0300 -0.7255 -0.0041 0.9250 -0.0116 43.1975 -0.5405 -0.0030 0.9500 -0.0077 44.3650 -0.3586 -0.0020 0.9750 -0.0038 45.5325 -0.1790 -0.0010 1.0000 0.0000 46.7000 0.0000 0.0000 y= -5.9000 y/(b/2) = -0.0360 chord= 46.7000 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0750 0.0111 0.1750 -0.0449 0.2750 -0.0807 0.3750 -0.1064 0.4750 -0.1251 0.5750 -0.1384 0.6750 -0.1470 0.7750 -0.1510 0.8750 -0.1500 0.9750 -0.1411 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.1036 0.0000 -4.8397 0.0000 0.0250 -0.1039 1.1675 -4.8534 -0.0029 0.0500 -0.1043 2.3350 -4.8689 -0.0058 0.0750 -0.1046 3.5025 -4.8840 -0.0087 0.1000 -0.1048 4.6700 -4.8922 -0.0115 0.1250 -0.1046 5.8375 -4.8860 -0.0139 0.1500 -0.1041 7.0050 -4.8615 -0.0160 0.1750 -0.1032 8.1725 -4.8179 -0.0177 0.2000 -0.1019 9.3400 -4.7580 -0.0190 0.2250 -0.1003 10.5075 -4.6856 -0.0200 0.2500 -0.0986 11.6750 -4.6033 -0.0208 0.2750 -0.0966 12.8425 -4.5129 -0.0215 0.3000 -0.0945 14.0100 -4.4148 -0.0220 0.3250 -0.0923 15.1775 -4.3089 -0.0223 0.3500 -0.0898 16.3450 -4.1954 -0.0225 0.3750 -0.0873 17.5125 -4.0746 -0.0225 0.4000 -0.0845 18.6800 -3.9473 -0.0223 0.4250 -0.0817 19.8475 -3.8139 -0.0221 0.4500 -0.0787 21.0150 -3.6751 -0.0217 0.4750 -0.0756 22.1825 -3.5315 -0.0212 0.5000 -0.0724 23.3500 -3.3832 -0.0206 0.5250 -0.0692 24.5175 -3.2308 -0.0200 0.5500 -0.0658 25.6850 -3.0744 -0.0192 0.5750 -0.0624 26.8525 -2.9146 -0.0184 0.6000 -0.0589 28.0200 -2.7515 -0.0175 0.6250 -0.0554 29.1875 -2.5855 -0.0165 0.6500 -0.0518 30.3550 -2.4170 -0.0155 0.6750 -0.0481 31.5225 -2.2464 -0.0144 0.7000 -0.0444 32.6900 -2.0739 -0.0133 0.7250 -0.0407 33.8575 -1.9001 -0.0122 0.7500 -0.0369 35.0250 -1.7251 -0.0110 0.7750 -0.0332 36.1925 -1.5492 -0.0099 0.8000 -0.0294 37.3600 -1.3726 -0.0087 0.8250 -0.0256 38.5275 -1.1954 -0.0075 0.8500 -0.0218 39.6950 -1.0184 -0.0063 0.8750 -0.0180 40.8625 -0.8423 -0.0051 0.9000 -0.0143 42.0300 -0.6685 -0.0040 0.9250 -0.0107 43.1975 -0.4977 -0.0029 0.9500 -0.0071 44.3650 -0.3301 -0.0019 0.9750 -0.0035 45.5325 -0.1647 -0.0009 1.0000 0.0000 46.7000 0.0000 0.0000 y= -159.9000 y/(b/2) = -0.9750 chord= 42.6243 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0750 -0.0583 0.1750 -0.1249 0.2750 -0.1780 0.3750 -0.2252 0.4750 -0.2693 0.5750 -0.3122 0.6750 -0.3670 0.7750 -0.3898 0.8750 -0.3805 0.9750 -0.3428 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.2578 0.0000 -10.9902 0.0000 0.0250 -0.2564 1.0656 -10.9288 -0.0050 0.0500 -0.2550 2.1312 -10.8692 -0.0101 0.0750 -0.2536 3.1968 -10.8093 -0.0151 0.1000 -0.2520 4.2624 -10.7420 -0.0200 0.1250 -0.2501 5.3280 -10.6596 -0.0245 0.1500 -0.2477 6.3936 -10.5574 -0.0285 0.1750 -0.2448 7.4593 -10.4343 -0.0321 0.2000 -0.2415 8.5249 -10.2923 -0.0352 0.2250 -0.2378 9.5905 -10.1345 -0.0379 0.2500 -0.2337 10.6561 -9.9632 -0.0404 0.2750 -0.2294 11.7217 -9.7795 -0.0425 0.3000 -0.2248 12.7873 -9.5837 -0.0444 0.3250 -0.2200 13.8529 -9.3754 -0.0459 0.3500 -0.2148 14.9185 -9.1544 -0.0472 0.3750 -0.2093 15.9841 -8.9207 -0.0481 0.4000 -0.2035 17.0497 -8.6746 -0.0488 0.4250 -0.1975 18.1153 -8.4162 -0.0492 0.4500 -0.1911 19.1809 -8.1461 -0.0493 0.4750 -0.1845 20.2465 -7.8647 -0.0491 0.5000 -0.1777 21.3121 -7.5724 -0.0487 0.5250 -0.1706 22.3778 -7.2696 -0.0481 0.5500 -0.1632 23.4434 -6.9558 -0.0472 0.5750 -0.1555 24.5090 -6.6298 -0.0460 0.6000 -0.1476 25.5746 -6.2899 -0.0444 0.6250 -0.1392 26.6402 -5.9346 -0.0425 0.6500 -0.1305 27.7058 -5.5639 -0.0403 0.6750 -0.1215 28.7714 -5.1791 -0.0377 0.7000 -0.1122 29.8370 -4.7829 -0.0349 0.7250 -0.1027 30.9026 -4.3782 -0.0318 0.7500 -0.0931 31.9682 -3.9679 -0.0286 0.7750 -0.0834 33.0338 -3.5538 -0.0254 0.8000 -0.0736 34.0994 -3.1375 -0.0220 0.8250 -0.0638 35.1650 -2.7208 -0.0187 0.8500 -0.0541 36.2306 -2.3060 -0.0154 0.8750 -0.0445 37.2962 -1.8966 -0.0123 0.9000 -0.0351 38.3619 -1.4966 -0.0093 0.9250 -0.0260 39.4275 -1.1086 -0.0067 0.9500 -0.0172 40.4931 -0.7326 -0.0043 0.9750 -0.0086 41.5587 -0.3650 -0.0021 1.0000 0.0000 42.6243 0.0000 0.0000 y= -151.7000 y/(b/2) = -0.9250 chord= 46.8727 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0750 -0.0374 0.1750 -0.1161 0.2750 -0.1795 0.3750 -0.2367 0.4750 -0.2916 0.5750 -0.3487 0.6750 -0.4312 0.7750 -0.4777 0.8750 -0.4842 0.9750 -0.4505 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.2952 0.0000 -13.8368 0.0000 0.0250 -0.2943 1.1718 -13.7939 -0.0065 0.0500 -0.2934 2.3436 -13.7534 -0.0130 0.0750 -0.2925 3.5155 -13.7125 -0.0195 0.1000 -0.2915 4.6873 -13.6620 -0.0258 0.1250 -0.2900 5.8591 -13.5918 -0.0317 0.1500 -0.2879 7.0309 -13.4961 -0.0370 0.1750 -0.2853 8.2027 -13.3731 -0.0418 0.2000 -0.2822 9.3745 -13.2254 -0.0460 0.2250 -0.2786 10.5464 -13.0571 -0.0498 0.2500 -0.2746 11.7182 -12.8710 -0.0532 0.2750 -0.2703 12.8900 -12.6687 -0.0563 0.3000 -0.2656 14.0618 -12.4502 -0.0590 0.3250 -0.2606 15.2336 -12.2152 -0.0613 0.3500 -0.2552 16.4055 -11.9632 -0.0633 0.3750 -0.2495 17.5773 -11.6943 -0.0650 0.4000 -0.2434 18.7491 -11.4086 -0.0663 0.4250 -0.2369 19.9209 -11.1062 -0.0672 0.4500 -0.2301 21.0927 -10.7878 -0.0678 0.4750 -0.2230 22.2646 -10.4537 -0.0680 0.5000 -0.2156 23.4364 -10.1046 -0.0680 0.5250 -0.2078 24.6082 -9.7406 -0.0676 0.5500 -0.1997 25.7800 -9.3606 -0.0669 0.5750 -0.1912 26.9518 -8.9622 -0.0657 0.6000 -0.1822 28.1237 -8.5422 -0.0642 0.6250 -0.1728 29.2955 -8.0975 -0.0621 0.6500 -0.1627 30.4673 -7.6275 -0.0594 0.6750 -0.1522 31.6391 -7.1333 -0.0562 0.7000 -0.1412 32.8109 -6.6183 -0.0526 0.7250 -0.1299 33.9827 -6.0867 -0.0487 0.7500 -0.1182 35.1546 -5.5418 -0.0444 0.7750 -0.1064 36.3264 -4.9865 -0.0400 0.8000 -0.0944 37.4982 -4.4229 -0.0353 0.8250 -0.0822 38.6700 -3.8534 -0.0305 0.8500 -0.0700 39.8418 -3.2813 -0.0257 0.8750 -0.0578 41.0137 -2.7111 -0.0209 0.9000 -0.0458 42.1855 -2.1484 -0.0163 0.9250 -0.0341 43.3573 -1.5971 -0.0119 0.9500 -0.0226 44.5291 -1.0580 -0.0078 0.9750 -0.0113 45.7009 -0.5276 -0.0039 1.0000 0.0000 46.8727 0.0000 0.0000 y= -143.5000 y/(b/2) = -0.8750 chord= 51.1212 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0750 -0.0045 0.1750 -0.0788 0.2750 -0.1374 0.3750 -0.1903 0.4750 -0.2422 0.5750 -0.2995 0.6750 -0.3895 0.7750 -0.4439 0.8750 -0.4565 0.9750 -0.4249 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.2564 0.0000 -13.1069 0.0000 0.0250 -0.2563 1.2780 -13.1022 -0.0063 0.0500 -0.2563 2.5561 -13.1000 -0.0127 0.0750 -0.2562 3.8341 -13.0974 -0.0190 0.1000 -0.2560 5.1121 -13.0847 -0.0252 0.1250 -0.2553 6.3902 -13.0519 -0.0310 0.1500 -0.2542 7.6682 -12.9926 -0.0362 0.1750 -0.2524 8.9462 -12.9052 -0.0409 0.2000 -0.2502 10.2242 -12.7926 -0.0451 0.2250 -0.2476 11.5023 -12.6591 -0.0489 0.2500 -0.2447 12.7803 -12.5078 -0.0524 0.2750 -0.2414 14.0583 -12.3402 -0.0555 0.3000 -0.2378 15.3364 -12.1565 -0.0583 0.3250 -0.2339 16.6144 -11.9561 -0.0608 0.3500 -0.2296 17.8924 -11.7387 -0.0630 0.3750 -0.2250 19.1705 -11.5042 -0.0648 0.4000 -0.2201 20.4485 -11.2524 -0.0663 0.4250 -0.2149 21.7265 -10.9837 -0.0674 0.4500 -0.2093 23.0046 -10.6982 -0.0683 0.4750 -0.2034 24.2826 -10.3966 -0.0688 0.5000 -0.1972 25.5606 -10.0792 -0.0690 0.5250 -0.1906 26.8386 -9.7461 -0.0689 0.5500 -0.1838 28.1167 -9.3955 -0.0684 0.5750 -0.1765 29.3947 -9.0244 -0.0676 0.6000 -0.1688 30.6727 -8.6284 -0.0662 0.6250 -0.1605 31.9508 -8.2035 -0.0643 0.6500 -0.1516 33.2288 -7.7483 -0.0618 0.6750 -0.1421 34.5068 -7.2640 -0.0588 0.7000 -0.1321 35.7849 -6.7543 -0.0552 0.7250 -0.1217 37.0629 -6.2238 -0.0512 0.7500 -0.1110 38.3409 -5.6763 -0.0469 0.7750 -0.1001 39.6190 -5.1151 -0.0424 0.8000 -0.0889 40.8970 -4.5425 -0.0376 0.8250 -0.0775 42.1750 -3.9612 -0.0326 0.8500 -0.0660 43.4530 -3.3752 -0.0276 0.8750 -0.0546 44.7311 -2.7895 -0.0225 0.9000 -0.0432 46.0091 -2.2106 -0.0176 0.9250 -0.0321 47.2871 -1.6432 -0.0129 0.9500 -0.0213 48.5652 -1.0883 -0.0085 0.9750 -0.0106 49.8432 -0.5427 -0.0042 1.0000 0.0000 51.1212 0.0000 0.0000 y= -135.3000 y/(b/2) = -0.8250 chord= 55.3697 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0750 0.0222 0.1750 -0.0471 0.2750 -0.1008 0.3750 -0.1496 0.4750 -0.1988 0.5750 -0.2552 0.6750 -0.3477 0.7750 -0.4054 0.8750 -0.4210 0.9750 -0.3911 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.2193 0.0000 -12.1409 0.0000 0.0250 -0.2198 1.3842 -12.1726 -0.0061 0.0500 -0.2205 2.7685 -12.2068 -0.0122 0.0750 -0.2211 4.1527 -12.2406 -0.0182 0.1000 -0.2215 5.5370 -12.2642 -0.0242 0.1250 -0.2216 6.9212 -12.2674 -0.0297 0.1500 -0.2211 8.3055 -12.2439 -0.0348 0.1750 -0.2202 9.6897 -12.1922 -0.0393 0.2000 -0.2188 11.0739 -12.1151 -0.0434 0.2250 -0.2170 12.4582 -12.0172 -0.0471 0.2500 -0.2149 13.8424 -11.9015 -0.0505 0.2750 -0.2126 15.2267 -11.7698 -0.0536 0.3000 -0.2099 16.6109 -11.6222 -0.0564 0.3250 -0.2069 17.9952 -11.4580 -0.0589 0.3500 -0.2037 19.3794 -11.2768 -0.0611 0.3750 -0.2001 20.7636 -11.0784 -0.0630 0.4000 -0.1962 22.1479 -10.8626 -0.0646 0.4250 -0.1920 23.5321 -10.6294 -0.0659 0.4500 -0.1875 24.9164 -10.3792 -0.0669 0.4750 -0.1826 26.3006 -10.1122 -0.0675 0.5000 -0.1775 27.6849 -9.8290 -0.0679 0.5250 -0.1721 29.0691 -9.5292 -0.0679 0.5500 -0.1664 30.4533 -9.2110 -0.0677 0.5750 -0.1602 31.8376 -8.8705 -0.0670 0.6000 -0.1536 33.2218 -8.5027 -0.0659 0.6250 -0.1463 34.6061 -8.1029 -0.0641 0.6500 -0.1385 35.9903 -7.6694 -0.0618 0.6750 -0.1301 37.3746 -7.2033 -0.0588 0.7000 -0.1212 38.7588 -6.7085 -0.0554 0.7250 -0.1118 40.1430 -6.1900 -0.0515 0.7500 -0.1021 41.5273 -5.6520 -0.0473 0.7750 -0.0921 42.9115 -5.0979 -0.0427 0.8000 -0.0818 44.2958 -4.5305 -0.0380 0.8250 -0.0714 45.6800 -3.9526 -0.0330 0.8500 -0.0608 47.0643 -3.3684 -0.0279 0.8750 -0.0503 48.4485 -2.7837 -0.0229 0.9000 -0.0398 49.8327 -2.2053 -0.0179 0.9250 -0.0296 51.2170 -1.6387 -0.0132 0.9500 -0.0196 52.6012 -1.0850 -0.0086 0.9750 -0.0098 53.9855 -0.5410 -0.0043 1.0000 0.0000 55.3697 0.0000 0.0000 y= -127.1000 y/(b/2) = -0.7750 chord= 59.6182 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0750 0.0430 0.1750 -0.0222 0.2750 -0.0724 0.3750 -0.1184 0.4750 -0.1657 0.5750 -0.2213 0.6750 -0.3146 0.7750 -0.3738 0.8750 -0.3912 0.9750 -0.3630 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.1899 0.0000 -11.3245 0.0000 0.0250 -0.1910 1.4905 -11.3896 -0.0058 0.0500 -0.1922 2.9809 -11.4573 -0.0117 0.0750 -0.1933 4.4714 -11.5245 -0.0176 0.1000 -0.1943 5.9618 -11.5815 -0.0233 0.1250 -0.1949 7.4523 -11.6177 -0.0287 0.1500 -0.1950 