williams-imac:LAMDESfolder williamhmason$ ./LamDes2 enter name of input file: LamDesTNsamp.inp Lamar Design Code mods by W.H. Mason Lamar program sample input - TN D-8990 canard example plan = 2.0 xmref = -0.0000 cref = 9.1800 tdklue = 0.0 case = 0.0 spnklu = 0.0 sref = 160.0000 1st REFERENCE PLANFORM HAS 3 CURVES ROOT CHORD HEIGHT = -1.0000 POINT X Y SWEEP DIHEDRAL REF REF ANGLE ANGLE 1 14.5700 0.0000 52.71754 0.00000 2 5.7300 -6.7300 90.00000 0.00000 3 4.2900 -6.7300 12.40255 0.00000 4 5.7700 0.0000 2nd REFERENCE PLANFORM HAS 3 CURVES ROOT CHORD HEIGHT = 0.0000 POINT X Y SWEEP DIHEDRAL REF REF ANGLE ANGLE 1 5.2900 0.0000 44.24539 0.00000 2 -4.4500 -10.0000 90.00000 0.00000 3 -6.6100 -10.0000 -8.58679 0.00000 4 -8.1200 0.0000 scw = 16.0 vic = 15.0 xitmax = 0.0 epsmax = 0.00000 CONFIGURATION NO. 2. delta ord shift for moment = -0.0000 CURVE 1 IS SWEPT 52.7175 DEGREES ON PLANFORM 1 CURVE 1 IS SWEPT 44.2454 DEGREES ON PLANFORM 2 BREAK POINTS FOR THIS CONFIGURATION POINT X Y Z SWEEP DIHEDRAL ANGLE ANGLE 1 14.5700 0.0000 -1.0000 52.7175 0.0000 2 5.7300 -6.7300 -1.0000 90.0000 0.0000 3 4.2900 -6.7300 -1.0000 12.4025 0.0000 4 5.7700 0.0000 -1.0000 SECOND PLANFORM BREAK POINTS 1 5.2900 0.0000 0.0000 44.2454 0.0000 2 -1.2650 -6.7300 0.0000 44.2454 0.0000 3 -4.4500 -10.0000 0.0000 90.0000 0.0000 4 -6.6100 -10.0000 0.0000 -8.5868 0.0000 5 -8.1200 0.0000 0.0000 a = 0.000 clmin = 0.000 cd0 =0.0000 400 HORSESHOE VORTICES USED PLANFORM TOTAL SPANWISE 1 160 10 2 240 15 16. HORSESHOE VORTICES IN EACH CHORDWISE ROW xcfw = 0.60 xcft = 0.80 fkon = 0.00 ficam = 1.00 punch = 0.00 crbmnt = 0.000 cmb = 0.00 iflag = 1 relax = 0.00 fioutw = 1.00 cd0 = 0.0000 firbm = 0.00 yrbm = 0.0000 zrbm = 0.0000 induced drag cd = 0.00401 pressure drag cdpt = 0.00000 induced drag alone was minimized on this run ref. chord = 9.180 c average = 8.0000 true area = 224.615 ref. area = 160.000 b/2 = 10.0000 ref ar = 2.5000 true ar = 1.7808 Mach number = 0.3000 first planform cl = 0.04917 cm = 0.04617 cb = -0.00681 second planform cl = 0.15083 cm = -0.04617 cb = -0.03411 1st planform CL = 0.0494 CDP = 0.0000 CM = 0.0463 CB = -0.0069 2nd planform CL = 0.1510 CDP = 0.0000 CM = -0.0463 CB = 0.0000 no root bending moment constraint CL DES = 0.20000 CL COMPUTED = 0.2004 CM = -0.0000 CD I = 0.00401 E = 1.2742 CDPRESS = 0.00000 CDTOTAL = 0.00401 first planform Y CL*C/CAVE C/CAVE CL CD -6.3967 0.02291 0.22557 0.10157 0.00000 -5.7300 0.04442 0.31670 0.14027 0.00000 -5.0633 0.05847 0.40784 0.14337 0.00000 -4.3967 0.06925 0.49897 0.13878 0.00000 -3.7300 0.07774 0.59010 0.13174 0.00000 -3.0633 0.08435 0.68124 0.12382 0.00000 -2.3967 0.08937 0.77237 0.11571 0.00000 -1.7300 0.09300 0.86351 0.10770 0.00000 -1.0633 0.09534 0.95464 0.09987 0.00000 -0.3650 0.09652 1.05011 0.09192 0.00000 second planform -9.6667 0.06198 0.31687 0.19559 0.00000 -9.0000 0.10043 0.41063 0.24457 0.00000 -8.3333 0.12546 0.50438 0.24874 0.00000 -7.6667 0.14335 0.59813 0.23967 0.00000 -7.0317 0.15469 0.68742 0.22503 0.00000 -6.3967 0.16077 0.77672 0.20698 0.00000 -5.7300 0.16350 0.87047 0.18783 0.00000 -5.0633 0.16515 0.96422 0.17128 0.00000 -4.3967 0.16662 1.05797 0.15749 0.00000 -3.7300 0.16798 1.15172 0.14585 0.00000 -3.0633 0.16919 1.24547 0.13584 0.00000 -2.3967 0.17020 1.33922 0.12709 0.00000 -1.7300 0.17099 1.43297 0.11933 0.00000 -1.0633 0.17152 1.52672 0.11235 0.00000 -0.3650 0.17179 1.62492 0.10572 0.00000 mean camber lines to obtain the spanload (subsonic linear theory) y= -6.3967 y/(b/2) = -0.6397 chord= 1.8045 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.0635 0.1094 0.0523 0.1719 0.0455 0.2344 0.0405 0.2969 0.0363 0.3594 0.0323 0.4219 0.0283 0.4844 0.0240 0.5469 0.0190 0.6094 0.0117 0.6719 0.0061 0.7344 0.0029 