williams-imac:LAMDESfolder williamhmason$ ./LamDes2 enter name of input file: ar1030.inp Lamar Design Code mods by W.H. Mason LamarDesign Program - AR = 10, lambda = 0.5 30 deg sweep - plan = 1.0 xmref = -0.0000 cref = 3.0000 tdklue = 0.0 case = 0.0 spnklu = 0.0 sref = 90.0000 REFERENCE PLANFORM HAS 3 CURVES ROOT CHORD HEIGHT = -0.0000 POINT X Y SWEEP DIHEDRAL REF REF ANGLE ANGLE 1 2.0000 0.0000 26.56505 0.00000 2 -5.5000 -15.0000 90.00000 0.00000 3 -7.5000 -15.0000 20.13630 0.00000 4 -2.0000 0.0000 scw = 16.0 vic = 22.0 xitmax = 40.0 epsmax = 0.00060 CONFIGURATION NO. 1. delta ord shift for moment = -0.0000 CURVE 1 IS SWEPT 26.5651 DEGREES ON PLANFORM 1 BREAK POINTS FOR THIS CONFIGURATION POINT X Y Z SWEEP DIHEDRAL ANGLE ANGLE 1 2.0000 0.0000 -0.0000 26.5651 0.0000 2 -5.5000 -15.0000 -0.0000 90.0000 0.0000 3 -7.5000 -15.0000 -0.0000 20.1363 0.0000 4 -2.0000 0.0000 -0.0000 a = 0.000 clmin = 0.000 cd0 =0.0000 352 HORSESHOE VORTICES USED PLANFORM TOTAL SPANWISE 1 352 22 16. HORSESHOE VORTICES IN EACH CHORDWISE ROW xcfw = 0.65 xcft = 0.65 fkon = 1.00 ficam = 1.00 punch = 0.00 crbmnt = 0.000 cmb = -.00 iflag = 1 relax = 0.03 fioutw = 1.00 cd0 = 0.0000 firbm = 0.00 yrbm = 0.0000 zrbm = 0.0000 induced drag cd = 0.03151 pressure drag cdpt = 0.00000 induced drag alone was minimized on this run ref. chord = 3.000 c average = 3.0000 true area = 90.000 ref. area = 90.000 b/2 = 15.0000 ref ar = 10.0000 true ar = 10.0000 Mach number = 0.3000 first planform cl = 1.00000 cm = -0.83082 cb = -0.21325 1st planform CL = 1.0002 CDP = 0.0000 CM = -0.8316 CB = -0.2134 2nd planform CL = 0.0000 CDP = 0.0000 CM = 0.0000 CB = 0.0000 no pitching moment or bending moment constraints CL DES = 1.00000 CL COMPUTED = 1.0002 CM = -0.8316 CD I = 0.03151 E = 1.0105 CDPRESS = 0.00000 CDTOTAL = 0.03151 first planform Y CL*C/CAVE C/CAVE CL CD -14.6591 0.29309 0.68182 0.42986 0.00000 -13.9773 0.47470 0.71212 0.66660 0.00000 -13.2955 0.59705 0.74243 0.80419 0.00000 -12.6136 0.69356 0.77273 0.89755 0.00000 -11.9318 0.77418 0.80303 0.96407 0.00000 -11.2500 0.84338 0.83333 1.01206 0.00000 -10.5682 0.90337 0.86364 1.04601 0.00000 -9.8864 0.95631 0.89394 1.06978 0.00000 -9.2045 1.00329 0.92424 1.08552 0.00000 -8.5227 1.04500 0.95455 1.09476 0.00000 -7.8409 1.08199 0.98485 1.09864 0.00000 -7.1591 1.11487 1.01515 1.09823 0.00000 -6.4773 1.14400 1.04545 1.09426 0.00000 -5.7955 1.16953 1.07576 1.08717 0.00000 -5.1136 1.19175 1.10606 1.07747 0.00000 -4.4318 1.21091 1.13636 1.06560 0.00000 -3.7500 1.22714 1.16667 1.05184 0.00000 -3.0682 1.24041 1.19697 1.03629 0.00000 -2.3864 1.25096 1.22727 1.01930 0.00000 -1.7045 1.25885 1.25758 1.00101 0.00000 -1.0227 1.26410 1.28788 0.98153 0.00000 -0.3409 1.26672 1.31818 0.96096 0.00000 mean camber lines to obtain the spanload (subsonic linear theory) y= -14.6591 y/(b/2) = -0.9773 chord= 2.0455 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.1607 0.1094 0.1294 0.1719 0.1084 0.2344 0.0909 0.2969 0.0747 0.3594 0.0589 0.4219 0.0428 0.4844 0.0258 0.5469 0.0070 0.6094 -0.0153 0.6719 -0.0499 0.7344 -0.0724 0.7969 -0.0862 0.8594 -0.0939 0.9219 -0.0952 0.9844 -0.0867 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 0.0163 0.0000 0.0333 0.0000 0.0250 0.0122 0.0511 0.0250 -0.0036 0.0500 0.0082 0.1023 0.0168 -0.0073 0.0750 0.0043 0.1534 0.0088 -0.0107 0.1000 0.0008 0.2045 0.0016 -0.0139 0.1250 -0.0024 0.2557 -0.0050 -0.0167 0.1500 -0.0054 0.3068 -0.0110 -0.0192 0.1750 -0.0082 0.3580 -0.0167 -0.0216 0.2000 -0.0108 0.4091 -0.0220 -0.0238 0.2250 -0.0132 0.4602 -0.0270 -0.0258 0.2500 -0.0154 0.5114 -0.0316 -0.0276 0.2750 -0.0175 0.5625 -0.0358 -0.0293 0.3000 -0.0195 0.6136 -0.0398 -0.0308 0.3250 -0.0212 0.6648 -0.0434 -0.0322 0.3500 -0.0228 0.7159 -0.0467 -0.0334 0.3750 -0.0243 0.7670 -0.0497 -0.0345 0.4000 -0.0256 0.8182 -0.0523 -0.0353 0.4250 -0.0267 0.8693 -0.0546 -0.0361 0.4500 -0.0277 0.9205 -0.0566 -0.0366 0.4750 -0.0285 0.9716 -0.0582 -0.0370 0.5000 -0.0291 1.0227 -0.0595 -0.0372 0.5250 -0.0295 1.0739 -0.0604 -0.0373 0.5500 -0.0298 1.1250 -0.0609 -0.0371 0.5750 -0.0298 1.1761 -0.0610 -0.0368 0.6000 -0.0297 1.2273 -0.0607 -0.0362 0.6250 -0.0293 1.2784 -0.0598 -0.0354 0.6500 -0.0285 1.3295 -0.0583 -0.0342 0.6750 -0.0274 1.3807 -0.0560 -0.0327 0.7000 -0.0259 1.4318 -0.0531 -0.0308 0.7250 -0.0243 1.4830 -0.0497 -0.0288 0.7500 -0.0225 1.5341 -0.0460 -0.0265 0.7750 -0.0205 1.5852 -0.0419 -0.0241 0.8000 -0.0184 1.6364 -0.0376 -0.0216 0.8250 -0.0162 1.6875 -0.0330 -0.0190 0.8500 -0.0139 1.7386 -0.0284 -0.0163 0.8750 -0.0115 1.7898 -0.0235 -0.0135 0.9000 -0.0091 1.8409 -0.0186 -0.0107 0.9250 -0.0067 1.8920 -0.0137 -0.0079 0.9500 -0.0044 1.9432 -0.0090 -0.0052 0.9750 -0.0022 1.9943 -0.0044 -0.0026 1.0000 0.0000 2.0455 0.0000 0.0000 1 y= -13.9773 y/(b/2) = -0.9318 chord= 2.1364 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.1930 0.1094 0.1423 0.1719 0.1085 0.2344 0.0811 0.2969 0.0566 0.3594 0.0332 0.4219 0.0099 0.4844 -0.0144 0.5469 -0.0410 0.6094 -0.0729 0.6719 -0.1234 0.7344 -0.1548 0.7969 -0.1728 0.8594 -0.1815 0.9219 -0.1807 0.9844 -0.1651 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0246 0.0000 -0.0525 0.0000 0.0250 -0.0294 0.0534 -0.0629 -0.0055 0.0500 -0.0343 0.1068 -0.0733 -0.0109 0.0750 -0.0389 0.1602 -0.0831 -0.0162 0.1000 -0.0430 0.2136 -0.0918 -0.0208 0.1250 -0.0465 0.2670 -0.0993 -0.0250 0.1500 -0.0496 0.3205 -0.1059 -0.0287 0.1750 -0.0524 0.3739 -0.1119 -0.0321 0.2000 -0.0549 0.4273 -0.1173 -0.0353 0.2250 -0.0572 0.4807 -0.1222 -0.0381 0.2500 -0.0592 0.5341 -0.1264 -0.0407 0.2750 -0.0609 0.5875 -0.1302 -0.0431 0.3000 -0.0624 0.6409 -0.1334 -0.0452 0.3250 -0.0637 0.6943 -0.1361 -0.0471 0.3500 -0.0647 0.7477 -0.1383 -0.0488 0.3750 -0.0655 0.8011 -0.1400 -0.0502 0.4000 -0.0661 0.8545 -0.1412 -0.0514 0.4250 -0.0664 