8.9427 -11.6268 -0.0336 0.1750 -0.1947 10.4332 -11.6074 -0.0380 0.2000 -0.1939 11.9236 -11.5624 -0.0420 0.2250 -0.1928 13.4141 -11.4963 -0.0456 0.2500 -0.1914 14.9045 -11.4125 -0.0490 0.2750 -0.1898 16.3950 -11.3126 -0.0520 0.3000 -0.1878 17.8855 -11.1966 -0.0548 0.3250 -0.1856 19.3759 -11.0639 -0.0574 0.3500 -0.1831 20.8664 -10.9139 -0.0596 0.3750 -0.1803 22.3568 -10.7464 -0.0615 0.4000 -0.1771 23.8473 -10.5610 -0.0632 0.4250 -0.1737 25.3377 -10.3577 -0.0645 0.4500 -0.1700 26.8282 -10.1367 -0.0656 0.4750 -0.1660 28.3186 -9.8983 -0.0663 0.5000 -0.1617 29.8091 -9.6429 -0.0668 0.5250 -0.1572 31.2996 -9.3701 -0.0669 0.5500 -0.1523 32.7900 -9.0777 -0.0668 0.5750 -0.1470 34.2805 -8.7615 -0.0662 0.6000 -0.1412 35.7709 -8.4158 -0.0652 0.6250 -0.1348 37.2614 -8.0356 -0.0636 0.6500 -0.1278 38.7518 -7.6188 -0.0613 0.6750 -0.1202 40.2423 -7.1666 -0.0585 0.7000 -0.1121 41.7327 -6.6829 -0.0551 0.7250 -0.1035 43.2232 -6.1732 -0.0513 0.7500 -0.0946 44.7136 -5.6419 -0.0471 0.7750 -0.0854 46.2041 -5.0927 -0.0427 0.8000 -0.0760 47.6946 -4.5285 -0.0380 0.8250 -0.0663 49.1850 -3.9524 -0.0331 0.8500 -0.0565 50.6755 -3.3688 -0.0280 0.8750 -0.0467 52.1659 -2.7840 -0.0230 0.9000 -0.0370 53.6564 -2.2051 -0.0180 0.9250 -0.0275 55.1468 -1.6381 -0.0132 0.9500 -0.0182 56.6373 -1.0844 -0.0087 0.9750 -0.0091 58.1277 -0.5406 -0.0043 1.0000 0.0000 59.6182 0.0000 0.0000 y= -118.9000 y/(b/2) = -0.7250 chord= 63.8667 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0750 0.0601 0.1750 -0.0022 0.2750 -0.0502 0.3750 -0.0946 0.4750 -0.1410 0.5750 -0.1964 0.6750 -0.2899 0.7750 -0.3501 0.8750 -0.3692 0.9750 -0.3429 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.1677 0.0000 -10.7102 0.0000 0.0250 -0.1692 1.5967 -10.8072 -0.0057 0.0500 -0.1708 3.1933 -10.9068 -0.0115 0.0750 -0.1723 4.7900 -11.0059 -0.0172 0.1000 -0.1737 6.3867 -11.0945 -0.0228 0.1250 -0.1748 7.9833 -11.1620 -0.0280 0.1500 -0.1754 9.5800 -11.2017 -0.0328 0.1750 -0.1756 11.1767 -11.2121 -0.0372 0.2000 -0.1753 12.7733 -11.1964 -0.0412 0.2250 -0.1747 14.3700 -11.1593 -0.0448 0.2500 -0.1739 15.9667 -11.1039 -0.0481 0.2750 -0.1727 17.5633 -11.0320 -0.0512 0.3000 -0.1713 19.1600 -10.9435 -0.0540 0.3250 -0.1697 20.7567 -10.8379 -0.0565 0.3500 -0.1678 22.3533 -10.7143 -0.0588 0.3750 -0.1655 23.9500 -10.5725 -0.0607 0.4000 -0.1630 25.5467 -10.4121 -0.0624 0.4250 -0.1602 27.1433 -10.2330 -0.0638 0.4500 -0.1571 28.7400 -10.0352 -0.0649 0.4750 -0.1537 30.3367 -9.8191 -0.0657 0.5000 -0.1501 31.9333 -9.5850 -0.0662 0.5250 -0.1461 33.5300 -9.3324 -0.0665 0.5500 -0.1418 35.1267 -9.0589 -0.0664 0.5750 -0.1372 36.7234 -8.7599 -0.0659 0.6000 -0.1320 38.3200 -8.4295 -0.0649 0.6250 -0.1262 39.9167 -8.0620 -0.0633 0.6500 -0.1199 41.5134 -7.6553 -0.0612 0.6750 -0.1129 43.1100 -7.2103 -0.0584 0.7000 -0.1054 44.7067 -6.7315 -0.0551 0.7250 -0.0975 46.3034 -6.2245 -0.0513 0.7500 -0.0892 47.9000 -5.6939 -0.0472 0.7750 -0.0805 49.4967 -5.1436 -0.0428 0.8000 -0.0717 51.0934 -4.5767 -0.0381 0.8250 -0.0626 52.6900 -3.9965 -0.0332 0.8500 -0.0534 54.2867 -3.4077 -0.0282 0.8750 -0.0441 55.8834 -2.8167 -0.0231 0.9000 -0.0349 57.4800 -2.2314 -0.0182 0.9250 -0.0260 59.0767 -1.6577 -0.0134 0.9500 -0.0172 60.6734 -1.0974 -0.0088 0.9750 -0.0086 62.2700 -0.5471 -0.0044 1.0000 0.0000 63.8667 0.0000 0.0000 y= -110.7000 y/(b/2) = -0.6750 chord= 68.1152 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0750 0.0757 0.1750 0.0158 0.2750 -0.0307 0.3750 -0.0743 0.4750 -0.1203 0.5750 -0.1757 0.6750 -0.2691 0.7750 -0.3302 0.8750 -0.3510 0.9750 -0.3270 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.1487 0.0000 -10.1318 0.0000 0.0250 -0.1507 1.7029 -10.2618 -0.0056 0.0500 -0.1526 3.4058 -10.3945 -0.0113 0.0750 -0.1545 5.1086 -10.5267 -0.0170 0.1000 -0.1563 6.8115 -10.6482 -0.0225 0.1250 -0.1578 8.5144 -10.7479 -0.0276 0.1500 -0.1588 10.2173 -10.8192 -0.0324 0.1750 -0.1594 11.9202 -10.8604 -0.0367 0.2000 -0.1597 13.6230 -10.8746 -0.0407 0.2250 -0.1595 15.3259 -10.8668 -0.0443 0.2500 -0.1591 17.0288 -10.8401 -0.0476 0.2750 -0.1585 18.7317 -10.7963 -0.0507 0.3000 -0.1576 20.4346 -10.7352 -0.0535 0.3250 -0.1564 22.1374 -10.6562 -0.0560 0.3500 -0.1550 23.8403 -10.5586 -0.0583 0.3750 -0.1533 25.5432 -10.4418 -0.0603 0.4000 -0.1513 27.2461 -10.3054 -0.0620 0.4250 -0.1490 28.9490 -10.1493 -0.0635 0.4500 -0.1464 30.6518 -9.9735 -0.0646 0.4750 -0.1436 32.3547 -9.7782 -0.0655 0.5000 -0.1404 34.0576 -9.5638 -0.0660 0.5250 -0.1370 35.7605 -9.3297 -0.0663 0.5500 -0.1332 37.4634 -9.0732 -0.0663 0.5750 -0.1290 39.1662 -8.7896 -0.0658 0.6000 -0.1244 40.8691 -8.4725 -0.0649 0.6250 -0.1192 42.5720 -8.1161 -0.0634 0.6500 -0.1133 44.2749 -7.7177 -0.0612 0.6750 -0.1069 45.9777 -7.2787 -0.0585 0.7000 -0.0999 47.6806 -6.8033 -0.0553 0.7250 -0.0925 49.3835 -6.2975 -0.0515 0.7500 -0.0847 51.0864 -5.7663 -0.0475 0.7750 -0.0765 52.7893 -5.2136 -0.0431 0.8000 -0.0682 54.4921 -4.6426 -0.0384 0.8250 -0.0596 56.1950 -4.0568 -0.0335 0.8500 -0.0508 57.8979 -3.4612 -0.0285 0.8750 -0.0420 59.6008 -2.8624 -0.0234 0.9000 -0.0333 61.3037 -2.2685 -0.0184 0.9250 -0.0247 63.0065 -1.6858 -0.0136 0.9500 -0.0164 64.7094 -1.1161 -0.0089 