0.7969 0.0010 0.8594 0.0002 0.9219 0.0006 0.9844 0.0030 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 0.0239 0.0000 0.0431 0.0000 0.0250 0.0223 0.0451 0.0402 -0.0010 0.0500 0.0207 0.0902 0.0373 -0.0020 0.0750 0.0192 0.1353 0.0346 -0.0029 0.1000 0.0177 0.1805 0.0320 -0.0038 0.1250 0.0164 0.2256 0.0297 -0.0045 0.1500 0.0152 0.2707 0.0275 -0.0051 0.1750 0.0141 0.3158 0.0254 -0.0056 0.2000 0.0130 0.3609 0.0234 -0.0061 0.2250 0.0119 0.4060 0.0215 -0.0066 0.2500 0.0109 0.4511 0.0197 -0.0070 0.2750 0.0099 0.4962 0.0179 -0.0074 0.3000 0.0090 0.5414 0.0163 -0.0077 0.3250 0.0081 0.5865 0.0147 -0.0080 0.3500 0.0073 0.6316 0.0132 -0.0082 0.3750 0.0065 0.6767 0.0117 -0.0084 0.4000 0.0057 0.7218 0.0103 -0.0086 0.4250 0.0050 0.7669 0.0090 -0.0087 0.4500 0.0043 0.8120 0.0078 -0.0088 0.4750 0.0037 0.8572 0.0067 -0.0088 0.5000 0.0031 0.9023 0.0056 -0.0088 0.5250 0.0025 0.9474 0.0046 -0.0088 0.5500 0.0021 0.9925 0.0037 -0.0087 0.5750 0.0016 1.0376 0.0029 -0.0085 0.6000 0.0013 1.0827 0.0023 -0.0083 0.6250 0.0010 1.1278 0.0018 -0.0080 0.6500 0.0008 1.1729 0.0014 -0.0076 0.6750 0.0006 1.2181 0.0011 -0.0072 0.7000 0.0005 1.2632 0.0008 -0.0067 0.7250 0.0004 1.3083 0.0007 -0.0062 0.7500 0.0003 1.3534 0.0005 -0.0057 0.7750 0.0002 1.3985 0.0004 -0.0051 0.8000 0.0002 1.4436 0.0004 -0.0046 0.8250 0.0002 1.4887 0.0004 -0.0040 0.8500 0.0002 1.5339 0.0003 -0.0034 0.8750 0.0002 1.5790 0.0003 -0.0028 0.9000 0.0002 1.6241 0.0003 -0.0022 0.9250 0.0002 1.6692 0.0003 -0.0016 0.9500 0.0001 1.7143 0.0002 -0.0011 0.9750 0.0001 1.7594 0.0001 -0.0005 1.0000 0.0000 1.8045 0.0000 0.0000 1 y= -5.7300 y/(b/2) = -0.5730 chord= 2.5336 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.0608 0.1094 0.0442 0.1719 0.0338 0.2344 0.0257 0.2969 0.0187 0.3594 0.0121 0.4219 0.0057 0.4844 -0.0009 0.5469 -0.0083 0.6094 -0.0187 0.6719 -0.0267 0.7344 -0.0313 0.7969 -0.0340 0.8594 -0.0350 0.9219 -0.0344 0.9844 -0.0311 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 0.0002 0.0000 0.0005 0.0000 0.0250 -0.0013 0.0633 -0.0033 -0.0015 0.0500 -0.0028 0.1267 -0.0072 -0.0030 0.0750 -0.0043 0.1900 -0.0109 -0.0045 0.1000 -0.0056 0.2534 -0.0141 -0.0058 0.1250 -0.0067 0.3167 -0.0169 -0.0068 0.1500 -0.0076 0.3800 -0.0193 -0.0078 0.1750 -0.0085 0.4434 -0.0215 -0.0087 0.2000 -0.0093 0.5067 -0.0235 -0.0095 0.2250 -0.0100 0.5701 -0.0253 -0.0102 0.2500 -0.0106 0.6334 -0.0269 -0.0108 0.2750 -0.0112 0.6967 -0.0284 -0.0113 0.3000 -0.0117 0.7601 -0.0296 -0.0118 0.3250 -0.0121 0.8234 -0.0307 -0.0122 0.3500 -0.0125 0.8868 -0.0316 -0.0126 0.3750 -0.0128 0.9501 -0.0323 -0.0129 0.4000 -0.0130 1.0134 -0.0329 -0.0131 0.4250 -0.0132 1.0768 -0.0333 -0.0133 0.4500 -0.0133 1.1401 -0.0336 -0.0134 0.4750 -0.0133 1.2035 -0.0337 -0.0134 0.5000 -0.0133 1.2668 -0.0336 -0.0134 0.5250 -0.0132 1.3301 -0.0334 -0.0133 0.5500 -0.0130 1.3935 -0.0329 -0.0131 0.5750 -0.0127 1.4568 -0.0322 -0.0128 0.6000 -0.0124 1.5202 -0.0313 -0.0124 0.6250 -0.0119 1.5835 -0.0301 -0.0120 0.6500 -0.0113 1.6468 -0.0286 -0.0114 0.6750 -0.0107 1.7102 -0.0270 -0.0107 0.7000 -0.0100 1.7735 -0.0252 -0.0100 0.7250 -0.0092 1.8369 -0.0233 -0.0093 0.7500 -0.0084 1.9002 -0.0213 -0.0085 0.7750 -0.0076 1.9636 -0.0193 -0.0077 0.8000 -0.0068 2.0269 -0.0171 -0.0068 0.8250 -0.0059 2.0902 -0.0150 -0.0059 0.8500 -0.0050 2.1536 -0.0128 -0.0051 0.8750 -0.0042 2.2169 -0.0105 -0.0042 0.9000 -0.0033 2.2803 -0.0083 -0.0033 0.9250 -0.0024 2.3436 -0.0061 -0.0024 0.9500 -0.0016 2.4069 -0.0040 -0.0016 0.9750 -0.0008 2.4703 -0.0020 -0.0008 1.0000 0.0000 2.5336 0.0000 0.0000 1 y= -5.0633 y/(b/2) = -0.5063 chord= 3.2627 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.0545 0.1094 0.0374 0.1719 0.0266 0.2344 0.0182 0.2969 0.0111 0.3594 0.0045 0.4219 -0.0017 0.4844 -0.0081 0.5469 -0.0153 