0.9080 -0.1419 -0.0523 0.4500 -0.0665 0.9614 -0.1422 -0.0530 0.4750 -0.0664 1.0148 -0.1419 -0.0535 0.5000 -0.0660 1.0682 -0.1410 -0.0537 0.5250 -0.0654 1.1216 -0.1396 -0.0537 0.5500 -0.0644 1.1750 -0.1376 -0.0534 0.5750 -0.0632 1.2284 -0.1351 -0.0528 0.6000 -0.0617 1.2818 -0.1319 -0.0519 0.6250 -0.0599 1.3352 -0.1279 -0.0506 0.6500 -0.0575 1.3886 -0.1228 -0.0489 0.6750 -0.0546 1.4420 -0.1166 -0.0466 0.7000 -0.0512 1.4955 -0.1095 -0.0439 0.7250 -0.0476 1.5489 -0.1017 -0.0408 0.7500 -0.0437 1.6023 -0.0933 -0.0375 0.7750 -0.0396 1.6557 -0.0846 -0.0341 0.8000 -0.0353 1.7091 -0.0755 -0.0304 0.8250 -0.0309 1.7625 -0.0661 -0.0266 0.8500 -0.0265 1.8159 -0.0565 -0.0228 0.8750 -0.0219 1.8693 -0.0468 -0.0188 0.9000 -0.0173 1.9227 -0.0370 -0.0149 0.9250 -0.0128 1.9761 -0.0273 -0.0109 0.9500 -0.0084 2.0296 -0.0179 -0.0071 0.9750 -0.0041 2.0830 -0.0088 -0.0035 1.0000 0.0000 2.1364 0.0000 0.0000 1 y= -13.2955 y/(b/2) = -0.8864 chord= 2.2273 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.2159 0.1094 0.1547 0.1719 0.1143 0.2344 0.0820 0.2969 0.0535 0.3594 0.0267 0.4219 0.0002 0.4844 -0.0273 0.5469 -0.0574 0.6094 -0.0937 0.6719 -0.1524 0.7344 -0.1879 0.7969 -0.2073 0.8594 -0.2157 0.9219 -0.2127 0.9844 -0.1921 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0374 0.0000 -0.0833 0.0000 0.0250 -0.0428 0.0557 -0.0954 -0.0064 0.0500 -0.0483 0.1114 -0.1075 -0.0127 0.0750 -0.0534 0.1670 -0.1190 -0.0188 0.1000 -0.0579 0.2227 -0.1289 -0.0242 0.1250 -0.0617 0.2784 -0.1374 -0.0290 0.1500 -0.0650 0.3341 -0.1448 -0.0332 0.1750 -0.0680 0.3898 -0.1514 -0.0371 0.2000 -0.0706 0.4455 -0.1573 -0.0407 0.2250 -0.0730 0.5011 -0.1625 -0.0440 0.2500 -0.0750 0.5568 -0.1670 -0.0469 0.2750 -0.0767 0.6125 -0.1708 -0.0496 0.3000 -0.0781 0.6682 -0.1740 -0.0520 0.3250 -0.0793 0.7239 -0.1766 -0.0541 0.3500 -0.0802 0.7795 -0.1786 -0.0559 0.3750 -0.0808 0.8352 -0.1800 -0.0575 0.4000 -0.0812 0.8909 -0.1809 -0.0588 0.4250 -0.0813 0.9466 -0.1811 -0.0598 0.4500 -0.0811 1.0023 -0.1807 -0.0606 0.4750 -0.0807 1.0580 -0.1798 -0.0611 0.5000 -0.0800 1.1136 -0.1782 -0.0613 0.5250 -0.0790 1.1693 -0.1759 -0.0612 0.5500 -0.0776 1.2250 -0.1729 -0.0608 0.5750 -0.0760 1.2807 -0.1693 -0.0601 0.6000 -0.0741 1.3364 -0.1650 -0.0591 0.6250 -0.0716 1.3920 -0.1596 -0.0576 0.6500 -0.0687 1.4477 -0.1529 -0.0556 0.6750 -0.0651 1.5034 -0.1449 -0.0529 0.7000 -0.0610 1.5591 -0.1358 -0.0497 0.7250 -0.0565 1.6148 -0.1259 -0.0462 0.7500 -0.0518 1.6705 -0.1153 -0.0424 0.7750 -0.0468 1.7261 -0.1043 -0.0384 0.8000 -0.0417 1.7818 -0.0929 -0.0342 0.8250 -0.0364 1.8375 -0.0812 -0.0299 0.8500 -0.0311 1.8932 -0.0693 -0.0255 0.8750 -0.0257 1.9489 -0.0573 -0.0210 0.9000 -0.0203 2.0046 -0.0452 -0.0165 0.9250 -0.0149 2.0602 -0.0332 -0.0121 0.9500 -0.0097 2.1159 -0.0217 -0.0079 0.9750 -0.0048 2.1716 -0.0107 -0.0039 1.0000 0.0000 2.2273 0.0000 0.0000 1 y= -12.6136 y/(b/2) = -0.8409 chord= 2.3182 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.2318 0.1094 0.1634 0.1719 0.1183 0.2344 0.0825 0.2969 0.0511 0.3594 0.0218 0.4219 -0.0071 0.4844 -0.0369 0.5469 -0.0696 0.6094 -0.1090 0.6719 -0.1734 0.7344 -0.2119 0.7969 -0.2325 0.8594 -0.2406 0.9219 -0.2362 0.9844 -0.2122 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c -0.0000 -0.0469 -0.0000 -0.1088 0.0000 0.0250 -0.0528 0.0580 -0.1223 -0.0070 0.0500 -0.0586 0.1159 -0.1358 -0.0140 0.0750 -0.0641 0.1739 -0.1486 -0.0207 0.1000 -0.0689 0.2318 -0.1596 -0.0266 0.1250 -0.0729 0.2898 -0.1689 -0.0318 0.1500 -0.0763 0.3477 -0.1770 -0.0365 0.1750 -0.0794 0.4057 -0.1841 -0.0407 0.2000 -0.0822 0.4636 -0.1905 -0.0446 0.2250 -0.0845 0.5216 -0.1960 -0.0482 0.2500 -0.0866 0.5795 -0.2007 -0.0514 0.2750 -0.0883 0.6375 -0.2046 -0.0542 0.3000 -0.0896 0.6955 -0.2078 -0.0568 0.3250 -0.0907 0.7534 -0.2104 -0.0591 0.3500 -0.0915 0.8114 -0.2122 -0.0610 0.3750 -0.0921 0.8693 -0.2134 -0.0627 0.4000 -0.0923 0.9273 -0.2139 -0.0641 0.4250 -0.0922 0.9852 -0.2137 -0.0652 0.4500 -0.0918 1.0432 -0.2129 -0.0660 0.4750 -0.0912 1.1011 -0.2114 -0.0666 0.5000 -0.0902 1.1591 -0.2092 -0.0668 0.5250 -0.0889 1.2171 -0.2062 -0.0667 0.5500 -0.0873 1.2750 -0.2024 -0.0662 0.5750 -0.0854 1.3330 -0.1979 -0.0654 0.6000 -0.0831 1.3909 -0.1926 -0.0643 0.6250 -0.0803 1.4489 -0.1861 -0.0627 0.6500 -0.0768 1.5068 -0.1781 -0.0604 0.6750 -0.0727 1.5648 -0.1686 -0.0575 0.7000 -0.0681 1.6227 -0.1578 -0.0540 0.7250 -0.0630 1.6807 -0.1461 -0.0501 0.7500 -0.0577 1.7386 -0.1338 -0.0460 0.7750 -0.0521 1.7966 -0.1209 -0.0416 0.8000 -0.0464 1.8546 -0.1075 -0.0370 0.8250 -0.0405 1.9125 -0.0939 -0.0323 0.8500 -0.0345 1.9705 -0.0801 -0.0275 0.8750 -0.0285 2.0284 -0.0661 -0.0227 0.9000 -0.0225 2.0864 -0.0521 -0.0178 0.9250 -0.0165 2.1443 -0.0383 -0.0130 0.9500 -0.0108 2.2023 -0.0250 -0.0084 0.9750 -0.0053 2.2602 -0.0123 -0.0041 1.0000 0.0000 2.3182 0.0000 0.0000 1 y= -11.9318 y/(b/2) = -0.7955 chord= 2.4091 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.2429 0.1094 0.1692 0.1719 0.1208 0.2344 0.0825 0.2969 0.0490 0.3594 0.0178 0.4219 -0.0129 0.4844 -0.0445 0.5469 -0.0791 0.6094 -0.1208 0.6719 -0.1894 0.7344 -0.2301 0.7969 -0.2514 0.8594 -0.2595 0.9219 -0.2542 0.9844 -0.2278 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0544 0.0000 -0.1312 0.0000 0.0250 -0.0606 0.0602 -0.1459 -0.0075 0.0500 -0.0667 0.1205 -0.1607 -0.0150 0.0750 -0.0724 0.1807 -0.1745 -0.0221 0.1000 -0.0774 0.2409 -0.1864 -0.0284 0.1250 -0.0815 0.3011 -0.1965 -0.0339 0.1500 -0.0851 0.3614 -0.2051 -0.0388 0.1750 -0.0883 0.4216 -0.2127 -0.0434 0.2000 -0.0911 0.4818 -0.2194 -0.0475 0.2250 -0.0935 0.5420 -0.2252 -0.0513 0.2500 -0.0955 0.6023 -0.2300 -0.0546 0.2750 -0.0971 0.6625 -0.2340 -0.0577 0.3000 -0.0985 0.7227 -0.2373 -0.0604 0.3250 -0.0995 0.7830 -0.2398 -0.0628 0.3500 -0.1002 0.8432 -0.2415 -0.0648 0.3750 -0.1006 0.9034 -0.2425 -0.0666 