0.9750 -0.0082 66.4123 -0.5565 -0.0045 1.0000 0.0000 68.1152 0.0000 0.0000 y= -102.5000 y/(b/2) = -0.6250 chord= 72.3637 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0750 0.0922 0.1750 0.0346 0.2750 -0.0106 0.3750 -0.0534 0.4750 -0.0990 0.5750 -0.1542 0.6750 -0.2470 0.7750 -0.3088 0.8750 -0.3314 0.9750 -0.3101 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.1288 0.0000 -9.3235 0.0000 0.0250 -0.1312 1.8091 -9.4915 -0.0055 0.0500 -0.1335 3.6182 -9.6622 -0.0111 0.0750 -0.1359 5.4273 -9.8323 -0.0167 0.1000 -0.1381 7.2364 -9.9916 -0.0221 0.1250 -0.1400 9.0455 -10.1286 -0.0272 0.1500 -0.1415 10.8546 -10.2365 -0.0319 0.1750 -0.1425 12.6636 -10.3137 -0.0362 0.2000 -0.1432 14.4727 -10.3633 -0.0401 0.2250 -0.1436 16.2818 -10.3901 -0.0437 0.2500 -0.1437 18.0909 -10.3975 -0.0471 0.2750 -0.1435 19.9000 -10.3872 -0.0501 0.3000 -0.1432 21.7091 -10.3589 -0.0530 0.3250 -0.1425 23.5182 -10.3120 -0.0555 0.3500 -0.1416 25.3273 -10.2456 -0.0578 0.3750 -0.1404 27.1364 -10.1592 -0.0599 0.4000 -0.1389 28.9455 -10.0523 -0.0616 0.4250 -0.1371 30.7546 -9.9246 -0.0631 0.4500 -0.1351 32.5637 -9.7762 -0.0642 0.4750 -0.1328 34.3727 -9.6072 -0.0651 0.5000 -0.1301 36.1818 -9.4179 -0.0657 0.5250 -0.1272 37.9909 -9.2077 -0.0660 0.5500 -0.1240 39.8000 -8.9739 -0.0660 0.5750 -0.1204 41.6091 -8.7114 -0.0656 0.6000 -0.1163 43.4182 -8.4135 -0.0647 0.6250 -0.1116 45.2273 -8.0740 -0.0633 0.6500 -0.1063 47.0364 -7.6905 -0.0612 0.6750 -0.1004 48.8455 -7.2638 -0.0585 0.7000 -0.0940 50.6546 -6.7987 -0.0553 0.7250 -0.0871 52.4637 -6.3010 -0.0516 0.7500 -0.0798 54.2728 -5.7760 -0.0476 0.7750 -0.0722 56.0819 -5.2277 -0.0433 0.8000 -0.0644 57.8909 -4.6596 -0.0386 0.8250 -0.0563 59.7000 -4.0751 -0.0338 0.8500 -0.0481 61.5091 -3.4795 -0.0288 0.8750 -0.0398 63.3182 -2.8795 -0.0237 0.9000 -0.0316 65.1273 -2.2834 -0.0187 0.9250 -0.0235 66.9364 -1.6976 -0.0138 0.9500 -0.0155 68.7455 -1.1243 -0.0091 0.9750 -0.0077 70.5546 -0.5606 -0.0045 1.0000 0.0000 72.3637 0.0000 0.0000 y= -94.3000 y/(b/2) = -0.5750 chord= 76.6122 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0750 0.1114 0.1750 0.0558 0.2750 0.0116 0.3750 -0.0308 0.4750 -0.0764 0.5750 -0.1316 0.6750 -0.2238 0.7750 -0.2864 0.8750 -0.3110 0.9750 -0.2930 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.1074 0.0000 -8.2301 0.0000 0.0250 -0.1102 1.9153 -8.4447 -0.0055 0.0500 -0.1131 3.8306 -8.6621 -0.0110 0.0750 -0.1159 5.7459 -8.8789 -0.0165 0.1000 -0.1186 7.6612 -9.0846 -0.0219 0.1250 -0.1210 9.5765 -9.2676 -0.0270 0.1500 -0.1230 11.4918 -9.4209 -0.0317 0.1750 -0.1246 13.4071 -9.5428 -0.0359 0.2000 -0.1258 15.3224 -9.6364 -0.0398 0.2250 -0.1267 17.2377 -9.7065 -0.0434 0.2500 -0.1273 19.1530 -9.7565 -0.0468 0.2750 -0.1278 21.0684 -9.7879 -0.0499 0.3000 -0.1279 22.9837 -9.8007 -0.0527 0.3250 -0.1278 24.8990 -9.7939 -0.0553 0.3500 -0.1275 26.8143 -9.7666 -0.0577 0.3750 -0.1269 28.7296 -9.7183 -0.0597 0.4000 -0.1259 30.6449 -9.6484 -0.0615 0.4250 -0.1247 32.5602 -9.5566 -0.0630 0.4500 -0.1233 34.4755 -9.4429 -0.0642 0.4750 -0.1215 36.3908 -9.3073 -0.0651 0.5000 -0.1194 38.3061 -9.1503 -0.0657 0.5250 -0.1171 40.2214 -8.9710 -0.0661 0.5500 -0.1144 42.1367 -8.7665 -0.0661 0.5750 -0.1114 44.0520 -8.5318 -0.0657 0.6000 -0.1078 45.9673 -8.2598 -0.0648 0.6250 -0.1037 47.8826 -7.9442 -0.0634 0.6500 -0.0990 49.7979 -7.5823 -0.0614 0.6750 -0.0937 51.7132 -7.1750 -0.0587 0.7000 -0.0878 53.6285 -6.7270 -0.0556 0.7250 -0.0815 55.5438 -6.2443 -0.0520 0.7500 -0.0748 57.4591 -5.7323 -0.0480 0.7750 -0.0678 59.3744 -5.1951 -0.0436 0.8000 -0.0605 61.2898 -4.6363 -0.0390 0.8250 -0.0530 63.2051 -4.0594 -0.0342 0.8500 -0.0453 65.1204 -3.4698 -0.0292 0.8750 -0.0375 67.0357 -2.8744 -0.0241 0.9000 -0.0298 68.9510 -2.2812 -0.0190 0.9250 -0.0222 70.8663 -1.6972 -0.0141 0.9500 -0.0147 72.7816 -1.1245 -0.0093 0.9750 -0.0073 74.6969 -0.5608 -0.0046 1.0000 0.0000 76.6122 0.0000 0.0000 y= -86.1000 y/(b/2) = -0.5250 chord= 80.8607 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0750 0.1364 0.1750 0.0826 0.2750 0.0389 0.3750 -0.0036 0.4750 -0.0495 0.5750 -0.1051 0.6750 -0.1967 0.7750 -0.2604 0.8750 -0.2877 0.9750 -0.2736 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0817 0.0000 -6.6089 0.0000 0.0250 -0.0852 2.0215 -6.8859 -0.0055 0.0500 -0.0886 4.0430 -7.1657 -0.0110 0.0750 -0.0921 6.0646 -7.4449 -0.0165 0.1000 -0.0954 8.0861 -7.7129 -0.0218 0.1250 -0.0984 10.1076 -7.9576 -0.0269 0.1500 -0.1011 12.1291 -8.1721 -0.0316 0.1750 -0.1033 14.1506 -8.3545 -0.0359 0.2000 -0.1052 16.1721 -8.5077 -0.0398 0.2250 -0.1068 18.1937 -8.6366 -0.0435 0.2500 -0.1081 20.2152 -8.7444 -0.0468 0.2750 -0.1092 22.2367 -8.8326 -0.0500 0.3000 -0.1101 24.2582 -8.9012 -0.0529 0.3250 -0.1107 26.2797 -8.9491 -0.0555 0.3500 -0.1110 28.3012 -8.9754 -0.0579 0.3750 -0.1110 30.3228 -8.9794 -0.0600 0.4000 -0.1108 32.3443 -8.9606 -0.0618 0.4250 -0.1103 34.3658 -8.9186 -0.0633 0.4500 -0.1095 36.3873 -8.8533 -0.0645 0.4750 -0.1084 38.4088 -8.7647 -0.0655 0.5000 -0.1070 40.4304 -8.6531 -0.0661 0.5250 -0.1053 42.4519 -8.5177 -0.0665 0.5500 -0.1033 44.4734 -8.3556 -0.0666 0.5750 -0.1009 46.4949 -8.1615 -0.0662 0.6000 -0.0980 48.5164 -7.9282 -0.0654 0.6250 -0.0946 50.5379 -7.6491 -0.0639 0.6500 -0.0905 52.5595 -7.3216 -0.0619 0.6750 -0.0859 54.5810 -6.9464 -0.0593 0.7000 -0.0807 56.6025 -6.5282 -0.0562 0.7250 -0.0751 58.6240 -6.0732 -0.0526 0.7500 -0.0691 60.6455 -5.5865 -0.0487 0.7750 -0.0627 62.6670 -5.0725 -0.0443 0.8000 -0.0561 64.6886 -4.5347 -0.0397 0.8250 -0.0492 66.7101 -3.9770 -0.0349 0.8500 -0.0421 68.7316 -3.4045 -0.0298 0.8750 -0.0349 70.7531 -2.8242 -0.0247 0.9000 -0.0278 72.7746 -2.2442 -0.0196 0.9250 -0.0207 74.7962 -1.6712 -0.0145 0.9500 -0.0137 76.8177 -1.1080 -0.0096 0.9750 -0.0068 78.8392 -0.5527 -0.0048 1.0000 0.0000 80.8607 0.0000 0.0000 y= -77.9000 y/(b/2) = -0.4750 chord= 85.1092 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0750 0.1694 0.1750 0.1168 0.2750 0.0730 0.3750 0.0299 0.4750 -0.0169 0.5750 -0.0733 0.6750 -0.1646 0.7750 -0.2300 0.8750 -0.2607 0.9750 -0.2513 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0503 0.0000 -4.2852 0.0000 0.0250 -0.0546 2.1277 -4.6469 -0.0055 0.0500 -0.0589 4.2555 -5.0115 -0.0111 0.0750 -0.0632 6.3832 -5.3756 -0.0166 0.1000 -0.0673 8.5109 -5.7281 -0.0220 0.1250 -0.0712 10.6386 -6.0568 -0.0271 0.1500 -0.0747 12.7664 -6.3544 -0.0319 0.1750 -0.0778 14.8941 -6.6189 -0.0362 0.2000 -0.0805 17.0218 -6.8531 -0.0402 0.2250 -0.0830 19.1496 -7.0619 -0.0440 0.2500 -0.0852 21.2773 -7.2484 -0.0474 0.2750 -0.0871 23.4050 -7.4141 -0.0506 0.3000 -0.0888 25.5327 -7.5587 -0.0536 0.3250 -0.0903 27.6605 -7.6813 -0.0563 0.3500 -0.0914 29.7882 -7.7808 -0.0587 0.3750 -0.0923 31.9159 -7.8565 -0.0608 0.4000 -0.0929 34.0437 -7.9077 -0.0627 0.4250 -0.0932 36.1714 -7.9341 -0.0643 0.4500 -0.0932 38.2991 -7.9355 -0.0655 0.4750 -0.0930 40.4269 -7.9120 -0.0665 0.5000 -0.0924 42.5546 -7.8636 -0.0672 0.5250 -0.0915 44.6823 -7.7896 -0.0676 0.5500 -0.0903 46.8100 -7.6869 -0.0677 0.5750 -0.0887 48.9378 -7.5502 -0.0673 0.6000 -0.0866 51.0655 -7.3723 -0.0665 0.6250 -0.0840 53.1932 -7.1465 -0.0651 0.6500 -0.0807 55.3210 -6.8700 -0.0631 0.6750 -0.0769 57.4487 -6.5435 -0.0605 0.7000 -0.0725 59.5764 -6.1715 -0.0574 0.7250 -0.0677 61.7041 -5.7601 -0.0538 0.7500 -0.0624 63.8319 -5.3144 -0.0499 0.7750 -0.0569 65.9596 -4.8389 -0.0455 0.8000 -0.0510 68.0873 -4.3370 -0.0409 0.8250 -0.0448 70.2151 -3.8126 -0.0360 0.8500 -0.0384 72.3428 -3.2710 -0.0309 0.8750 -0.0319 74.4705 -2.7190 -0.0257 0.9000 -0.0254 76.5982 -2.1644 -0.0204 0.9250 -0.0190 78.7260 -1.6142 -0.0152 0.9500 -0.0126 80.8537 -1.0712 -0.0101 0.9750 -0.0063 82.9814 -0.5345 -0.0050 1.0000 0.0000 85.1092 0.0000 0.0000 y= -69.5500 y/(b/2) = -0.4241 chord= 89.4354 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0750 0.1821 0.1750 0.1344 0.2750 0.0943 0.3750 0.0543 0.4750 0.0104 0.5750 -0.0430 0.6750 -0.1296 0.7750 -0.1937 0.8750 -0.2262 0.9750 -0.2213 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0238 0.0000 -2.1326 0.0000 0.0250 -0.0284 2.2359 -2.5408 -0.0052 0.0500 -0.0330 4.4718 -2.9517 -0.0104 0.0750 -0.0376 6.7077 -3.3621 -0.0155 0.1000 -0.0421 8.9435 -3.7615 -0.0206 0.1250 -0.0463 11.1794 -4.1383 -0.0254 0.1500 -0.0502 13.4153 -4.4856 -0.0299 0.1750 -0.0537 15.6512 -4.8013 -0.0340 0.2000 -0.0569 17.8871 -5.0882 -0.0378 0.2250 -0.0598 20.1230 -5.3506 -0.0413 0.2500 -0.0625 22.3588 -5.5915 -0.0446 0.2750 -0.0650 24.5947 -5.8124 -0.0477 0.3000 -0.0672 26.8306 -6.0128 -0.0505 0.3250 -0.0692 29.0665 -6.1917 -0.0531 0.3500 -0.0710 31.3024 -6.3482 -0.0555 0.3750 -0.0725 33.5383 -6.4814 -0.0576 0.4000 -0.0737 35.7742 -6.5906 -0.0594 0.4250 -0.0746 38.0100 -6.6755 -0.0609 0.4500 -0.0753 40.2459 -6.7356 -0.0622 0.4750 -0.0757 42.4818 -6.7711 -0.0632 0.5000 -0.0758 44.7177 -6.7820 -0.0639 0.5250 -0.0757 46.9536 -6.7673 -0.0643 0.5500 -0.0752 49.1895 -6.7241 -0.0645 0.5750 -0.0743 51.4253 -6.6471 -0.0642 0.6000 -0.0730 53.6612 -6.5291 -0.0635 0.6250 -0.0712 55.8971 -6.3636 -0.0622 0.6500 -0.0687 58.1330 -6.1475 -0.0604 0.6750 -0.0658 60.3689 -5.8815 -0.0580 0.7000 -0.0623 62.6048 -5.5697 -0.0551 0.7250 -0.0583 64.8407 -5.2176 -0.0518 0.7500 -0.0540 67.0765 -4.8302 -0.0480 0.7750 -0.0493 69.3124 -4.4116 -0.0440 0.8000 -0.0443 71.5483 -3.9652 -0.0396 0.8250 -0.0391 73.7842 -3.4949 -0.0349 0.8500 -0.0336 76.0201 -3.0056 -0.0300 0.8750 -0.0280 78.2560 -2.5037 -0.0250 0.9000 -0.0223 80.4918 -1.9968 -0.0199 0.9250 -0.0167 82.7277 -1.4914 -0.0149 0.9500 -0.0111 84.9636 -0.9907 -0.0099 0.9750 -0.0055 87.1995 -0.4945 -0.0049 1.0000 0.0000 89.4354 0.0000 0.0000 y= -61.2000 y/(b/2) = -0.3732 chord= 93.7616 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0750 0.0810 0.1750 0.0502 0.2750 0.0257 0.3750 0.0006 0.4750 -0.0285 0.5750 -0.0668 0.6750 -0.1361 0.7750 -0.1883 0.8750 -0.2154 0.9750 -0.2114 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0617 0.0000 -5.7807 0.0000 0.0250 -0.0637 2.3440 -5.9712 -0.0036 0.0500 -0.0657 4.6881 -6.1637 -0.0072 0.0750 -0.0678 7.0321 -6.3558 -0.0108 0.1000 -0.0698 9.3762 -6.5403 -0.0143 0.1250 -0.0716 11.7202 -6.7095 -0.0176 0.1500 -0.0731 14.0642 -6.8586 -0.0207 0.1750 -0.0745 16.4083 -6.9865 -0.0237 0.2000 -0.0757 18.7523 -7.0953 -0.0264 0.2250 -0.0767 21.0964 -7.1883 -0.0289 0.2500 -0.0775 23.4404 -7.2676 -0.0313 0.2750 -0.0782 25.7844 -7.3342 -0.0335 0.3000 -0.0788 28.1285 -7.3878 -0.0356 0.3250 -0.0792 30.4725 -7.4276 -0.0376 0.3500 -0.0795 32.8166 -7.4526 -0.0394 0.3750 -0.0796 35.1606 -7.4621 -0.0411 0.4000 -0.0795 37.5046 -7.4554 -0.0425 0.4250 -0.0793 39.8487 -7.4319 -0.0438 0.4500 -0.0788 42.1927 -7.3911 -0.0449 0.4750 -0.0782 44.5368 -7.3331 -0.0458 0.5000 -0.0774 46.8808 -7.2576 -0.0466 0.5250 -0.0764 49.2248 -7.1639 -0.0471 0.5500 -0.0752 51.5689 -7.0488 -0.0474 0.5750 -0.0737 53.9129 -6.9075 -0.0475 0.6000 -0.0718 56.2570 -6.7330 -0.0471 0.6250 -0.0695 58.6010 -6.5192 -0.0464 0.6500 -0.0668 60.9450 -6.2628 -0.0452 0.6750 -0.0636 63.2891 -5.9641 -0.0436 0.7000 -0.0600 65.6331 -5.6264 -0.0415 0.7250 -0.0560 67.9772 -5.2544 -0.0391 0.7500 -0.0517 70.3212 -4.8521 -0.0363 0.7750 -0.0472 72.6653 -4.4231 -0.0333 0.8000 -0.0423 75.0093 -3.9700 -0.0300 0.8250 -0.0373 77.3533 -3.4961 -0.0265 0.8500 -0.0321 79.6974 -3.0056 -0.0228 0.8750 -0.0267 82.0414 -2.5040 -0.0190 0.9000 -0.0213 84.3855 -1.9979 -0.0151 0.9250 -0.0159 86.7295 -1.4930 -0.0113 0.9500 -0.0106 89.0735 -0.9922 -0.0075 0.9750 -0.0053 91.4176 -0.4954 -0.0037 1.0000 0.0000 93.7616 0.0000 0.0000 y= -53.0000 y/(b/2) = -0.3232 chord= 98.0101 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0750 0.0099 0.1750 -0.0063 0.2750 -0.0180 0.3750 -0.0308 0.4750 -0.0479 0.5750 -0.0738 0.6750 -0.1276 0.7750 -0.1686 0.8750 -0.1896 0.9750 -0.1853 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0790 0.0000 -7.7392 0.0000 0.0250 -0.0792 2.4503 -7.7638 -0.0022 0.0500 -0.0795 4.9005 -7.7895 -0.0045 0.0750 -0.0797 7.3508 -7.8150 -0.0067 0.1000 -0.0800 9.8010 -7.8363 -0.0089 0.1250 -0.0801 12.2513 -7.8489 -0.0110 0.1500 -0.0801 14.7015 -7.8505 -0.0130 0.1750 -0.0800 17.1518 -7.8405 -0.0149 0.2000 -0.0798 19.6020 -7.8204 -0.0166 0.2250 -0.0795 22.0523 -7.7922 -0.0183 0.2500 -0.0791 24.5025 -7.7574 -0.0199 0.2750 -0.0787 26.9528 -7.7163 -0.0215 0.3000 -0.0782 29.4030 -7.6689 -0.0230 0.3250 -0.0777 31.8533 -7.6144 -0.0244 0.3500 -0.0771 34.3035 -7.5520 -0.0257 0.3750 -0.0763 36.7538 -7.4810 -0.0270 0.4000 -0.0755 39.2040 -7.4007 -0.0281 0.4250 -0.0746 41.6543 -7.3102 -0.0292 0.4500 -0.0736 44.1045 -7.2092 -0.0301 0.4750 -0.0724 46.5548 -7.0974 -0.0310 0.5000 -0.0712 49.0050 -6.9746 -0.0317 0.5250 -0.0698 51.4553 -6.8398 -0.0323 0.5500 -0.0683 53.9055 -6.6902 -0.0327 0.5750 -0.0665 56.3558 -6.5211 -0.0330 0.6000 -0.0645 58.8060 -6.3263 -0.0330 0.6250 -0.0622 61.2563 -6.0997 -0.0326 0.6500 -0.0596 63.7065 -5.8385 -0.0319 0.6750 -0.0565 66.1568 -5.5424 -0.0309 0.7000 -0.0532 68.6070 -5.2143 -0.0295 0.7250 -0.0496 71.0573 -4.8580 -0.0279 0.7500 -0.0457 73.5075 -4.4770 -0.0259 0.7750 -0.0416 75.9578 -4.0741 -0.0238 0.8000 -0.0373 78.4080 -3.6515 -0.0215 0.8250 -0.0328 80.8583 -3.2118 -0.0190 0.8500 -0.0281 83.3085 -2.7585 -0.0163 0.8750 -0.0234 85.7588 -2.2964 -0.0136 0.9000 -0.0187 88.2091 -1.8313 -0.0108 0.9250 -0.0140 90.6593 -1.3680 -0.0080 0.9500 -0.0093 93.1096 -0.9089 -0.0053 0.9750 -0.0046 95.5598 -0.4538 -0.0027 1.0000 0.0000 98.0101 0.0000 0.0000 y= -44.8000 y/(b/2) = -0.2732 chord= 102.2586 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0750 -0.0187 0.1750 -0.0266 0.2750 -0.0319 0.3750 -0.0387 0.4750 -0.0498 0.5750 -0.0692 0.6750 -0.1136 0.7750 -0.1475 0.8750 -0.1650 0.9750 -0.1611 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0787 0.0000 -8.0451 0.0000 0.0250 -0.0782 2.5565 -7.9976 -0.0015 0.0500 -0.0778 5.1129 -7.9506 -0.0030 0.0750 -0.0773 7.6694 -7.9035 -0.0045 0.1000 -0.0768 10.2259 -7.8542 -0.0060 0.1250 -0.0763 12.7823 -7.8005 -0.0074 0.1500 -0.0757 15.3388 -7.7410 -0.0088 0.1750 -0.0751 17.8953 -7.6757 -0.0102 0.2000 -0.0744 20.4517 -7.6054 -0.0114 0.2250 -0.0736 23.0082 -7.5313 -0.0127 0.2500 -0.0729 25.5646 -7.4541 -0.0139 0.2750 -0.0721 28.1211 -7.3740 -0.0151 0.3000 -0.0713 30.6776 -7.2907 -0.0162 0.3250 -0.0704 33.2340 -7.2039 -0.0173 0.3500 -0.0696 35.7905 -7.1127 -0.0184 0.3750 -0.0686 38.3470 -7.0164 -0.0194 0.4000 -0.0676 40.9034 -6.9143 -0.0204 0.4250 -0.0666 43.4599 -6.8056 -0.0213 0.4500 -0.0654 46.0164 -6.6897 -0.0221 0.4750 -0.0642 48.5728 -6.5663 -0.0229 0.5000 -0.0629 51.1293 -6.4352 -0.0236 0.5250 -0.0616 53.6858 -6.2952 -0.0242 0.5500 -0.0601 56.2422 -6.1439 -0.0247 0.5750 -0.0584 58.7987 -5.9767 -0.0250 0.6000 -0.0566 61.3551 -5.7879 -0.0251 0.6250 -0.0545 63.9116 -5.5720 -0.0250 0.6500 -0.0521 66.4681 -5.3261 -0.0245 0.6750 -0.0494 69.0245 -5.0501 -0.0238 0.7000 -0.0464 71.5810 -4.7463 -0.0228 0.7250 -0.0432 74.1375 -4.4182 -0.0216 0.7500 -0.0398 76.6939 -4.0688 -0.0201 0.7750 -0.0362 79.2504 -3.7005 -0.0185 0.8000 -0.0324 81.8069 -3.3152 -0.0167 0.8250 -0.0285 84.3633 -2.9151 -0.0147 0.8500 -0.0245 86.9198 -2.5031 -0.0127 0.8750 -0.0204 89.4763 -2.0836 -0.0105 0.9000 -0.0162 92.0327 -1.6615 -0.0084 0.9250 -0.0121 94.5892 -1.2411 -0.0062 0.9500 -0.0081 97.1456 -0.8247 -0.0041 0.9750 -0.0040 99.7021 -0.4117 -0.0021 1.0000 0.0000 102.2586 0.0000 0.0000 y= -37.3500 y/(b/2) = -0.2277 chord= 106.1185 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0750 -0.0193 0.1750 -0.0219 0.2750 -0.0238 0.3750 -0.0282 0.4750 -0.0373 0.5750 -0.0546 0.6750 -0.0947 0.7750 -0.1267 0.8750 -0.1444 0.9750 -0.1430 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0663 0.0000 -7.0368 0.0000 0.0250 -0.0658 2.6530 -6.9858 -0.0012 0.0500 -0.0654 5.3059 -6.9349 -0.0024 0.0750 -0.0649 7.9589 -6.8840 -0.0035 0.1000 -0.0644 10.6119 -6.8323 -0.0047 0.1250 -0.0639 13.2648 -6.7791 -0.0059 0.1500 -0.0634 15.9178 -6.7240 -0.0070 0.1750 -0.0628 18.5707 -6.6668 -0.0081 0.2000 -0.0623 21.2237 -6.6080 -0.0092 0.2250 -0.0617 23.8767 -6.5479 -0.0103 0.2500 -0.0611 26.5296 -6.4867 -0.0114 0.2750 -0.0605 29.1826 -6.4242 -0.0125 0.3000 -0.0599 31.8356 -6.3602 -0.0135 0.3250 -0.0593 34.4885 -6.2939 -0.0146 0.3500 -0.0587 37.1415 -6.2248 -0.0156 0.3750 -0.0580 39.7944 -6.1520 -0.0165 0.4000 -0.0572 42.4474 -6.0747 -0.0175 0.4250 -0.0565 45.1004 -5.9919 -0.0183 0.4500 -0.0556 47.7533 -5.9029 -0.0192 0.4750 -0.0547 50.4063 -5.8073 -0.0199 0.5000 -0.0538 53.0593 -5.7048 -0.0206 0.5250 -0.0527 55.7122 -5.5942 -0.0212 0.5500 -0.0516 58.3652 -5.4730 -0.0217 0.5750 -0.0503 61.0182 -5.3372 -0.0221 0.6000 -0.0488 63.6711 -5.1812 -0.0223 0.6250 -0.0471 66.3241 -5.0000 -0.0223 0.6500 -0.0451 68.9770 -4.7908 -0.0219 0.6750 -0.0429 71.6300 -4.5531 -0.0214 0.7000 -0.0404 74.2830 -4.2891 -0.0205 0.7250 -0.0377 76.9359 -4.0015 -0.0195 0.7500 -0.0348 79.5889 -3.6930 -0.0182 0.7750 -0.0317 82.2419 -3.3658 -0.0168 0.8000 -0.0285 84.8948 -3.0214 -0.0152 0.8250 -0.0251 87.5478 -2.6620 -0.0135 0.8500 -0.0216 90.2007 -2.2903 -0.0116 0.8750 -0.0180 92.8537 -1.9100 -0.0097 0.9000 -0.0144 95.5067 -1.5257 -0.0077 0.9250 -0.0108 98.1596 -1.1414 -0.0058 0.9500 -0.0072 100.8126 -0.7591 -0.0038 0.9750 -0.0036 103.4656 -0.3791 -0.0019 1.0000 0.0000 106.1185 0.0000 0.0000 y= -29.9000 y/(b/2) = -0.1823 chord= 111.9969 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0750 -0.0367 0.1750 -0.0353 0.2750 -0.0331 0.3750 -0.0332 0.4750 -0.0379 0.5750 -0.0505 0.6750 -0.0833 0.7750 -0.1119 0.8750 -0.1299 0.9750 -0.1318 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0660 0.0000 -7.3892 0.0000 0.0250 -0.0651 2.7999 -7.2866 -0.0007 0.0500 -0.0641 5.5998 -7.1838 -0.0015 0.0750 -0.0632 8.3998 -7.0811 -0.0022 0.1000 -0.0623 11.1997 -6.9787 -0.0029 0.1250 -0.0614 13.9996 -6.8769 -0.0037 0.1500 -0.0605 16.7995 -6.7761 -0.0044 0.1750 -0.0596 19.5995 -6.6765 -0.0052 0.2000 -0.0587 22.3994 -6.5785 -0.0060 0.2250 -0.0579 25.1993 -6.4820 -0.0067 0.2500 -0.0570 27.9992 -6.3872 -0.0075 0.2750 -0.0562 30.7992 -6.2938 -0.0084 0.3000 -0.0554 33.5991 -6.2015 -0.0092 0.3250 -0.0546 36.3990 -6.1099 -0.0100 0.3500 -0.0537 39.1989 -6.0184 -0.0109 0.3750 -0.0529 41.9988 -5.9260 -0.0117 0.4000 -0.0521 44.7988 -5.8320 -0.0125 0.4250 -0.0512 47.5987 -5.7355 -0.0133 0.4500 -0.0503 50.3986 -5.6356 -0.0140 0.4750 -0.0494 53.1985 -5.5317 -0.0148 0.5000 -0.0484 55.9985 -5.4232 -0.0154 0.5250 -0.0474 58.7984 -5.3091 -0.0161 0.5500 -0.0463 61.5983 -5.1869 -0.0166 0.5750 -0.0451 64.3982 -5.0529 -0.0171 0.6000 -0.0438 67.1982 -4.9022 -0.0174 0.6250 -0.0422 69.9981 -4.7302 -0.0175 0.6500 -0.0405 72.7980 -4.5340 -0.0174 0.6750 -0.0385 75.5979 -4.3131 -0.0171 0.7000 -0.0363 78.3979 -4.0685 -0.0165 0.7250 -0.0339 81.1978 -3.8021 -0.0158 0.7500 -0.0314 83.9977 -3.5159 -0.0149 0.7750 -0.0287 86.7976 -3.2114 -0.0138 0.8000 -0.0258 89.5975 -2.8898 -0.0126 0.8250 -0.0228 92.3975 -2.5529 -0.0112 0.8500 -0.0197 95.1974 -2.2030 -0.0098 0.8750 -0.0165 97.9973 -1.8430 -0.0082 0.9000 -0.0132 100.7972 -1.4767 -0.0066 0.9250 -0.0099 103.5972 -1.1077 -0.0049 0.9500 -0.0066 106.3971 -0.7381 -0.0033 0.9750 -0.0033 109.1970 -0.3689 -0.0016 1.0000 0.0000 111.9969 0.0000 0.0000 y= -22.9000 y/(b/2) = -0.1396 chord= 119.0698 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0750 -0.0463 0.1750 -0.0412 0.2750 -0.0346 0.3750 -0.0296 0.4750 -0.0280 0.5750 -0.0330 0.6750 -0.0558 0.7750 -0.0803 0.8750 -0.1007 0.9750 -0.1104 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0544 0.0000 -6.4741 0.0000 0.0250 -0.0532 2.9767 -6.3362 -0.0002 0.0500 -0.0521 5.9535 -6.1978 -0.0004 0.0750 -0.0509 8.9302 -6.0595 -0.0006 0.1000 -0.0497 11.9070 -5.9227 -0.0008 0.1250 -0.0486 14.8837 -5.7887 -0.0010 0.1500 -0.0475 17.8605 -5.6589 -0.0013 0.1750 -0.0465 20.8372 -5.5338 -0.0016 0.2000 -0.0455 23.8140 -5.4137 -0.0020 0.2250 -0.0445 26.7907 -5.2986 -0.0024 0.2500 -0.0436 29.7675 -5.1884 -0.0028 0.2750 -0.0427 32.7442 -5.0830 -0.0033 0.3000 -0.0418 35.7209 -4.9822 -0.0038 0.3250 -0.0410 38.6977 -4.8857 -0.0043 0.3500 -0.0403 41.6744 -4.7930 -0.0049 0.3750 -0.0395 44.6512 -4.7036 -0.0055 0.4000 -0.0388 47.6279 -4.6167 -0.0061 0.4250 -0.0381 50.6047 -4.5315 -0.0068 0.4500 -0.0374 53.5814 -4.4474 -0.0074 0.4750 -0.0366 56.5582 -4.3639 -0.0081 0.5000 -0.0359 59.5349 -4.2804 -0.0088 0.5250 -0.0352 62.5117 -4.1961 -0.0094 0.5500 -0.0345 65.4884 -4.1086 -0.0100 0.5750 -0.0337 68.4651 -4.0149 -0.0106 0.6000 -0.0328 71.4419 -3.9105 -0.0111 0.6250 -0.0318 74.4186 -3.7912 -0.0115 0.6500 -0.0307 77.3954 -3.6542 -0.0117 0.6750 -0.0294 80.3721 -3.4979 -0.0117 0.7000 -0.0279 83.3489 -3.3222 -0.0116 0.7250 -0.0263 86.3256 -3.1277 -0.0113 0.7500 -0.0245 89.3024 -2.9150 -0.0109 0.7750 -0.0225 92.2791 -2.6847 -0.0103 0.8000 -0.0205 95.2559 -2.4372 -0.0096 0.8250 -0.0183 98.2326 -2.1733 -0.0087 0.8500 -0.0159 101.2093 -1.8940 -0.0078 0.8750 -0.0134 104.1861 -1.6006 -0.0066 0.9000 -0.0109 107.1628 -1.2950 -0.0054 0.9250 -0.0082 110.1396 -0.9794 -0.0041 0.9500 -0.0055 113.1163 -0.6562 -0.0028 0.9750 -0.0028 116.0931 -0.3287 -0.0014 1.0000 0.0000 119.0698 0.0000 0.0000 y= -15.9000 y/(b/2) = -0.0970 chord= 122.0000 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0750 -0.0491 0.1750 -0.0460 0.2750 -0.0416 0.3750 -0.0388 0.4750 -0.0397 0.5750 -0.0466 0.6750 -0.0674 0.7750 -0.0879 0.8750 -0.1036 0.9750 -0.1099 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0615 0.0000 -7.5069 0.0000 0.0250 -0.0603 3.0500 -7.3571 -0.0003 0.0500 -0.0591 6.1000 -7.2071 -0.0006 0.0750 -0.0578 9.1500 -7.0572 -0.0009 0.1000 -0.0566 12.2000 -6.9080 -0.0012 0.1250 -0.0554 15.2500 -6.7607 -0.0016 0.1500 -0.0542 18.3000 -6.6158 -0.0019 0.1750 -0.0531 21.3500 -6.4739 -0.0023 0.2000 -0.0519 24.4000 -6.3353 -0.0027 0.2250 -0.0508 27.4500 -6.2002 -0.0031 0.2500 -0.0497 30.5000 -6.0686 -0.0036 0.2750 -0.0487 33.5500 -5.9403 -0.0041 0.3000 -0.0477 36.6000 -5.8150 -0.0046 0.3250 -0.0467 39.6500 -5.6924 -0.0051 0.3500 -0.0457 42.7000 -5.5720 -0.0057 0.3750 -0.0447 45.7500 -5.4530 -0.0062 0.4000 -0.0437 48.8000 -5.3349 -0.0068 0.4250 -0.0428 51.8500 -5.2167 -0.0074 0.4500 -0.0418 54.9000 -5.0978 -0.0079 0.4750 -0.0408 57.9500 -4.9776 -0.0085 0.5000 -0.0398 61.0000 -4.8554 -0.0090 0.5250 -0.0388 64.0500 -4.7304 -0.0095 0.5500 -0.0377 67.1000 -4.6005 -0.0100 0.5750 -0.0366 70.1500 -4.4632 -0.0104 0.6000 -0.0354 73.2000 -4.3149 -0.0108 0.6250 -0.0340 76.2500 -4.1522 -0.0110 0.6500 -0.0326 79.3000 -3.9729 -0.0110 0.6750 -0.0310 82.3500 -3.7762 -0.0110 0.7000 -0.0292 85.4000 -3.5622 -0.0107 0.7250 -0.0273 88.4500 -3.3317 -0.0104 0.7500 -0.0253 91.5000 -3.0856 -0.0099 0.7750 -0.0232 94.5500 -2.8246 -0.0093 0.8000 -0.0209 97.6000 -2.5494 -0.0086 0.8250 -0.0185 100.6500 -2.2609 -0.0078 0.8500 -0.0161 103.7000 -1.9603 -0.0068 0.8750 -0.0135 106.7500 -1.6491 -0.0058 0.9000 -0.0109 109.8000 -1.3290 -0.0047 0.9250 -0.0082 112.8500 -1.0019 -0.0036 0.9500 -0.0055 115.9000 -0.6700 -0.0024 0.9750 -0.0027 118.9500 -0.3354 -0.0012 1.0000 0.0000 122.0000 0.0000 0.0000 y= -5.9000 y/(b/2) = -0.0360 chord= 122.0000 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0750 -0.0501 0.1750 -0.0505 0.2750 -0.0495 0.3750 -0.0500 0.4750 -0.0537 0.5750 -0.0623 0.6750 -0.0814 0.7750 -0.0975 0.8750 -0.1077 0.9750 -0.1097 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0697 0.0000 -8.5090 0.0000 0.0250 -0.0685 3.0500 -8.3562 -0.0005 0.0500 -0.0672 6.1000 -8.2034 -0.0010 0.0750 -0.0660 9.1500 -8.0506 -0.0015 0.1000 -0.0647 12.2000 -7.8975 -0.0020 0.1250 -0.0635 15.2500 -7.7440 -0.0024 0.1500 -0.0622 18.3000 -7.5900 -0.0029 0.1750 -0.0609 21.3500 -7.4358 -0.0034 0.2000 -0.0597 24.4000 -7.2818 -0.0039 0.2250 -0.0584 27.4500 -7.1286 -0.0044 0.2500 -0.0572 30.5000 -6.9763 -0.0049 0.2750 -0.0559 33.5500 -6.8249 -0.0054 0.3000 -0.0547 36.6000 -6.6742 -0.0059 0.3250 -0.0535 39.6500 -6.5237 -0.0064 0.3500 -0.0522 42.7000 -6.3728 -0.0069 0.3750 -0.0510 45.7500 -6.2210 -0.0074 0.4000 -0.0497 48.8000 -6.0676 -0.0079 0.4250 -0.0485 51.8500 -5.9121 -0.0084 0.4500 -0.0472 54.9000 -5.7537 -0.0088 0.4750 -0.0458 57.9500 -5.5919 -0.0092 0.5000 -0.0445 61.0000 -5.4262 -0.0096 0.5250 -0.0431 64.0500 -5.2558 -0.0100 0.5500 -0.0416 67.1000 -5.0791 -0.0102 0.5750 -0.0401 70.1500 -4.8940 -0.0105 0.6000 -0.0385 73.2000 -4.6978 -0.0106 0.6250 -0.0368 76.2500 -4.4878 -0.0106 0.6500 -0.0349 79.3000 -4.2627 -0.0105 0.6750 -0.0330 82.3500 -4.0221 -0.0103 0.7000 -0.0309 85.4000 -3.7669 -0.0100 0.7250 -0.0287 88.4500 -3.4982 -0.0095 0.7500 -0.0264 91.5000 -3.2174 -0.0089 0.7750 -0.0240 94.5500 -2.9253 -0.0083 0.8000 -0.0215 97.6000 -2.6231 -0.0076 0.8250 -0.0189 100.6500 -2.3115 -0.0067 0.8500 -0.0163 103.7000 -1.9920 -0.0059 0.8750 -0.0137 106.7500 -1.6662 -0.0049 0.9000 -0.0110 109.8000 -1.3359 -0.0040 0.9250 -0.0082 112.8500 -1.0031 -0.0030 0.9500 -0.0055 115.9000 -0.6690 -0.0020 0.9750 -0.0027 118.9500 -0.3345 -0.0010 1.0000 0.0000 122.0000 0.0000 0.0000 twist table i y y/(b/2) twist 1 -61.20000 -0.37317 1.71469 2 -53.00000 -0.32317 5.91587 3 -44.80000 -0.27317 7.36720 4 -37.35000 -0.22774 10.25835 5 -29.90000 -0.18232 9.47910 6 -22.90000 -0.13963 7.60813 7 -15.90000 -0.09695 6.49868 8 -5.90000 -0.03598 5.91663 9 -159.89999 -0.97500 14.45816 10 -151.70001 -0.92500 16.44655 11 -143.50000 -0.87500 14.38027 12 -135.30002 -0.82500 12.36750 13 -127.10001 -0.77500 10.75520 14 -118.90002 -0.72500 9.51973 15 -110.70002 -0.67500 8.46040 16 -102.50002 -0.62500 7.34168 17 -94.30003 -0.57500 6.13154 18 -86.10003 -0.52500 4.67249 19 -77.90003 -0.47500 2.88238 20 -69.55002 -0.42409 1.36595 21 -61.20000 -0.37317 3.52797 22 -53.00000 -0.32317 4.51491 23 -44.80000 -0.27317 4.49845 24 -37.35000 -0.22774 3.79378 25 -29.90000 -0.18232 3.77474 26 -22.90000 -0.13963 3.11226 27 -15.90000 -0.09695 3.52109 28 -5.90000 -0.03598 3.98970 STOP