0.6094 -0.0254 0.6719 -0.0332 0.7344 -0.0373 0.7969 -0.0395 0.8594 -0.0401 0.9219 -0.0390 0.9844 -0.0353 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0063 0.0000 -0.0205 -0.0000 0.0250 -0.0077 0.0816 -0.0250 -0.0015 0.0500 -0.0090 0.1631 -0.0295 -0.0031 0.0750 -0.0103 0.2447 -0.0336 -0.0045 0.1000 -0.0114 0.3263 -0.0372 -0.0058 0.1250 -0.0123 0.4078 -0.0402 -0.0068 0.1500 -0.0131 0.4894 -0.0428 -0.0078 0.1750 -0.0138 0.5710 -0.0451 -0.0086 0.2000 -0.0144 0.6525 -0.0471 -0.0094 0.2250 -0.0150 0.7341 -0.0488 -0.0101 0.2500 -0.0154 0.8157 -0.0503 -0.0107 0.2750 -0.0158 0.8972 -0.0515 -0.0112 0.3000 -0.0161 0.9788 -0.0524 -0.0117 0.3250 -0.0163 1.0604 -0.0532 -0.0121 0.3500 -0.0165 1.1419 -0.0538 -0.0124 0.3750 -0.0166 1.2235 -0.0541 -0.0127 0.4000 -0.0166 1.3051 -0.0543 -0.0129 0.4250 -0.0166 1.3866 -0.0542 -0.0130 0.4500 -0.0165 1.4682 -0.0539 -0.0131 0.4750 -0.0164 1.5498 -0.0534 -0.0131 0.5000 -0.0162 1.6313 -0.0527 -0.0130 0.5250 -0.0159 1.7129 -0.0518 -0.0129 0.5500 -0.0155 1.7945 -0.0507 -0.0127 0.5750 -0.0151 1.8760 -0.0493 -0.0124 0.6000 -0.0146 1.9576 -0.0475 -0.0120 0.6250 -0.0139 2.0392 -0.0454 -0.0115 0.6500 -0.0132 2.1207 -0.0430 -0.0110 0.6750 -0.0124 2.2023 -0.0403 -0.0103 0.7000 -0.0115 2.2839 -0.0375 -0.0096 0.7250 -0.0106 2.3654 -0.0346 -0.0089 0.7500 -0.0097 2.4470 -0.0315 -0.0081 0.7750 -0.0087 2.5286 -0.0284 -0.0073 0.8000 -0.0077 2.6101 -0.0252 -0.0065 0.8250 -0.0067 2.6917 -0.0219 -0.0056 0.8500 -0.0057 2.7733 -0.0187 -0.0048 0.8750 -0.0047 2.8548 -0.0154 -0.0039 0.9000 -0.0037 2.9364 -0.0121 -0.0031 0.9250 -0.0027 3.0180 -0.0089 -0.0023 0.9500 -0.0018 3.0995 -0.0058 -0.0015 0.9750 -0.0009 3.1811 -0.0029 -0.0007 1.0000 0.0000 3.2627 0.0000 0.0000 1 y= -4.3967 y/(b/2) = -0.4397 chord= 3.9918 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.0477 0.1094 0.0311 0.1719 0.0205 0.2344 0.0123 0.2969 0.0054 0.3594 -0.0009 0.4219 -0.0069 0.4844 -0.0130 0.5469 -0.0197 0.6094 -0.0293 0.6719 -0.0365 0.7344 -0.0403 0.7969 -0.0421 0.8594 -0.0424 0.9219 -0.0410 0.9844 -0.0371 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0107 0.0000 -0.0427 0.0000 0.0250 -0.0119 0.0998 -0.0475 -0.0015 0.0500 -0.0131 0.1996 -0.0523 -0.0029 0.0750 -0.0142 0.2994 -0.0568 -0.0043 0.1000 -0.0152 0.3992 -0.0605 -0.0055 0.1250 -0.0159 0.4990 -0.0636 -0.0066 0.1500 -0.0166 0.5988 -0.0661 -0.0075 0.1750 -0.0171 0.6986 -0.0683 -0.0083 0.2000 -0.0176 0.7984 -0.0701 -0.0090 0.2250 -0.0179 0.8981 -0.0716 -0.0097 0.2500 -0.0182 0.9979 -0.0728 -0.0102 0.2750 -0.0185 1.0977 -0.0737 -0.0107 0.3000 -0.0186 1.1975 -0.0743 -0.0111 0.3250 -0.0187 1.2973 -0.0747 -0.0115 0.3500 -0.0187 1.3971 -0.0748 -0.0118 0.3750 -0.0187 1.4969 -0.0747 -0.0120 0.4000 -0.0186 1.5967 -0.0744 -0.0122 0.4250 -0.0185 1.6965 -0.0738 -0.0123 0.4500 -0.0183 1.7963 -0.0729 -0.0124 0.4750 -0.0180 1.8961 -0.0718 -0.0124 0.5000 -0.0177 1.9959 -0.0705 -0.0123 0.5250 -0.0173 2.0957 -0.0690 -0.0122 0.5500 -0.0168 2.1955 -0.0671 -0.0120 0.5750 -0.0163 2.2953 -0.0649 -0.0117 0.6000 -0.0156 2.3951 -0.0623 -0.0113 0.6250 -0.0149 2.4949 -0.0594 -0.0109 0.6500 -0.0140 2.5946 -0.0561 -0.0103 0.6750 -0.0132 2.6944 -0.0525 -0.0097 0.7000 -0.0122 2.7942 -0.0488 -0.0090 0.7250 -0.0112 2.8940 -0.0448 -0.0083 0.7500 -0.0102 2.9938 -0.0408 -0.0076 0.7750 -0.0092 3.0936 -0.0367 -0.0068 0.8000 -0.0081 3.1934 -0.0325 -0.0060 0.8250 -0.0071 3.2932 -0.0283 -0.0052 0.8500 -0.0060 3.3930 -0.0241 -0.0044 0.8750 -0.0050 3.4928 -0.0198 -0.0036 0.9000 -0.0039 3.5926 -0.0156 -0.0028 0.9250 -0.0029 3.6924 -0.0115 -0.0021 0.9500 -0.0019 3.7922 -0.0075 -0.0013 0.9750 -0.0009 3.8920 -0.0037 -0.0007 1.0000 0.0000 3.9918 0.0000 0.0000 1 y= -3.7300 y/(b/2) = -0.3730 chord= 4.7208 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.0412 