0.4000 -0.1007 0.9636 -0.2427 -0.0681 0.4250 -0.1005 1.0239 -0.2422 -0.0692 0.4500 -0.1000 1.0841 -0.2410 -0.0701 0.4750 -0.0992 1.1443 -0.2390 -0.0706 0.5000 -0.0980 1.2045 -0.2362 -0.0708 0.5250 -0.0965 1.2648 -0.2326 -0.0707 0.5500 -0.0947 1.3250 -0.2281 -0.0702 0.5750 -0.0925 1.3852 -0.2228 -0.0694 0.6000 -0.0899 1.4455 -0.2166 -0.0681 0.6250 -0.0868 1.5057 -0.2091 -0.0664 0.6500 -0.0830 1.5659 -0.2000 -0.0640 0.6750 -0.0785 1.6261 -0.1892 -0.0608 0.7000 -0.0735 1.6864 -0.1770 -0.0571 0.7250 -0.0680 1.7466 -0.1638 -0.0530 0.7500 -0.0622 1.8068 -0.1499 -0.0486 0.7750 -0.0562 1.8670 -0.1353 -0.0439 0.8000 -0.0500 1.9273 -0.1203 -0.0391 0.8250 -0.0436 1.9875 -0.1050 -0.0341 0.8500 -0.0372 2.0477 -0.0895 -0.0290 0.8750 -0.0307 2.1080 -0.0739 -0.0239 0.9000 -0.0242 2.1682 -0.0582 -0.0187 0.9250 -0.0177 2.2284 -0.0427 -0.0137 0.9500 -0.0116 2.2886 -0.0279 -0.0088 0.9750 -0.0057 2.3489 -0.0137 -0.0043 1.0000 0.0000 2.4091 0.0000 0.0000 1 y= -11.2500 y/(b/2) = -0.7500 chord= 2.5000 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.2504 0.1094 0.1729 0.1719 0.1221 0.2344 0.0819 0.2969 0.0468 0.3594 0.0142 0.4219 -0.0177 0.4844 -0.0506 0.5469 -0.0867 0.6094 -0.1302 0.6719 -0.2017 0.7344 -0.2440 0.7969 -0.2660 0.8594 -0.2740 0.9219 -0.2679 0.9844 -0.2398 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0606 0.0000 -0.1515 0.0000 0.0250 -0.0669 0.0625 -0.1672 -0.0078 0.0500 -0.0732 0.1250 -0.1830 -0.0156 0.0750 -0.0791 0.1875 -0.1978 -0.0231 0.1000 -0.0842 0.2500 -0.2105 -0.0297 0.1250 -0.0885 0.3125 -0.2211 -0.0354 0.1500 -0.0921 0.3750 -0.2302 -0.0406 0.1750 -0.0953 0.4375 -0.2382 -0.0453 0.2000 -0.0981 0.5000 -0.2452 -0.0496 0.2250 -0.1005 0.5625 -0.2512 -0.0535 0.2500 -0.1025 0.6250 -0.2562 -0.0570 0.2750 -0.1041 0.6875 -0.2603 -0.0602 0.3000 -0.1054 0.7500 -0.2635 -0.0630 0.3250 -0.1064 0.8125 -0.2659 -0.0655 0.3500 -0.1070 0.8750 -0.2675 -0.0676 0.3750 -0.1073 0.9375 -0.2683 -0.0695 0.4000 -0.1073 1.0000 -0.2683 -0.0710 0.4250 -0.1070 1.0625 -0.2675 -0.0722 0.4500 -0.1064 1.1250 -0.2659 -0.0730 0.4750 -0.1054 1.1875 -0.2635 -0.0736 0.5000 -0.1041 1.2500 -0.2602 -0.0738 0.5250 -0.1024 1.3125 -0.2560 -0.0736 0.5500 -0.1004 1.3750 -0.2509 -0.0731 0.5750 -0.0980 1.4375 -0.2450 -0.0722 0.6000 -0.0952 1.5000 -0.2380 -0.0710 0.6250 -0.0918 1.5625 -0.2296 -0.0691 0.6500 -0.0878 1.6250 -0.2195 -0.0666 0.6750 -0.0830 1.6875 -0.2075 -0.0633 0.7000 -0.0776 1.7500 -0.1941 -0.0594 0.7250 -0.0718 1.8125 -0.1795 -0.0551 0.7500 -0.0657 1.8750 -0.1642 -0.0505 0.7750 -0.0593 1.9375 -0.1482 -0.0457 0.8000 -0.0527 2.0000 -0.1317 -0.0406 0.8250 -0.0460 2.0625 -0.1149 -0.0354 0.8500 -0.0392 2.1250 -0.0979 -0.0301 0.8750 -0.0323 2.1875 -0.0808 -0.0247 0.9000 -0.0254 2.2500 -0.0636 -0.0194 0.9250 -0.0187 2.3125 -0.0467 -0.0141 0.9500 -0.0122 2.3750 -0.0304 -0.0091 0.9750 -0.0060 2.4375 -0.0150 -0.0045 1.0000 0.0000 2.5000 0.0000 0.0000 1 y= -10.5682 y/(b/2) = -0.7045 chord= 2.5909 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.2552 0.1094 0.1751 0.1719 0.1225 0.2344 0.0810 0.2969 0.0448 0.3594 0.0113 0.4219 -0.0216 0.4844 -0.0554 0.5469 -0.0924 0.6094 -0.1370 0.6719 -0.2107 0.7344 -0.2541 0.7969 -0.2764 0.8594 -0.2844 0.9219 -0.2778 0.9844 -0.2484 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0652 0.0000 -0.1690 0.0000 0.0250 -0.0717 0.0648 -0.1857 -0.0081 0.0500 -0.0781 0.1295 -0.2024 -0.0161 0.0750 -0.0841 0.1943 -0.2180 -0.0238 0.1000 -0.0893 0.2591 -0.2314 -0.0306 0.1250 -0.0936 0.3239 -0.2425 -0.0365 0.1500 -0.0973 0.3886 -0.2520 -0.0418 0.1750 -0.1005 0.4534 -0.2603 -0.0466 0.2000 -0.1033 0.5182 -0.2676 -0.0511 0.2250 -0.1057 0.5830 -0.2738 -0.0551 0.2500 -0.1076 0.6477 -0.2789 -0.0587 0.2750 -0.1092 0.7125 -0.2830 -0.0619 0.3000 -0.1105 0.7773 -0.2863 -0.0648 0.3250 -0.1114 0.8420 -0.2886 -0.0674 0.3500 -0.1120 0.9068 -0.2901 -0.0696 0.3750 -0.1122 0.9716 -0.2907 -0.0714 0.4000 -0.1121 1.0364 -0.2905 -0.0730 0.4250 -0.1117 1.1011 -0.2894 -0.0742 0.4500 -0.1110 1.1659 -0.2875 -0.0751 0.4750 -0.1099 1.2307 -0.2847 -0.0756 0.5000 -0.1085 1.2955 -0.2810 -0.0758 0.5250 -0.1067 1.3602 -0.2763 -0.0757 0.5500 -0.1045 1.4250 -0.2707 -0.0751 0.5750 -0.1019 1.4898 -0.2641 -0.0742 0.6000 -0.0990 1.5545 -0.2565 -0.0729 0.6250 -0.0955 1.6193 -0.2474 -0.0710 0.6500 -0.0912 1.6841 -0.2364 -0.0684 0.6750 -0.0862 1.7489 -0.2234 -0.0650 0.7000 -0.0806 1.8136 -0.2088 -0.0610 0.7250 -0.0745 1.8784 -0.1931 -0.0566 0.7500 -0.0682 1.9432 -0.1766 -0.0518 0.7750 -0.0615 2.0080 -0.1594 -0.0468 0.8000 -0.0547 2.0727 -0.1416 -0.0416 0.8250 -0.0477 2.1375 -0.1235 -0.0363 0.8500 -0.0406 2.2023 -0.1052 -0.0308 0.8750 -0.0335 2.2670 -0.0868 -0.0253 0.9000 -0.0264 2.3318 -0.0683 -0.0198 0.9250 -0.0194 2.3966 -0.0501 -0.0145 0.9500 -0.0126 2.4614 -0.0327 -0.0093 0.9750 -0.0062 2.5261 -0.0161 -0.0046 1.0000 0.0000 2.5909 0.0000 0.0000 1 y= -9.8864 y/(b/2) = -0.6591 chord= 2.6818 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.2579 0.1094 0.1759 0.1719 0.1221 0.2344 0.0796 0.2969 0.0427 0.3594 0.0084 0.4219 -0.0250 0.4844 -0.0595 0.5469 -0.0971 0.6094 -0.1426 0.6719 -0.2177 0.7344 -0.2619 0.7969 -0.2845 0.8594 -0.2924 0.9219 -0.2854 0.9844 -0.2551 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0693 0.0000 -0.1857 0.0000 0.0250 -0.0757 0.0670 -0.2031 -0.0082 0.0500 -0.0823 0.1341 -0.2206 -0.0165 0.0750 -0.0883 0.2011 -0.2369 -0.0243 0.1000 -0.0935 0.2682 -0.2509 -0.0312 0.1250 -0.0979 0.3352 -0.2624 -0.0373 0.1500 -0.1015 0.4023 -0.2723 -0.0427 0.1750 -0.1047 0.4693 -0.2809 -0.0476 0.2000 -0.1075 0.5364 -0.2883 -0.0521 0.2250 -0.1099 0.6034 -0.2947 -0.0562 0.2500 -0.1118 0.6705 -0.2999 -0.0599 0.2750 -0.1134 0.7375 -0.3040 -0.0632 0.3000 -0.1146 0.8045 -0.3073 -0.0661 0.3250 -0.1154 0.8716 -0.3095 -0.0687 0.3500 -0.1159 0.9386 -0.3109 -0.0709 0.3750 -0.1161 1.0057 -0.3114 -0.0728 0.4000 -0.1159 1.0727 -0.3109 -0.0744 0.4250 -0.1154 1.1398 -0.3096 -0.0756 0.4500 -0.1146 1.2068 -0.3073 -0.0765 0.4750 -0.1134 1.2739 -0.3042 -0.0771 0.5000 -0.1119 1.3409 -0.3001 -0.0773 0.5250 -0.1100 1.4080 -0.2949 -0.0771 0.5500 -0.1077 1.4750 -0.2888 -0.0765 0.5750 -0.1050 1.5420 -0.2817 -0.0756 0.6000 -0.1019 1.6091 -0.2734 -0.0742 0.6250 -0.0983 1.6761 -0.2636 -0.0723 0.6500 -0.0939 1.7432 -0.2518 -0.0696 0.6750 -0.0887 1.8102 -0.2379 -0.0662 0.7000 -0.0829 1.8773 -0.2223 -0.0621 0.7250 -0.0767 1.9443 -0.2056 -0.0576 0.7500 -0.0701 2.0114 -0.1879 -0.0528 0.7750 -0.0632 2.0784 -0.1696 -0.0476 0.8000 -0.0562 2.1454 -0.1507 -0.0423 0.8250 -0.0490 2.2125 -0.1314 -0.0369 0.8500 -0.0417 2.2795 -0.1119 -0.0313 0.8750 -0.0344 2.3466 -0.0923 -0.0258 0.9000 -0.0271 2.4136 -0.0727 -0.0202 0.9250 -0.0199 2.4807 -0.0533 -0.0147 0.9500 -0.0130 2.5477 -0.0347 -0.0095 0.9750 -0.0064 2.6148 -0.0171 -0.0047 1.0000 0.0000 2.6818 0.0000 0.0000 1 y= -9.2045 y/(b/2) = -0.6136 chord= 2.7727 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.2589 0.1094 0.1756 0.1719 0.1210 0.2344 0.0779 0.2969 0.0404 0.3594 0.0057 0.4219 -0.0282 0.4844 -0.0630 0.5469 -0.1011 0.6094 -0.1471 0.6719 -0.2232 0.7344 -0.2678 0.7969 -0.2905 0.8594 -0.2984 0.9219 -0.2911 0.9844 -0.2602 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0727 0.0000 -0.2015 0.0000 0.0250 -0.0792 0.0693 -0.2196 -0.0083 0.0500 -0.0857 0.1386 -0.2377 -0.0167 0.0750 -0.0918 0.2080 -0.2546 -0.0246 0.1000 -0.0970 0.2773 -0.2691 -0.0316 0.1250 -0.1014 0.3466 -0.2810 -0.0378 0.1500 -0.1050 0.4159 -0.2911 -0.0432 0.1750 -0.1082 0.4852 -0.3000 -0.0482 0.2000 -0.1109 0.5545 -0.3076 -0.0528 0.2250 -0.1133 0.6239 -0.3140 -0.0569 0.2500 -0.1152 0.6932 -0.3193 -0.0606 0.2750 -0.1167 0.7625 -0.3235 -0.0640 0.3000 -0.1178 0.8318 -0.3266 -0.0669 0.3250 -0.1186 0.9011 -0.3288 -0.0695 0.3500 -0.1190 0.9705 -0.3301 -0.0718 0.3750 -0.1191 1.0398 -0.3304 -0.0737 0.4000 -0.1189 1.1091 -0.3297 -0.0753 0.4250 -0.1183 1.1784 -0.3281 -0.0765 0.4500 -0.1174 1.2477 -0.3256 -0.0774 0.4750 -0.1162 1.3170 -0.3221 -0.0780 0.5000 -0.1145 1.3864 -0.3176 -0.0782 0.5250 -0.1125 1.4557 -0.3120 -0.0780 0.5500 -0.1101 1.5250 -0.3054 -0.0774 0.5750 -0.1074 1.5943 -0.2977 -0.0765 0.6000 -0.1042 1.6636 -0.2889 -0.0751 0.6250 -0.1004 1.7330 -0.2784 -0.0732 0.6500 -0.0959 1.8023 -0.2659 -0.0705 0.6750 -0.0906 1.8716 -0.2512 -0.0670 0.7000 -0.0846 1.9409 -0.2347 -0.0628 0.7250 -0.0782 2.0102 -0.2169 -0.0583 0.7500 -0.0715 2.0795 -0.1983 -0.0533 0.7750 -0.0645 2.1489 -0.1789 -0.0482 0.8000 -0.0573 2.2182 -0.1589 -0.0428 0.8250 -0.0500 2.2875 -0.1386 -0.0373 0.8500 -0.0426 2.3568 -0.1180 -0.0317 0.8750 -0.0351 2.4261 -0.0973 -0.0260 0.9000 -0.0276 2.4955 -0.0766 -0.0204 0.9250 -0.0203 2.5648 -0.0562 -0.0148 0.9500 -0.0132 2.6341 -0.0366 -0.0096 0.9750 -0.0065 2.7034 -0.0181 -0.0047 1.0000 0.0000 2.7727 0.0000 0.0000 1 y= -8.5227 y/(b/2) = -0.5682 chord= 2.8636 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.2585 0.1094 0.1745 0.1719 0.1193 0.2344 0.0758 0.2969 0.0381 0.3594 0.0031 0.4219 -0.0310 0.4844 -0.0660 0.5469 -0.1044 0.6094 -0.1507 0.6719 -0.2272 0.7344 -0.2721 0.7969 -0.2949 0.8594 -0.3026 0.9219 -0.2951 0.9844 -0.2638 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0756 0.0000 -0.2165 0.0000 0.0250 -0.0821 0.0716 -0.2351 -0.0084 0.0500 -0.0886 0.1432 -0.2538 -0.0168 0.0750 -0.0947 0.2148 -0.2712 -0.0248 0.1000 -0.0999 0.2864 -0.2861 -0.0319 0.1250 -0.1042 0.3580 -0.2984 -0.0380 0.1500 -0.1078 0.4295 -0.3087 -0.0435 0.1750 -0.1109 0.5011 -0.3177 -0.0486 0.2000 -0.1137 0.5727 -0.3255 -0.0532 0.2250 -0.1159 0.6443 -0.3320 -0.0573 0.2500 -0.1178 0.7159 -0.3373 -0.0611 0.2750 -0.1192 0.7875 -0.3414 -0.0644 0.3000 -0.1203 0.8591 -0.3445 -0.0674 0.3250 -0.1210 0.9307 -0.3466 -0.0700 0.3500 -0.1214 1.0023 -0.3477 -0.0723 0.3750 -0.1215 1.0739 -0.3478 -0.0742 0.4000 -0.1212 1.1455 -0.3470 -0.0758 0.4250 -0.1205 1.2170 -0.3451 -0.0770 0.4500 -0.1195 1.2886 -0.3423 -0.0779 0.4750 -0.1182 1.3602 -0.3384 -0.0785 0.5000 -0.1165 1.4318 -0.3336 -0.0787 0.5250 -0.1144 1.5034 -0.3276 -0.0785 0.5500 -0.1119 1.5750 -0.3206 -0.0779 0.5750 -0.1091 1.6466 -0.3124 -0.0770 0.6000 -0.1058 1.7182 -0.3030 -0.0756 0.6250 -0.1020 1.7898 -0.2920 -0.0736 0.6500 -0.0973 1.8614 -0.2787 -0.0709 0.6750 -0.0919 1.9330 -0.2633 -0.0674 0.7000 -0.0859 2.0045 -0.2459 -0.0632 0.7250 -0.0794 2.0761 -0.2273 -0.0586 0.7500 -0.0725 2.1477 -0.2077 -0.0536 0.7750 -0.0654 2.2193 -0.1874 -0.0484 0.8000 -0.0581 2.2909 -0.1665 -0.0430 0.8250 -0.0507 2.3625 -0.1451 -0.0374 0.8500 -0.0432 2.4341 -0.1236 -0.0318 0.8750 -0.0356 2.5057 -0.1019 -0.0261 0.9000 -0.0280 2.5773 -0.0802 -0.0205 0.9250 -0.0206 2.6489 -0.0589 -0.0149 0.9500 -0.0134 2.7205 -0.0384 -0.0096 0.9750 -0.0066 2.7920 -0.0189 -0.0047 1.0000 0.0000 2.8636 0.0000 0.0000 1 y= -7.8409 y/(b/2) = -0.5227 chord= 2.9545 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.2570 0.1094 0.1726 0.1719 0.1172 0.2344 0.0736 0.2969 0.0357 0.3594 0.0007 0.4219 -0.0335 0.4844 -0.0686 0.5469 -0.1070 0.6094 -0.1534 0.6719 -0.2301 0.7344 -0.2750 0.7969 -0.2977 0.8594 -0.3053 0.9219 -0.2977 0.9844 -0.2662 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0781 0.0000 -0.2306 0.0000 0.0250 -0.0845 0.0739 -0.2497 -0.0084 0.0500 -0.0910 0.1477 -0.2689 -0.0169 0.0750 -0.0971 0.2216 -0.2868 -0.0249 0.1000 -0.1022 0.2955 -0.3020 -0.0320 0.1250 -0.1064 0.3693 -0.3145 -0.0381 0.1500 -0.1100 0.4432 -0.3250 -0.0437 0.1750 -0.1131 0.5170 -0.3341 -0.0487 0.2000 -0.1157 0.5909 -0.3420 -0.0533 0.2250 -0.1180 0.6648 -0.3485 -0.0575 0.2500 -0.1198 0.7386 -0.3538 -0.0612 0.2750 -0.1211 0.8125 -0.3579 -0.0646 0.3000 -0.1222 0.8864 -0.3610 -0.0675 0.3250 -0.1228 0.9602 -0.3630 -0.0702 