0.1094 0.0253 0.1719 0.0151 0.2344 0.0073 0.2969 0.0006 0.3594 -0.0053 0.4219 -0.0109 0.4844 -0.0166 0.5469 -0.0228 0.6094 -0.0318 0.6719 -0.0385 0.7344 -0.0419 0.7969 -0.0434 0.8594 -0.0434 0.9219 -0.0419 0.9844 -0.0379 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0141 0.0000 -0.0665 0.0000 0.0250 -0.0151 0.1180 -0.0714 -0.0014 0.0500 -0.0162 0.2360 -0.0763 -0.0028 0.0750 -0.0171 0.3541 -0.0809 -0.0041 0.1000 -0.0179 0.4721 -0.0846 -0.0052 0.1250 -0.0185 0.5901 -0.0875 -0.0062 0.1500 -0.0190 0.7081 -0.0898 -0.0071 0.1750 -0.0194 0.8261 -0.0917 -0.0078 0.2000 -0.0198 0.9442 -0.0933 -0.0085 0.2250 -0.0200 1.0622 -0.0945 -0.0091 0.2500 -0.0202 1.1802 -0.0953 -0.0096 0.2750 -0.0203 1.2982 -0.0958 -0.0101 0.3000 -0.0203 1.4162 -0.0960 -0.0105 0.3250 -0.0203 1.5343 -0.0959 -0.0108 0.3500 -0.0202 1.6523 -0.0955 -0.0111 0.3750 -0.0201 1.7703 -0.0948 -0.0113 0.4000 -0.0199 1.8883 -0.0939 -0.0114 0.4250 -0.0196 2.0064 -0.0927 -0.0115 0.4500 -0.0193 2.1244 -0.0912 -0.0116 0.4750 -0.0190 2.2424 -0.0895 -0.0116 0.5000 -0.0185 2.3604 -0.0875 -0.0115 0.5250 -0.0181 2.4784 -0.0853 -0.0114 0.5500 -0.0175 2.5965 -0.0827 -0.0112 0.5750 -0.0169 2.7145 -0.0798 -0.0109 0.6000 -0.0162 2.8325 -0.0764 -0.0105 0.6250 -0.0154 2.9505 -0.0726 -0.0101 0.6500 -0.0145 3.0685 -0.0684 -0.0096 0.6750 -0.0135 3.1866 -0.0639 -0.0090 0.7000 -0.0126 3.3046 -0.0593 -0.0083 0.7250 -0.0115 3.4226 -0.0544 -0.0077 0.7500 -0.0105 3.5406 -0.0495 -0.0070 0.7750 -0.0094 3.6586 -0.0444 -0.0062 0.8000 -0.0083 3.7767 -0.0393 -0.0055 0.8250 -0.0072 3.8947 -0.0342 -0.0048 0.8500 -0.0062 4.0127 -0.0291 -0.0040 0.8750 -0.0051 4.1307 -0.0240 -0.0033 0.9000 -0.0040 4.2487 -0.0189 -0.0026 0.9250 -0.0029 4.3668 -0.0139 -0.0019 0.9500 -0.0019 4.4848 -0.0091 -0.0012 0.9750 -0.0009 4.6028 -0.0045 -0.0006 1.0000 0.0000 4.7208 0.0000 0.0000 1 y= -3.0633 y/(b/2) = -0.3063 chord= 5.4499 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.0350 0.1094 0.0199 0.1719 0.0102 0.2344 0.0027 0.2969 -0.0035 0.3594 -0.0090 0.4219 -0.0143 0.4844 -0.0195 0.5469 -0.0253 0.6094 -0.0336 0.6719 -0.0397 0.7344 -0.0427 0.7969 -0.0439 0.8594 -0.0437 0.9219 -0.0420 0.9844 -0.0379 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c -0.0000 -0.0168 -0.0000 -0.0918 0.0000 0.0250 -0.0177 0.1362 -0.0966 -0.0013 0.0500 -0.0186 0.2725 -0.1014 -0.0026 0.0750 -0.0194 0.4087 -0.1058 -0.0038 0.1000 -0.0201 0.5450 -0.1093 -0.0049 0.1250 -0.0205 0.6812 -0.1120 -0.0058 0.1500 -0.0209 0.8175 -0.1139 -0.0066 0.1750 -0.0212 0.9537 -0.1155 -0.0073 0.2000 -0.0214 1.0900 -0.1166 -0.0079 0.2250 -0.0215 1.2262 -0.1173 -0.0085 0.2500 -0.0216 1.3625 -0.1177 -0.0090 0.2750 -0.0216 1.4987 -0.1176 -0.0094 0.3000 -0.0215 1.6350 -0.1173 -0.0097 0.3250 -0.0214 1.7712 -0.1166 -0.0100 0.3500 -0.0212 1.9075 -0.1156 -0.0103 0.3750 -0.0210 2.0437 -0.1144 -0.0105 0.4000 -0.0207 2.1800 -0.1128 -0.0106 0.4250 -0.0204 2.3162 -0.1110 -0.0107 0.4500 -0.0200 2.4525 -0.1089 -0.0107 0.4750 -0.0195 2.5887 -0.1064 -0.0107 0.5000 -0.0190 2.7250 -0.1037 -0.0106 0.5250 -0.0185 2.8612 -0.1008 -0.0105 0.5500 -0.0179 2.9975 -0.0974 -0.0103 0.5750 -0.0172 3.1337 -0.0937 -0.0100 0.6000 -0.0164 3.2699 -0.0895 -0.0097 0.6250 -0.0156 3.4062 -0.0849 -0.0093 0.6500 -0.0147 3.5424 -0.0799 -0.0088 0.6750 -0.0137 3.6787 -0.0746 -0.0082 0.7000 -0.0127 3.8149 -0.0690 -0.0076 0.7250 -0.0116 3.9512 -0.0633 -0.0070 0.7500 -0.0106 4.0874 -0.0575 -0.0063 0.7750 -0.0095 4.2237 -0.0516 -0.0057 0.8000 -0.0084 4.3599 -0.0456 -0.0050 0.8250 -0.0073 4.4962 -0.0396 -0.0043 0.8500 -0.0062 4.6324 -0.0337 -0.0036 0.8750 -0.0051 4.7687 -0.0277 -0.0030 0.9000 -0.0040 4.9049 -0.0218 -0.0023 0.9250 -0.0029 5.0412 -0.0160 -0.0017 0.9500 -0.0019 5.1774 -0.0105 -0.0011 0.9750 -0.0009 5.3137 -0.0052 -0.0005 1.0000 0.0000 5.4499 0.0000 0.0000 1 y= -2.3967 y/(b/2) = -0.2397 chord= 6.1790 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.0287 0.1094 0.0145 0.1719 0.0054 0.2344 -0.0016 0.2969 -0.0075 0.3594 -0.0126 0.4219 -0.0175 0.4844 -0.0223 0.5469 -0.0275 0.6094 -0.0351 0.6719 -0.0407 0.7344 -0.0432 0.7969 -0.0441 0.8594 -0.0436 0.9219 -0.0417 0.9844 -0.0377 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0194 0.0000 -0.1198 0.0000 0.0250 -0.0201 0.1545 -0.1243 -0.0012 0.0500 -0.0208 0.3089 -0.1288 -0.0024 0.0750 -0.0215 0.4634 -0.1328 -0.0036 0.1000 -0.0220 0.6179 -0.1359 -0.0046 0.1250 -0.0223 0.7724 -0.1381 -0.0054 0.1500 -0.0226 0.9268 -0.1395 -0.0061 0.1750 -0.0227 1.0813 -0.1405 -0.0068 0.2000 -0.0228 1.2358 -0.1411 -0.0073 0.2250 -0.0229 1.3903 -0.1412 -0.0078 0.2500 -0.0228 1.5447 -0.1409 -0.0083 0.2750 -0.0227 1.6992 -0.1402 -0.0086 0.3000 -0.0225 1.8537 -0.1392 -0.0090 0.3250 -0.0223 2.0082 -0.1378 -0.0092 0.3500 -0.0220 2.1626 -0.1362 -0.0094 0.3750 -0.0217 2.3171 -0.1342 -0.0096 0.4000 -0.0213 2.4716 -0.1319 -0.0097 0.4250 -0.0209 2.6261 -0.1293 -0.0098 0.4500 -0.0205 2.7805 -0.1264 -0.0098 0.4750 -0.0199 2.9350 -0.1232 -0.0098 0.5000 -0.0194 3.0895 -0.1198 -0.0097 0.5250 -0.0188 3.2440 -0.1160 -0.0096 0.5500 -0.0181 3.3984 -0.1119 -0.0094 0.5750 -0.0174 3.5529 -0.1074 -0.0091 0.6000 -0.0166 3.7074 -0.1023 -0.0088 0.6250 -0.0157 3.8619 -0.0969 -0.0084 0.6500 -0.0147 4.0163 -0.0910 -0.0079 0.6750 -0.0137 4.1708 -0.0848 -0.0074 0.7000 -0.0127 4.3253 -0.0784 -0.0069 0.7250 -0.0116 4.4798 -0.0718 -0.0063 0.7500 -0.0105 4.6342 -0.0651 -0.0057 0.7750 -0.0094 4.7887 -0.0584 -0.0051 0.8000 -0.0083 4.9432 -0.0516 -0.0045 0.8250 -0.0072 5.0977 -0.0448 -0.0039 0.8500 -0.0061 5.2521 -0.0380 -0.0032 0.8750 -0.0051 5.4066 -0.0312 -0.0026 0.9000 -0.0040 5.5611 -0.0246 -0.0020 0.9250 -0.0029 5.7156 -0.0181 -0.0015 0.9500 -0.0019 5.8700 -0.0118 -0.0009 0.9750 -0.0009 6.0245 -0.0058 -0.0005 1.0000 0.0000 6.1790 0.0000 0.0000 1 y= -1.7300 y/(b/2) = -0.1730 chord= 6.9080 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.0222 0.1094 0.0087 0.1719 0.0001 0.2344 -0.0065 0.2969 -0.0119 0.3594 -0.0166 0.4219 -0.0210 0.4844 -0.0254 0.5469 -0.0301 0.6094 -0.0369 0.6719 -0.0418 0.7344 -0.0439 0.7969 -0.0444 0.8594 -0.0437 0.9219 -0.0416 0.9844 -0.0374 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0222 0.0000 -0.1534 0.0000 0.0250 -0.0228 0.1727 -0.1573 -0.0011 0.0500 -0.0233 0.3454 -0.1612 -0.0022 0.0750 -0.0238 0.5181 -0.1646 -0.0033 0.1000 -0.0242 0.6908 -0.1671 -0.0042 0.1250 -0.0244 0.8635 -0.1685 -0.0050 0.1500 -0.0245 1.0362 -0.1692 -0.0056 0.1750 -0.0245 1.2089 -0.1694 -0.0062 0.2000 -0.0245 1.3816 -0.1691 -0.0067 0.2250 -0.0244 1.5543 -0.1684 -0.0072 0.2500 -0.0242 1.7270 -0.1672 -0.0075 0.2750 -0.0240 1.8997 -0.1656 -0.0079 0.3000 -0.0237 2.0724 -0.1637 -0.0082 0.3250 -0.0234 2.2451 -0.1615 -0.0084 0.3500 -0.0230 2.4178 -0.1589 -0.0086 0.3750 -0.0226 2.5905 -0.1560 -0.0087 0.4000 -0.0221 2.7632 -0.1527 -0.0088 0.4250 -0.0216 2.9359 -0.1492 -0.0088 0.4500 -0.0210 3.1086 -0.1454 -0.0088 0.4750 -0.0205 3.2813 -0.1413 -0.0088 0.5000 -0.0198 3.4540 -0.1369 -0.0087 0.5250 -0.0191 3.6267 -0.1322 -0.0086 0.5500 -0.0184 3.7994 -0.1271 -0.0084 0.5750 -0.0176 3.9721 -0.1216 -0.0082 0.6000 -0.0167 4.1448 -0.1157 -0.0079 0.6250 -0.0158 4.3175 -0.1093 -0.0075 0.6500 -0.0148 4.4902 -0.1024 -0.0071 0.6750 -0.0138 4.6629 -0.0953 -0.0066 0.7000 -0.0127 4.8356 -0.0880 -0.0061 0.7250 -0.0116 5.0083 -0.0805 -0.0055 0.7500 -0.0106 5.1810 -0.0729 -0.0050 0.7750 -0.0094 5.3537 -0.0652 -0.0044 0.8000 -0.0083 5.5264 -0.0576 -0.0039 0.8250 -0.0072 5.6991 -0.0499 -0.0033 0.8500 -0.0061 5.8718 -0.0423 -0.0028 0.8750 -0.0050 6.0445 -0.0348 -0.0023 