0.3500 -0.1232 1.0341 -0.3639 -0.0724 0.3750 -0.1231 1.1080 -0.3638 -0.0744 0.4000 -0.1228 1.1818 -0.3627 -0.0759 0.4250 -0.1221 1.2557 -0.3606 -0.0772 0.4500 -0.1210 1.3295 -0.3575 -0.0781 0.4750 -0.1196 1.4034 -0.3534 -0.0786 0.5000 -0.1178 1.4773 -0.3482 -0.0788 0.5250 -0.1157 1.5511 -0.3418 -0.0786 0.5500 -0.1132 1.6250 -0.3344 -0.0780 0.5750 -0.1103 1.6989 -0.3257 -0.0771 0.6000 -0.1069 1.7727 -0.3159 -0.0757 0.6250 -0.1030 1.8466 -0.3043 -0.0737 0.6500 -0.0983 1.9205 -0.2904 -0.0710 0.6750 -0.0928 1.9943 -0.2742 -0.0674 0.7000 -0.0867 2.0682 -0.2561 -0.0633 0.7250 -0.0801 2.1420 -0.2367 -0.0587 0.7500 -0.0732 2.2159 -0.2163 -0.0537 0.7750 -0.0660 2.2898 -0.1951 -0.0485 0.8000 -0.0586 2.3636 -0.1733 -0.0430 0.8250 -0.0511 2.4375 -0.1511 -0.0375 0.8500 -0.0435 2.5114 -0.1286 -0.0318 0.8750 -0.0359 2.5852 -0.1061 -0.0261 0.9000 -0.0283 2.6591 -0.0835 -0.0205 0.9250 -0.0207 2.7330 -0.0613 -0.0149 0.9500 -0.0135 2.8068 -0.0399 -0.0096 0.9750 -0.0067 2.8807 -0.0197 -0.0047 1.0000 0.0000 2.9545 0.0000 0.0000 1 y= -7.1591 y/(b/2) = -0.4773 chord= 3.0455 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.2544 0.1094 0.1700 0.1719 0.1146 0.2344 0.0710 0.2969 0.0332 0.3594 -0.0019 0.4219 -0.0360 0.4844 -0.0711 0.5469 -0.1094 0.6094 -0.1556 0.6719 -0.2322 0.7344 -0.2770 0.7969 -0.2996 0.8594 -0.3071 0.9219 -0.2993 0.9844 -0.2677 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0803 0.0000 -0.2445 0.0000 0.0250 -0.0867 0.0761 -0.2641 -0.0084 0.0500 -0.0931 0.1523 -0.2836 -0.0168 0.0750 -0.0991 0.2284 -0.3018 -0.0248 0.1000 -0.1042 0.3045 -0.3173 -0.0319 0.1250 -0.1084 0.3807 -0.3300 -0.0381 0.1500 -0.1119 0.4568 -0.3407 -0.0436 0.1750 -0.1149 0.5330 -0.3499 -0.0486 0.2000 -0.1175 0.6091 -0.3578 -0.0532 0.2250 -0.1196 0.6852 -0.3643 -0.0574 0.2500 -0.1214 0.7614 -0.3696 -0.0611 0.2750 -0.1227 0.8375 -0.3736 -0.0645 0.3000 -0.1236 0.9136 -0.3766 -0.0674 0.3250 -0.1243 0.9898 -0.3784 -0.0701 0.3500 -0.1245 1.0659 -0.3792 -0.0723 0.3750 -0.1244 1.1420 -0.3789 -0.0742 0.4000 -0.1240 1.2182 -0.3776 -0.0758 0.4250 -0.1232 1.2943 -0.3753 -0.0771 0.4500 -0.1221 1.3705 -0.3719 -0.0779 0.4750 -0.1206 1.4466 -0.3674 -0.0785 0.5000 -0.1188 1.5227 -0.3619 -0.0787 0.5250 -0.1166 1.5989 -0.3552 -0.0785 0.5500 -0.1140 1.6750 -0.3473 -0.0779 0.5750 -0.1111 1.7511 -0.3382 -0.0769 0.6000 -0.1077 1.8273 -0.3279 -0.0755 0.6250 -0.1037 1.9034 -0.3157 -0.0736 0.6500 -0.0989 1.9795 -0.3013 -0.0708 0.6750 -0.0934 2.0557 -0.2844 -0.0673 0.7000 -0.0872 2.1318 -0.2656 -0.0631 0.7250 -0.0806 2.2080 -0.2454 -0.0585 0.7500 -0.0736 2.2841 -0.2243 -0.0536 0.7750 -0.0664 2.3602 -0.2022 -0.0483 0.8000 -0.0590 2.4364 -0.1796 -0.0429 0.8250 -0.0514 2.5125 -0.1566 -0.0374 0.8500 -0.0438 2.5886 -0.1333 -0.0317 0.8750 -0.0361 2.6648 -0.1099 -0.0261 0.9000 -0.0284 2.7409 -0.0865 -0.0204 0.9250 -0.0209 2.8170 -0.0635 -0.0148 0.9500 -0.0136 2.8932 -0.0414 -0.0096 0.9750 -0.0067 2.9693 -0.0204 -0.0047 1.0000 0.0000 3.0455 0.0000 0.0000 1 y= -6.4773 y/(b/2) = -0.4318 chord= 3.1364 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.2510 0.1094 0.1668 0.1719 0.1116 0.2344 0.0681 0.2969 0.0304 0.3594 -0.0045 0.4219 -0.0385 0.4844 -0.0734 0.5469 -0.1115 0.6094 -0.1575 0.6719 -0.2337 0.7344 -0.2782 0.7969 -0.3007 0.8594 -0.3080 0.9219 -0.3002 0.9844 -0.2686 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0824 0.0000 -0.2585 0.0000 0.0250 -0.0887 0.0784 -0.2783 -0.0084 0.0500 -0.0951 0.1568 -0.2982 -0.0168 0.0750 -0.1010 0.2352 -0.3167 -0.0247 0.1000 -0.1060 0.3136 -0.3324 -0.0318 0.1250 -0.1101 0.3920 -0.3452 -0.0379 0.1500 -0.1135 0.4705 -0.3559 -0.0434 0.1750 -0.1164 0.5489 -0.3652 -0.0484 0.2000 -0.1190 0.6273 -0.3731 -0.0530 0.2250 -0.1210 0.7057 -0.3796 -0.0572 0.2500 -0.1227 0.7841 -0.3848 -0.0609 0.2750 -0.1239 0.8625 -0.3887 -0.0642 0.3000 -0.1248 0.9409 -0.3915 -0.0671 0.3250 -0.1254 1.0193 -0.3932 -0.0697 0.3500 -0.1256 1.0977 -0.3938 -0.0720 0.3750 -0.1254 1.1761 -0.3933 -0.0739 0.4000 -0.1249 1.2545 -0.3918 -0.0755 0.4250 -0.1241 1.3330 -0.3892 -0.0767 0.4500 -0.1229 1.4114 -0.3855 -0.0776 0.4750 -0.1214 1.4898 -0.3807 -0.0781 0.5000 -0.1195 1.5682 -0.3748 -0.0783 0.5250 -0.1172 1.6466 -0.3677 -0.0781 0.5500 -0.1146 1.7250 -0.3594 -0.0775 0.5750 -0.1116 1.8034 -0.3500 -0.0766 0.6000 -0.1081 1.8818 -0.3391 -0.0752 0.6250 -0.1041 1.9602 -0.3265 -0.0732 0.6500 -0.0993 2.0386 -0.3115 -0.0705 0.6750 -0.0937 2.1170 -0.2940 -0.0670 0.7000 -0.0875 2.1955 -0.2745 -0.0628 0.7250 -0.0809 2.2739 -0.2536 -0.0582 0.7500 -0.0739 2.3523 -0.2317 -0.0533 0.7750 -0.0666 2.4307 -0.2090 -0.0481 0.8000 -0.0592 2.5091 -0.1856 -0.0427 0.8250 -0.0516 2.5875 -0.1618 -0.0372 0.8500 -0.0439 2.6659 -0.1377 -0.0316 0.8750 -0.0362 2.7443 -0.1136 -0.0259 0.9000 -0.0285 2.8227 -0.0894 -0.0203 0.9250 -0.0209 2.9011 -0.0656 -0.0147 0.9500 -0.0136 2.9795 -0.0428 -0.0095 0.9750 -0.0067 3.0580 -0.0211 -0.0047 1.0000 0.0000 3.1364 0.0000 0.0000 1 y= -5.7955 y/(b/2) = -0.3864 chord= 3.2273 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.2467 0.1094 0.1630 0.1719 0.1082 0.2344 0.0649 0.2969 0.0275 0.3594 -0.0071 0.4219 -0.0409 0.4844 -0.0755 0.5469 -0.1133 0.6094 -0.1590 0.6719 -0.2347 0.7344 -0.2788 0.7969 -0.3010 0.8594 -0.3082 0.9219 -0.3003 0.9844 -0.2688 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0844 0.0000 -0.2723 0.0000 0.0250 -0.0906 0.0807 -0.2924 -0.0083 0.0500 -0.0968 0.1614 -0.3125 -0.0167 0.0750 -0.1026 0.2420 -0.3312 -0.0246 0.1000 -0.1075 0.3227 -0.3470 -0.0316 0.1250 -0.1115 0.4034 -0.3599 -0.0377 0.1500 -0.1148 0.4841 -0.3706 -0.0431 0.1750 -0.1177 0.5648 -0.3799 -0.0481 0.2000 -0.1201 0.6455 -0.3877 -0.0526 0.2250 -0.1221 0.7261 -0.3942 -0.0567 0.2500 -0.1237 0.8068 -0.3992 -0.0604 0.2750 -0.1249 0.8875 -0.4031 -0.0637 0.3000 -0.1257 0.9682 -0.4057 -0.0666 0.3250 -0.1262 1.0489 -0.4072 -0.0692 0.3500 -0.1263 1.1295 -0.4076 -0.0715 0.3750 -0.1261 1.2102 -0.4069 -0.0733 0.4000 -0.1255 1.2909 -0.4051 -0.0749 0.4250 -0.1246 1.3716 -0.4022 -0.0761 0.4500 -0.1234 1.4523 -0.3982 -0.0770 0.4750 -0.1218 1.5330 -0.3931 -0.0775 0.5000 -0.1199 1.6136 -0.3869 -0.0777 0.5250 -0.1176 1.6943 -0.3794 -0.0775 0.5500 -0.1149 1.7750 -0.3707 -0.0769 0.5750 -0.1118 1.8557 -0.3608 -0.0759 0.6000 -0.1083 1.9364 -0.3496 -0.0746 0.6250 -0.1042 2.0170 -0.3364 -0.0726 0.6500 -0.0994 2.0977 -0.3209 -0.0699 0.6750 -0.0938 2.1784 -0.3028 -0.0664 0.7000 -0.0876 2.2591 -0.2827 -0.0623 0.7250 -0.0809 2.3398 -0.2612 -0.0577 0.7500 -0.0739 2.4205 -0.2386 -0.0528 0.7750 -0.0667 2.5011 -0.2151 -0.0477 0.8000 -0.0592 2.5818 -0.1910 -0.0423 0.8250 -0.0516 2.6625 -0.1665 -0.0368 0.8500 -0.0439 2.7432 -0.1418 -0.0313 0.8750 -0.0362 2.8239 -0.1169 -0.0257 0.9000 -0.0285 2.9045 -0.0920 -0.0201 0.9250 -0.0209 2.9852 -0.0676 -0.0146 0.9500 -0.0136 3.0659 -0.0440 -0.0094 0.9750 -0.0067 3.1466 -0.0217 -0.0046 1.0000 0.0000 3.2273 0.0000 0.0000 1 y= -5.1136 y/(b/2) = -0.3409 chord= 3.3182 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.2416 0.1094 0.1587 0.1719 0.1042 0.2344 0.0614 0.2969 0.0243 0.3594 -0.0100 0.4219 -0.0434 0.4844 -0.0777 0.5469 -0.1151 0.6094 -0.1603 0.6719 -0.2352 0.7344 -0.2788 0.7969 -0.3008 0.8594 -0.3078 0.9219 -0.2999 0.9844 -0.2685 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0863 0.0000 -0.2865 0.0000 0.0250 -0.0924 0.0830 -0.3067 -0.0082 0.0500 -0.0985 0.1659 -0.3270 -0.0165 0.0750 -0.1042 0.2489 -0.3458 -0.0243 0.1000 -0.1090 0.3318 -0.3617 -0.0313 0.1250 -0.1129 0.4148 -0.3746 -0.0373 0.1500 -0.1161 0.4977 -0.3853 -0.0427 0.1750 -0.1189 0.5807 -0.3944 -0.0476 0.2000 -0.1212 0.6636 -0.4022 -0.0521 0.2250 -0.1231 0.7466 -0.4085 -0.0562 0.2500 -0.1246 0.8295 -0.4134 -0.0598 0.2750 -0.1257 0.9125 -0.4171 -0.0631 0.3000 -0.1264 0.9955 -0.4195 -0.0660 0.3250 -0.1268 1.0784 -0.4208 -0.0685 0.3500 -0.1269 1.1614 -0.4210 -0.0707 0.3750 -0.1266 1.2443 -0.4200 -0.0726 0.4000 -0.1259 1.3273 -0.4179 -0.0741 0.4250 -0.1250 1.4102 -0.4147 -0.0753 0.4500 -0.1237 1.4932 -0.4104 -0.0762 0.4750 -0.1221 1.5761 -0.4050 -0.0767 0.5000 -0.1201 1.6591 -0.3984 -0.0769 0.5250 -0.1177 1.7420 -0.3906 -0.0767 0.5500 -0.1150 1.8250 -0.3815 -0.0761 0.5750 -0.1119 1.9080 -0.3712 -0.0752 0.6000 -0.1083 1.9909 -0.3595 -0.0738 0.6250 -0.1042 2.0739 -0.3459 -0.0719 0.6500 -0.0994 2.1568 -0.3298 -0.0692 0.6750 -0.0938 2.2398 -0.3112 -0.0657 0.7000 -0.0875 2.3227 -0.2905 -0.0616 0.7250 -0.0809 2.4057 -0.2683 -0.0571 0.7500 -0.0739 2.4886 -0.2451 -0.0523 0.7750 -0.0666 2.5716 -0.2210 -0.0472 0.8000 -0.0591 2.6545 -0.1962 -0.0419 0.8250 -0.0515 2.7375 -0.1710 -0.0364 0.8500 -0.0439 2.8205 -0.1456 -0.0309 0.8750 -0.0362 2.9034 -0.1201 -0.0254 0.9000 -0.0285 2.9864 -0.0945 -0.0199 0.9250 -0.0209 3.0693 -0.0694 -0.0144 0.9500 -0.0136 3.1523 -0.0452 -0.0093 0.9750 -0.0067 3.2352 -0.0223 -0.0046 1.0000 0.0000 3.3182 0.0000 0.0000 1 y= -4.4318 y/(b/2) = -0.2955 chord= 3.4091 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.2357 0.1094 0.1535 0.1719 0.0997 0.2344 0.0573 0.2969 0.0206 0.3594 -0.0133 0.4219 -0.0463 0.4844 -0.0801 0.5469 -0.1171 0.6094 -0.1617 0.6719 -0.2357 0.7344 -0.2787 0.7969 -0.3003 0.8594 -0.3072 0.9219 -0.2992 0.9844 -0.2681 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0885 0.0000 -0.3018 0.0000 0.0250 -0.0945 0.0852 -0.3221 -0.0082 0.0500 -0.1004 0.1705 -0.3424 -0.0163 0.0750 -0.1060 0.2557 -0.3612 -0.0241 0.1000 -0.1106 0.3409 -0.3771 -0.0309 0.1250 -0.1144 0.4261 -0.3899 -0.0369 0.1500 -0.1175 0.5114 -0.4005 -0.0422 0.1750 -0.1201 0.5966 -0.4095 -0.0471 0.2000 -0.1223 0.6818 -0.4171 -0.0515 0.2250 -0.1241 0.7670 -0.4232 -0.0555 0.2500 -0.1255 0.8523 -0.4279 -0.0591 0.2750 -0.1265 0.9375 -0.4314 -0.0623 0.3000 -0.1272 1.0227 -0.4336 -0.0652 0.3250 -0.1275 1.1080 -0.4346 -0.0677 0.3500 -0.1274 1.1932 -0.4344 -0.0699 0.3750 -0.1271 1.2784 -0.4332 -0.0717 0.4000 -0.1264 1.3636 -0.4308 -0.0732 0.4250 -0.1253 1.4489 -0.4272 -0.0744 0.4500 -0.1240 1.5341 -0.4226 -0.0753 0.4750 -0.1223 1.6193 -0.4168 -0.0758 0.5000 -0.1202 1.7045 -0.4098 -0.0759 0.5250 -0.1178 1.7898 -0.4016 -0.0757 0.5500 -0.1150 1.8750 -0.3921 -0.0752 0.5750 -0.1119 1.9602 -0.3813 -0.0742 0.6000 -0.1083 2.0455 -0.3691 -0.0729 0.6250 -0.1041 2.1307 -0.3550 -0.0709 0.6500 -0.0993 2.2159 -0.3385 -0.0683 0.6750 -0.0937 2.3011 -0.3193 -0.0649 0.7000 -0.0874 2.3864 -0.2980 -0.0608 0.7250 -0.0807 2.4716 -0.2752 -0.0564 0.7500 -0.0737 2.5568 -0.2513 -0.0516 0.7750 -0.0665 2.6420 -0.2266 -0.0465 0.8000 -0.0590 2.7273 -0.2012 -0.0413 0.8250 -0.0514 2.8125 -0.1754 -0.0359 0.8500 -0.0438 2.8977 -0.1493 -0.0305 0.8750 -0.0361 2.9830 -0.1231 -0.0250 0.9000 -0.0284 3.0682 -0.0969 -0.0196 0.9250 -0.0209 3.1534 -0.0712 -0.0142 0.9500 -0.0136 3.2386 -0.0464 -0.0092 0.9750 -0.0067 3.3239 -0.0229 -0.0045 1.0000 0.0000 3.4091 0.0000 0.0000 1 y= -3.7500 y/(b/2) = -0.2500 chord= 3.5000 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.2287 0.1094 0.1475 0.1719 0.0943 0.2344 0.0525 0.2969 0.0163 0.3594 -0.0172 0.4219 -0.0497 0.4844 -0.0830 0.5469 -0.1194 0.6094 -0.1634 0.6719 -0.2363 0.7344 -0.2787 0.7969 -0.2999 0.8594 -0.3065 0.9219 -0.2985 0.9844 -0.2677 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0912 0.0000 -0.3191 0.0000 0.0250 -0.0969 0.0875 -0.3393 -0.0080 0.0500 -0.1027 0.1750 -0.3595 -0.0161 0.0750 -0.1081 0.2625 -0.3782 -0.0237 0.1000 -0.1126 0.3500 -0.3939 -0.0305 0.1250 -0.1162 0.4375 -0.4065 -0.0364 0.1500 -0.1191 0.5250 -0.4169 -0.0416 0.1750 -0.1216 0.6125 -0.4257 -0.0464 0.2000 -0.1237 0.7000 -0.4331 -0.0508 0.2250 -0.1254 0.7875 -0.4389 -0.0548 0.2500 -0.1267 0.8750 -0.4433 -0.0583 0.2750 -0.1276 0.9625 -0.4464 -0.0615 0.3000 -0.1281 1.0500 -0.4483 -0.0643 0.3250 -0.1283 1.1375 -0.4490 -0.0668 0.3500 -0.1281 1.2250 -0.4485 -0.0689 0.3750 -0.1277 1.3125 -0.4469 -0.0707 0.4000 -0.1269 1.4000 -0.4441 -0.0722 0.4250 -0.1258 1.4875 -0.4402 -0.0733 0.4500 -0.1243 1.5750 -0.4351 -0.0742 0.4750 -0.1225 1.6625 -0.4289 -0.0747 0.5000 -0.1204 1.7500 -0.4215 -0.0748 0.5250 -0.1179 1.8375 -0.4128 -0.0746 0.5500 -0.1151 1.9250 -0.4028 -0.0741 0.5750 -0.1119 2.0125 -0.3916 -0.0731 0.6000 -0.1083 2.1000 -0.3789 -0.0718 0.6250 -0.1041 2.1875 -0.3643 -0.0699 0.6500 -0.0992 2.2750 -0.3471 -0.0673 0.6750 -0.0935 2.3625 -0.3274 -0.0639 0.7000 -0.0873 2.4500 -0.3055 -0.0599 0.7250 -0.0806 2.5375 -0.2821 -0.0555 0.7500 -0.0736 2.6250 -0.2576 -0.0508 0.7750 -0.0663 2.7125 -0.2322 -0.0458 0.8000 -0.0589 2.8000 -0.2061 -0.0407 0.8250 -0.0513 2.8875 -0.1797 -0.0354 0.8500 -0.0437 2.9750 -0.1530 -0.0300 0.8750 -0.0360 3.0625 -0.1261 -0.0246 0.9000 -0.0284 3.1500 -0.0993 -0.0193 0.9250 -0.0208 3.2375 -0.0729 -0.0140 0.9500 -0.0136 3.3250 -0.0476 -0.0090 0.9750 -0.0067 3.4125 -0.0235 -0.0044 1.0000 0.0000 3.5000 0.0000 0.0000 1 y= -3.0682 y/(b/2) = -0.2045 chord= 3.5909 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.2203 0.1094 0.1403 0.1719 0.0878 0.2344 0.0466 0.2969 0.0109 0.3594 -0.0219 0.4219 -0.0539 0.4844 -0.0867 0.5469 -0.1224 0.6094 -0.1656 0.6719 -0.2373 0.7344 -0.2789 0.7969 -0.2995 0.8594 -0.3059 0.9219 -0.2979 0.9844 -0.2673 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0944 0.0000 -0.3391 0.0000 0.0250 -0.1000 0.0898 -0.3591 -0.0079 0.0500 -0.1056 0.1795 -0.3790 -0.0158 0.0750 -0.1107 0.2693 -0.3975 -0.0234 0.1000 -0.1150 0.3591 -0.4130 -0.0300 0.1250 -0.1184 0.4489 -0.4253 -0.0358 0.1500 -0.1212 0.5386 -0.4353 -0.0410 0.1750 -0.1236 0.6284 -0.4437 -0.0457 0.2000 -0.1255 0.7182 -0.4507 -0.0500 0.2250 -0.1270 0.8080 -0.4562 -0.0538 0.2500 -0.1281 0.8977 -0.4602 -0.0573 0.2750 -0.1289 0.9875 -0.4629 -0.0604 0.3000 -0.1293 1.0773 -0.4643 -0.0632 0.3250 -0.1294 1.1670 -0.4645 -0.0656 0.3500 -0.1291 1.2568 -0.4636 -0.0677 0.3750 -0.1285 1.3466 -0.4615 -0.0695 0.4000 -0.1276 1.4364 -0.4582 -0.0709 0.4250 -0.1264 1.5261 -0.4538 -0.0721 0.4500 -0.1248 1.6159 -0.4482 -0.0729 0.4750 -0.1230 1.7057 -0.4415 -0.0734 0.5000 -0.1207 1.7955 -0.4336 -0.0735 0.5250 -0.1182 1.8852 -0.4244 -0.0733 0.5500 -0.1152 1.9750 -0.4138 -0.0728 0.5750 -0.1120 2.0648 -0.4021 -0.0718 0.6000 -0.1083 2.1545 -0.3888 -0.0705 0.6250 -0.1041 2.2443 -0.3737 -0.0686 0.6500 -0.0991 2.3341 -0.3559 -0.0661 0.6750 -0.0934 2.4239 -0.3355 -0.0627 0.7000 -0.0872 2.5136 -0.3130 -0.0588 0.7250 -0.0805 2.6034 -0.2890 -0.0545 0.7500 -0.0735 2.6932 -0.2638 -0.0499 0.7750 -0.0662 2.7830 -0.2378 -0.0450 0.8000 -0.0588 2.8727 -0.2111 -0.0399 0.8250 -0.0512 2.9625 -0.1840 -0.0347 0.8500 -0.0436 3.0523 -0.1566 -0.0295 0.8750 -0.0360 3.1420 -0.1292 -0.0242 0.9000 -0.0283 3.2318 -0.1017 -0.0189 0.9250 -0.0208 3.3216 -0.0747 -0.0137 0.9500 -0.0136 3.4114 -0.0487 -0.0088 0.9750 -0.0067 3.5011 -0.0240 -0.0043 1.0000 0.0000 3.5909 0.0000 0.0000 1 y= -2.3864 y/(b/2) = -0.1591 chord= 3.6818 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.2098 0.1094 0.1310 0.1719 0.0793 0.2344 0.0387 0.2969 0.0037 0.3594 -0.0286 0.4219 -0.0599 0.4844 -0.0920 0.5469 -0.1269 0.6094 -0.1692 0.6719 -0.2394 0.7344 -0.2801 0.7969 -0.3001 0.8594 -0.3061 0.9219 -0.2979 0.9844 -0.2676 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0992 0.0000 -0.3654 0.0000 0.0250 -0.1045 0.0920 -0.3848 -0.0078 0.0500 -0.1098 0.1841 -0.4044 -0.0156 0.0750 -0.1147 0.2761 -0.4224 -0.0229 0.1000 -0.1188 0.3682 -0.4373 -0.0295 0.1250 -0.1220 0.4602 -0.4491 -0.0351 0.1500 -0.1245 0.5523 -0.4585 -0.0402 0.1750 -0.1267 0.6443 -0.4664 -0.0448 0.2000 -0.1284 0.7364 -0.4727 -0.0490 0.2250 -0.1297 0.8284 -0.4776 -0.0528 0.2500 -0.1306 0.9205 -0.4810 -0.0562 0.2750 -0.1312 1.0125 -0.4830 -0.0593 0.3000 -0.1314 1.1045 -0.4838 -0.0619 0.3250 -0.1313 1.1966 -0.4834 -0.0643 0.3500 -0.1309 1.2886 -0.4818 -0.0664 0.3750 -0.1301 1.3807 -0.4790 -0.0681 0.4000 -0.1290 1.4727 -0.4751 -0.0695 0.4250 -0.1277 1.5648 -0.4700 -0.0706 0.4500 -0.1260 1.6568 -0.4638 -0.0714 0.4750 -0.1240 1.7489 -0.4564 -0.0719 0.5000 -0.1216 1.8409 -0.4478 -0.0720 0.5250 -0.1189 1.9330 -0.4378 -0.0718 0.5500 -0.1159 2.0250 -0.4266 -0.0712 0.5750 -0.1125 2.1170 -0.4142 -0.0703 0.6000 -0.1087 2.2091 -0.4002 -0.0690 0.6250 -0.1044 2.3011 -0.3844 -0.0672 0.6500 -0.0994 2.3932 -0.3659 -0.0646 0.6750 -0.0936 2.4852 -0.3448 -0.0614 0.7000 -0.0873 2.5773 -0.3215 -0.0576 0.7250 -0.0806 2.6693 -0.2967 -0.0533 0.7500 -0.0736 2.7614 -0.2708 -0.0487 0.7750 -0.0663 2.8534 -0.2440 -0.0440 0.8000 -0.0588 2.9455 -0.2166 -0.0390 0.8250 -0.0513 3.0375 -0.1888 -0.0339 0.8500 -0.0436 3.1295 -0.1607 -0.0288 0.8750 -0.0360 3.2216 -0.1325 -0.0236 0.9000 -0.0283 3.3136 -0.1044 -0.0184 0.9250 -0.0208 3.4057 -0.0766 -0.0134 0.9500 -0.0136 3.4977 -0.0500 -0.0086 0.9750 -0.0067 3.5898 -0.0247 -0.0042 1.0000 0.0000 3.6818 0.0000 0.0000 1 y= -1.7045 y/(b/2) = -0.1136 chord= 3.7727 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.1956 0.1094 0.1178 0.1719 0.0668 0.2344 0.0269 0.2969 -0.0075 0.3594 -0.0391 0.4219 -0.0697 0.4844 -0.1009 0.5469 -0.1348 0.6094 -0.1759 0.6719 -0.2444 0.7344 -0.2837 0.7969 -0.3029 0.8594 -0.3082 0.9219 -0.2997 0.9844 -0.2694 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.1072 0.0000 -0.4043 0.0000 0.0250 -0.1121 0.0943 -0.4229 -0.0076 0.0500 -0.1170 0.1886 -0.4415 -0.0152 0.0750 -0.1216 0.2830 -0.4587 -0.0225 0.1000 -0.1253 0.3773 -0.4727 -0.0289 0.1250 -0.1282 0.4716 -0.4835 -0.0344 0.1500 -0.1304 0.5659 -0.4920 -0.0393 0.1750 -0.1322 0.6602 -0.4989 -0.0438 0.2000 -0.1336 0.7545 -0.5042 -0.0479 0.2250 -0.1347 0.8489 -0.5081 -0.0516 0.2500 -0.1353 0.9432 -0.5104 -0.0549 0.2750 -0.1356 1.0375 -0.5114 -0.0579 0.3000 -0.1355 1.1318 -0.5112 -0.0605 0.3250 -0.1351 1.2261 -0.5097 -0.0628 0.3500 -0.1344 1.3205 -0.5071 -0.0647 0.3750 -0.1334 1.4148 -0.5032 -0.0664 0.4000 -0.1321 1.5091 -0.4982 -0.0678 0.4250 -0.1304 1.6034 -0.4921 -0.0688 0.4500 -0.1285 1.6977 -0.4848 -0.0696 0.4750 -0.1263 1.7920 -0.4763 -0.0700 0.5000 -0.1237 1.8864 -0.4667 -0.0701 0.5250 -0.1208 1.9807 -0.4557 -0.0699 0.5500 -0.1175 2.0750 -0.4435 -0.0693 0.5750 -0.1140 2.1693 -0.4300 -0.0684 0.6000 -0.1100 2.2636 -0.4150 -0.0671 0.6250 -0.1055 2.3580 -0.3981 -0.0653 0.6500 -0.1004 2.4523 -0.3786 -0.0629 0.6750 -0.0945 2.5466 -0.3565 -0.0597 0.7000 -0.0881 2.6409 -0.3322 -0.0559 0.7250 -0.0812 2.7352 -0.3065 -0.0518 0.7500 -0.0741 2.8295 -0.2796 -0.0473 0.7750 -0.0668 2.9239 -0.2518 -0.0426 0.8000 -0.0592 3.0182 -0.2235 -0.0378 0.8250 -0.0516 3.1125 -0.1947 -0.0328 0.8500 -0.0439 3.2068 -0.1657 -0.0278 0.8750 -0.0362 3.3011 -0.1366 -0.0228 0.9000 -0.0285 3.3955 -0.1076 -0.0178 0.9250 -0.0209 3.4898 -0.0790 -0.0129 0.9500 -0.0137 3.5841 -0.0516 -0.0083 0.9750 -0.0067 3.6784 -0.0254 -0.0041 1.0000 0.0000 3.7727 0.0000 0.0000 1 y= -1.0227 y/(b/2) = -0.0682 chord= 3.8636 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.1731 0.1094 0.0957 0.1719 0.0450 0.2344 0.0053 0.2969 -0.0286 0.3594 -0.0595 0.4219 -0.0892 0.4844 -0.1191 0.5469 -0.1516 0.6094 -0.1907 0.6719 -0.2566 0.7344 -0.2938 0.7969 -0.3112 0.8594 -0.3150 0.9219 -0.3053 0.9844 -0.2745 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.1229 0.0000 -0.4747 0.0000 0.0250 -0.1272 0.0966 -0.4916 -0.0074 0.0500 -0.1316 0.1932 -0.5085 -0.0149 0.0750 -0.1356 0.2898 -0.5239 -0.0220 0.1000 -0.1388 0.3864 -0.5361 -0.0282 0.1250 -0.1411 0.4830 -0.5451 -0.0336 0.1500 -0.1428 0.5795 -0.5516 -0.0383 0.1750 -0.1440 0.6761 -0.5565 -0.0427 0.2000 -0.1449 0.7727 -0.5599 -0.0466 0.2250 -0.1454 0.8693 -0.5618 -0.0502 0.2500 -0.1455 0.9659 -0.5621 -0.0533 0.2750 -0.1452 1.0625 -0.5611 -0.0561 0.3000 -0.1446 1.1591 -0.5588 -0.0586 0.3250 -0.1437 1.2557 -0.5552 -0.0608 0.3500 -0.1425 1.3523 -0.5505 -0.0626 0.3750 -0.1410 1.4489 -0.5446 -0.0642 0.4000 -0.1391 1.5455 -0.5376 -0.0654 0.4250 -0.1370 1.6420 -0.5294 -0.0664 0.4500 -0.1346 1.7386 -0.5201 -0.0670 0.4750 -0.1319 1.8352 -0.5096 -0.0674 0.5000 -0.1289 1.9318 -0.4979 -0.0674 0.5250 -0.1255 2.0284 -0.4850 -0.0672 0.5500 -0.1219 2.1250 -0.4708 -0.0666 0.5750 -0.1179 2.2216 -0.4554 -0.0657 0.6000 -0.1135 2.3182 -0.4386 -0.0644 0.6250 -0.1087 2.4148 -0.4199 -0.0626 0.6500 -0.1032 2.5114 -0.3986 -0.0602 0.6750 -0.0970 2.6080 -0.3747 -0.0571 0.7000 -0.0903 2.7045 -0.3488 -0.0534 0.7250 -0.0832 2.8011 -0.3213 -0.0494 0.7500 -0.0758 2.8977 -0.2928 -0.0451 0.7750 -0.0682 2.9943 -0.2635 -0.0406 0.8000 -0.0605 3.0909 -0.2336 -0.0359 0.8250 -0.0526 3.1875 -0.2034 -0.0311 0.8500 -0.0448 3.2841 -0.1730 -0.0263 0.8750 -0.0369 3.3807 -0.1426 -0.0215 0.9000 -0.0291 3.4773 -0.1123 -0.0168 0.9250 -0.0213 3.5739 -0.0824 -0.0121 0.9500 -0.0139 3.6705 -0.0538 -0.0078 0.9750 -0.0069 3.7670 -0.0265 -0.0038 1.0000 0.0000 3.8636 0.0000 0.0000 1 y= -0.3409 y/(b/2) = -0.0227 chord= 3.9545 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.1183 0.1094 0.0373 0.1719 -0.0158 0.2344 -0.0567 0.2969 -0.0910 0.3594 -0.1215 0.4219 -0.1499 0.4844 -0.1778 0.5469 -0.2072 0.6094 -0.2419 0.6719 -0.3015 0.7344 -0.3319 0.7969 -0.3424 0.8594 -0.3397 0.9219 -0.3243 0.9844 -0.2892 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.1709 0.0000 -0.6760 0.0000 0.0250 -0.1739 0.0989 -0.6879 -0.0073 0.0500 -0.1770 0.1977 -0.6998 -0.0146 0.0750 -0.1796 0.2966 -0.7101 -0.0214 0.1000 -0.1813 0.3955 -0.7169 -0.0275 0.1250 -0.1821 0.4943 -0.7203 -0.0326 0.1500 -0.1824 0.5932 -0.7211 -0.0371 0.1750 -0.1821 0.6920 -0.7202 -0.0411 0.2000 -0.1815 0.7909 -0.7176 -0.0447 0.2250 -0.1804 0.8898 -0.7134 -0.0479 0.2500 -0.1789 0.9886 -0.7076 -0.0507 0.2750 -0.1771 1.0875 -0.7004 -0.0532 0.3000 -0.1749 1.1864 -0.6918 -0.0553 0.3250 -0.1725 1.2852 -0.6821 -0.0571 0.3500 -0.1697 1.3841 -0.6711 -0.0586 0.3750 -0.1666 1.4830 -0.6589 -0.0598 0.4000 -0.1633 1.5818 -0.6456 -0.0607 0.4250 -0.1596 1.6807 -0.6312 -0.0613 0.4500 -0.1557 1.7795 -0.6157 -0.0617 0.4750 -0.1515 1.8784 -0.5991 -0.0618 0.5000 -0.1470 1.9773 -0.5814 -0.0616 0.5250 -0.1422 2.0761 -0.5625 -0.0610 0.5500 -0.1372 2.1750 -0.5425 -0.0602 0.5750 -0.1318 2.2739 -0.5213 -0.0592 0.6000 -0.1261 2.3727 -0.4988 -0.0578 0.6250 -0.1200 2.4716 -0.4746 -0.0559 0.6500 -0.1133 2.5705 -0.4481 -0.0535 0.6750 -0.1060 2.6693 -0.4191 -0.0504 0.7000 -0.0982 2.7682 -0.3882 -0.0469 0.7250 -0.0901 2.8670 -0.3561 -0.0431 0.7500 -0.0817 2.9659 -0.3233 -0.0390 0.7750 -0.0733 3.0648 -0.2898 -0.0348 0.8000 -0.0647 3.1636 -0.2560 -0.0306 0.8250 -0.0562 3.2625 -0.2222 -0.0263 0.8500 -0.0476 3.3614 -0.1884 -0.0220 0.8750 -0.0392 3.4602 -0.1548 -0.0178 0.9000 -0.0308 3.5591 -0.1216 -0.0137 0.9250 -0.0225 3.6580 -0.0891 -0.0097 0.9500 -0.0147 3.7568 -0.0581 -0.0061 0.9750 -0.0072 3.8557 -0.0286 -0.0030 1.0000 0.0000 3.9545 0.0000 0.0000 1 twist table i y y/(b/2) twist 1 -14.65909 -0.97727 -0.93214 2 -13.97727 -0.93182 1.40810 3 -13.29545 -0.88636 2.14216 4 -12.61364 -0.84091 2.68619 5 -11.93182 -0.79545 3.11652 6 -11.25000 -0.75000 3.46716 7 -10.56818 -0.70455 3.73306 8 -9.88636 -0.65909 3.96142 9 -9.20455 -0.61364 4.15675 10 -8.52273 -0.56818 4.32319 11 -7.84091 -0.52273 4.46291 12 -7.15909 -0.47727 4.59056 13 -6.47727 -0.43182 4.71150 14 -5.79546 -0.38636 4.82281 15 -5.11364 -0.34091 4.93510 16 -4.43182 -0.29545 5.05965 17 -3.75000 -0.25000 5.20895 18 -3.06818 -0.20455 5.39483 19 -2.38637 -0.15909 5.66716 20 -1.70455 -0.11364 6.11619 21 -1.02273 -0.06818 7.00442 22 -0.34091 -0.02273 9.70040 calculation complete williams-imac:LAMDESfolder williamhmason$