0.9000 -0.0040 6.2172 -0.0273 -0.0017 0.9250 -0.0029 6.3899 -0.0201 -0.0012 0.9500 -0.0019 6.5626 -0.0131 -0.0008 0.9750 -0.0009 6.7353 -0.0065 -0.0004 1.0000 0.0000 6.9080 0.0000 0.0000 1 y= -1.0633 y/(b/2) = -0.1063 chord= 7.6371 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.0143 0.1094 0.0014 0.1719 -0.0068 0.2344 -0.0129 0.2969 -0.0179 0.3594 -0.0222 0.4219 -0.0261 0.4844 -0.0298 0.5469 -0.0338 0.6094 -0.0398 0.6719 -0.0438 0.7344 -0.0452 0.7969 -0.0452 0.8594 -0.0440 0.9219 -0.0416 0.9844 -0.0374 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0261 0.0000 -0.1996 -0.0000 0.0250 -0.0265 0.1909 -0.2024 -0.0010 0.0500 -0.0269 0.3819 -0.2052 -0.0020 0.0750 -0.0272 0.5728 -0.2075 -0.0030 0.1000 -0.0273 0.7637 -0.2087 -0.0038 0.1250 -0.0274 0.9546 -0.2089 -0.0045 0.1500 -0.0273 1.1456 -0.2083 -0.0051 0.1750 -0.0271 1.3365 -0.2072 -0.0056 0.2000 -0.0269 1.5274 -0.2056 -0.0060 0.2250 -0.0267 1.7184 -0.2036 -0.0064 0.2500 -0.0263 1.9093 -0.2010 -0.0067 0.2750 -0.0259 2.1002 -0.1981 -0.0070 0.3000 -0.0255 2.2911 -0.1948 -0.0072 0.3250 -0.0250 2.4821 -0.1912 -0.0074 0.3500 -0.0245 2.6730 -0.1872 -0.0075 0.3750 -0.0240 2.8639 -0.1829 -0.0076 0.4000 -0.0234 3.0548 -0.1784 -0.0077 0.4250 -0.0227 3.2458 -0.1735 -0.0077 0.4500 -0.0220 3.4367 -0.1683 -0.0077 0.4750 -0.0213 3.6276 -0.1629 -0.0076 0.5000 -0.0206 3.8186 -0.1571 -0.0075 0.5250 -0.0198 4.0095 -0.1511 -0.0074 0.5500 -0.0190 4.2004 -0.1448 -0.0072 0.5750 -0.0181 4.3913 -0.1381 -0.0070 0.6000 -0.0171 4.5823 -0.1309 -0.0067 0.6250 -0.0161 4.7732 -0.1232 -0.0063 0.6500 -0.0151 4.9641 -0.1152 -0.0059 0.6750 -0.0140 5.1551 -0.1070 -0.0055 0.7000 -0.0129 5.3460 -0.0985 -0.0051 0.7250 -0.0118 5.5369 -0.0899 -0.0046 0.7500 -0.0106 5.7278 -0.0813 -0.0041 0.7750 -0.0095 5.9188 -0.0726 -0.0036 0.8000 -0.0084 6.1097 -0.0640 -0.0031 0.8250 -0.0072 6.3006 -0.0554 -0.0027 0.8500 -0.0061 6.4915 -0.0469 -0.0022 0.8750 -0.0050 6.6825 -0.0385 -0.0018 0.9000 -0.0040 6.8734 -0.0302 -0.0013 0.9250 -0.0029 7.0643 -0.0222 -0.0009 0.9500 -0.0019 7.2553 -0.0145 -0.0006 0.9750 -0.0009 7.4462 -0.0071 -0.0003 1.0000 0.0000 7.6371 0.0000 0.0000 1 y= -0.3650 y/(b/2) = -0.0365 chord= 8.4008 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 -0.0012 0.1094 -0.0141 0.1719 -0.0222 0.2344 -0.0279 0.2969 -0.0323 0.3594 -0.0359 0.4219 -0.0388 0.4844 -0.0414 0.5469 -0.0440 0.6094 -0.0481 0.6719 -0.0503 0.7344 -0.0500 0.7969 -0.0484 0.8594 -0.0459 0.9219 -0.0426 0.9844 -0.0378 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0357 0.0000 -0.3003 0.0000 0.0250 -0.0357 0.2100 -0.3001 -0.0009 0.0500 -0.0357 0.4200 -0.3000 -0.0017 0.0750 -0.0356 0.6301 -0.2992 -0.0026 0.1000 -0.0354 0.8401 -0.2973 -0.0032 0.1250 -0.0350 1.0501 -0.2943 -0.0037 0.1500 -0.0346 1.2601 -0.2904 -0.0042 0.1750 -0.0340 1.4701 -0.2859 -0.0045 0.2000 -0.0334 1.6802 -0.2809 -0.0048 0.2250 -0.0328 1.8902 -0.2755 -0.0051 0.2500 -0.0321 2.1002 -0.2696 -0.0053 0.2750 -0.0313 2.3102 -0.2632 -0.0054 0.3000 -0.0305 2.5203 -0.2566 -0.0055 0.3250 -0.0297 2.7303 -0.2496 -0.0056 0.3500 -0.0288 2.9403 -0.2423 -0.0056 0.3750 -0.0279 3.1503 -0.2347 -0.0056 0.4000 -0.0270 3.3603 -0.2269 -0.0056 0.4250 -0.0261 3.5704 -0.2189 -0.0055 0.4500 -0.0251 3.7804 -0.2106 -0.0054 0.4750 -0.0241 3.9904 -0.2021 -0.0053 0.5000 -0.0230 4.2004 -0.1933 -0.0051 0.5250 -0.0220 4.4104 -0.1844 -0.0050 0.5500 -0.0209 4.6205 -0.1753 -0.0048 0.5750 -0.0197 4.8305 -0.1658 -0.0045 0.6000 -0.0186 5.0405 -0.1560 -0.0043 0.6250 -0.0174 5.2505 -0.1458 -0.0040 0.6500 -0.0161 5.4605 -0.1355 -0.0036 0.6750 -0.0149 5.6706 -0.1249 -0.0033 0.7000 -0.0136 5.8806 -0.1144 -0.0029 0.7250 -0.0124 6.0906 -0.1038 -0.0025 0.7500 -0.0111 6.3006 -0.0933 -0.0022 0.7750 -0.0099 6.5107 -0.0830 -0.0018 0.8000 -0.0087 6.7207 -0.0727 -0.0015 0.8250 -0.0075 6.9307 -0.0627 -0.0012 0.8500 -0.0063 7.1407 -0.0529 -0.0009 0.8750 -0.0051 7.3507 -0.0432 -0.0007 0.9000 -0.0040 7.5608 -0.0338 -0.0005 0.9250 -0.0029 7.7708 -0.0248 -0.0003 0.9500 -0.0019 7.9808 -0.0161 -0.0001 0.9750 -0.0009 8.1908 -0.0079 -0.0001 1.0000 0.0000 8.4008 0.0000 0.0000 1 y= -9.6667 y/(b/2) = -0.9667 chord= 2.5350 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.0824 0.1094 0.0658 0.1719 0.0550 0.2344 0.0461 0.2969 0.0379 0.3594 0.0300 0.4219 0.0221 0.4844 0.0143 0.5469 0.0062 0.6094 -0.0022 0.6719 -0.0112 0.7344 -0.0217 0.7969 -0.0369 0.8594 -0.0510 0.9219 -0.0552 0.9844 -0.0511 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 0.0102 0.0000 0.0259 0.0000 0.0250 0.0081 0.0634 0.0206 -0.0018 0.0500 0.0061 0.1268 0.0154 -0.0036 0.0750 0.0041 0.1901 0.0104 -0.0054 0.1000 0.0023 0.2535 0.0058 -0.0069 0.1250 0.0006 0.3169 0.0016 -0.0083 0.1500 -0.0009 0.3802 -0.0022 -0.0095 0.1750 -0.0023 0.4436 -0.0057 -0.0107 0.2000 -0.0036 0.5070 -0.0091 -0.0118 0.2250 -0.0048 0.5704 -0.0122 -0.0127 0.2500 -0.0059 0.6337 -0.0151 -0.0136 0.2750 -0.0070 0.6971 -0.0178 -0.0144 0.3000 -0.0080 0.7605 -0.0202 -0.0151 0.3250 -0.0089 0.8239 -0.0225 -0.0158 0.3500 -0.0097 0.8873 -0.0246 -0.0163 0.3750 -0.0104 0.9506 -0.0265 -0.0168 0.4000 -0.0111 1.0140 -0.0281 -0.0172 0.4250 -0.0117 1.0774 -0.0296 -0.0176 0.4500 -0.0122 1.1407 -0.0309 -0.0178 0.4750 -0.0126 1.2041 -0.0320 -0.0180 0.5000 -0.0130 1.2675 -0.0328 -0.0181 0.5250 -0.0132 1.3309 -0.0335 -0.0181 0.5500 -0.0134 1.3942 -0.0340 -0.0180 0.5750 -0.0135 1.4576 -0.0343 -0.0179 0.6000 -0.0135 1.5210 -0.0343 -0.0176 0.6250 -0.0135 1.5844 -0.0341 -0.0173 0.6500 -0.0133 1.6477 -0.0338 -0.0169 0.6750 -0.0131 1.7111 -0.0331 -0.0164 0.7000 -0.0127 1.7745 -0.0323 -0.0158 0.7250 -0.0123 1.8379 -0.0312 -0.0151 0.7500 -0.0117 1.9012 -0.0297 -0.0143 0.7750 -0.0110 1.9646 -0.0280 -0.0133 0.8000 -0.0102 2.0280 -0.0258 -0.0122 0.8250 -0.0091 2.0914 -0.0232 -0.0109 0.8500 -0.0080 2.1547 -0.0202 -0.0095 0.8750 -0.0067 2.2181 -0.0170 -0.0080 0.9000 -0.0053 2.2815 -0.0135 -0.0063 0.9250 -0.0039 2.3449 -0.0100 -0.0047 0.9500 -0.0026 2.4082 -0.0066 -0.0031 0.9750 -0.0013 2.4716 -0.0032 -0.0015 1.0000 0.0000 2.5350 0.0000 0.0000 1 y= -9.0000 y/(b/2) = -0.9000 chord= 3.2850 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.0793 0.1094 0.0574 0.1719 0.0429 0.2344 0.0312 0.2969 0.0210 0.3594 0.0114 0.4219 0.0023 0.4844 -0.0068 0.5469 -0.0160 0.6094 -0.0256 0.6719 -0.0360 0.7344 -0.0482 0.7969 -0.0665 0.8594 -0.0836 0.9219 -0.0885 0.9844 -0.0831 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0105 0.0000 -0.0346 0.0000 0.0250 -0.0125 0.0821 -0.0412 -0.0023 0.0500 -0.0145 0.1643 -0.0477 -0.0045 0.0750 -0.0164 0.2464 -0.0539 -0.0067 0.1000 -0.0181 0.3285 -0.0594 -0.0086 0.1250 -0.0195 0.4106 -0.0640 -0.0103 0.1500 -0.0207 0.4928 -0.0681 -0.0118 0.1750 -0.0218 0.5749 -0.0717 -0.0131 0.2000 -0.0228 0.6570 -0.0750 -0.0144 0.2250 -0.0237 0.7391 -0.0779 -0.0155 0.2500 -0.0245 0.8213 -0.0804 -0.0166 0.2750 -0.0251 0.9034 -0.0826 -0.0175 0.3000 -0.0257 0.9855 -0.0844 -0.0183 0.3250 -0.0262 1.0676 -0.0860 -0.0191 0.3500 -0.0265 1.1498 -0.0872 -0.0197 0.3750 -0.0268 1.2319 -0.0881 -0.0202 0.4000 -0.0270 1.3140 -0.0887 -0.0207 0.4250 -0.0271 1.3961 -0.0890 -0.0210 0.4500 -0.0271 1.4783 -0.0890 -0.0213 0.4750 -0.0270 1.5604 -0.0887 -0.0215 0.5000 -0.0268 1.6425 -0.0881 -0.0215 0.5250 -0.0265 1.7246 -0.0872 -0.0215 0.5500 -0.0262 1.8068 -0.0860 -0.0214 0.5750 -0.0257 1.8889 -0.0845 -0.0212 0.6000 -0.0252 1.9710 -0.0827 -0.0209 0.6250 -0.0245 2.0531 -0.0805 -0.0206 0.6500 -0.0238 2.1353 -0.0780 -0.0201 0.6750 -0.0229 2.2174 -0.0752 -0.0195 0.7000 -0.0219 2.2995 -0.0720 -0.0188 0.7250 -0.0208 2.3816 -0.0684 -0.0179 0.7500 -0.0196 2.4638 -0.0644 -0.0170 0.7750 -0.0182 2.5459 -0.0598 -0.0158 0.8000 -0.0166 2.6280 -0.0546 -0.0145 0.8250 -0.0148 2.7101 -0.0488 -0.0130 0.8500 -0.0129 2.7923 -0.0423 -0.0113 0.8750 -0.0108 2.8744 -0.0354 -0.0095 0.9000 -0.0086 2.9565 -0.0282 -0.0075 0.9250 -0.0064 3.0386 -0.0209 -0.0056 0.9500 -0.0042 3.1208 -0.0138 -0.0037 0.9750 -0.0021 3.2029 -0.0068 -0.0018 1.0000 0.0000 3.2850 0.0000 0.0000 1 y= -8.3333 y/(b/2) = -0.8333 chord= 4.0350 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.0747 0.1094 0.0520 0.1719 0.0370 0.2344 0.0253 0.2969 0.0151 0.3594 0.0059 0.4219 -0.0029 0.4844 -0.0115 0.5469 -0.0201 0.6094 -0.0292 0.6719 -0.0390 0.7344 -0.0506 0.7969 -0.0686 0.8594 -0.0854 0.9219 -0.0900 0.9844 -0.0843 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0145 0.0000 -0.0586 0.0000 0.0250 -0.0164 0.1009 -0.0662 -0.0022 0.0500 -0.0183 0.2018 -0.0738 -0.0045 0.0750 -0.0200 0.3026 -0.0809 -0.0066 0.1000 -0.0216 0.4035 -0.0870 -0.0085 0.1250 -0.0228 0.5044 -0.0922 -0.0101 0.1500 -0.0239 0.6053 -0.0966 -0.0116 0.1750 -0.0249 0.7061 -0.1005 -0.0129 0.2000 -0.0258 0.8070 -0.1040 -0.0142 0.2250 -0.0265 0.9079 -0.1069 -0.0152 0.2500 -0.0271 1.0088 -0.1094 -0.0162 0.2750 -0.0276 1.1096 -0.1115 -0.0171 0.3000 -0.0280 1.2105 -0.1132 -0.0179 0.3250 -0.0284 1.3114 -0.1144 -0.0186 0.3500 -0.0286 1.4123 -0.1154 -0.0192 0.3750 -0.0287 1.5131 -0.1159 -0.0197 0.4000 -0.0288 1.6140 -0.1161 -0.0201 0.4250 -0.0287 1.7149 -0.1159 -0.0204 0.4500 -0.0286 1.8158 -0.1154 -0.0206 0.4750 -0.0284 1.9166 -0.1146 -0.0208 0.5000 -0.0281 2.0175 -0.1134 -0.0208 0.5250 -0.0277 2.1184 -0.1118 -0.0208 0.5500 -0.0272 2.2193 -0.1099 -0.0207 0.5750 -0.0267 2.3201 -0.1077 -0.0205 0.6000 -0.0260 2.4210 -0.1051 -0.0202 0.6250 -0.0253 2.5219 -0.1021 -0.0199 0.6500 -0.0245 2.6228 -0.0987 -0.0194 0.6750 -0.0235 2.7236 -0.0949 -0.0188 0.7000 -0.0225 2.8245 -0.0907 -0.0181 0.7250 -0.0213 2.9254 -0.0861 -0.0173 0.7500 -0.0200 3.0263 -0.0809 -0.0164 0.7750 -0.0186 3.1271 -0.0750 -0.0153 0.8000 -0.0169 3.2280 -0.0684 -0.0140 0.8250 -0.0151 3.3289 -0.0610 -0.0126 0.8500 -0.0131 3.4298 -0.0529 -0.0109 0.8750 -0.0110 3.5306 -0.0442 -0.0091 0.9000 -0.0087 3.6315 -0.0352 -0.0073 0.9250 -0.0065 3.7324 -0.0261 -0.0054 0.9500 -0.0043 3.8333 -0.0172 -0.0035 0.9750 -0.0021 3.9341 -0.0085 -0.0017 1.0000 0.0000 4.0350 0.0000 0.0000 1 y= -7.6667 y/(b/2) = -0.7667 chord= 4.7850 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.0697 0.1094 0.0473 0.1719 0.0327 0.2344 0.0212 0.2969 0.0113 0.3594 0.0024 0.4219 -0.0059 0.4844 -0.0141 0.5469 -0.0222 0.6094 -0.0307 0.6719 -0.0400 0.7344 -0.0510 0.7969 -0.0681 0.8594 -0.0841 0.9219 -0.0884 0.9844 -0.0828 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0166 0.0000 -0.0792 0.0000 0.0250 -0.0183 0.1196 -0.0876 -0.0022 0.0500 -0.0201 0.2392 -0.0960 -0.0043 0.0750 -0.0217 0.3589 -0.1039 -0.0064 0.1000 -0.0231 0.4785 -0.1106 -0.0082 0.1250 -0.0243 0.5981 -0.1161 -0.0098 0.1500 -0.0253 0.7177 -0.1209 -0.0112 0.1750 -0.0261 0.8374 -0.1250 -0.0125 0.2000 -0.0269 0.9570 -0.1285 -0.0136 0.2250 -0.0275 1.0766 -0.1315 -0.0147 0.2500 -0.0280 1.1963 -0.1340 -0.0156 0.2750 -0.0284 1.3159 -0.1360 -0.0164 0.3000 -0.0287 1.4355 -0.1375 -0.0171 0.3250 -0.0290 1.5551 -0.1386 -0.0178 0.3500 -0.0291 1.6748 -0.1393 -0.0183 0.3750 -0.0292 1.7944 -0.1395 -0.0188 0.4000 -0.0291 1.9140 -0.1393 -0.0192 0.4250 -0.0290 2.0336 -0.1388 -0.0195 0.4500 -0.0288 2.1532 -0.1378 -0.0197 0.4750 -0.0285 2.2729 -0.1365 -0.0198 0.5000 -0.0282 2.3925 -0.1347 -0.0199 0.5250 -0.0277 2.5121 -0.1326 -0.0199 0.5500 -0.0272 2.6317 -0.1301 -0.0197 0.5750 -0.0266 2.7514 -0.1272 -0.0195 0.6000 -0.0259 2.8710 -0.1239 -0.0193 0.6250 -0.0251 2.9906 -0.1202 -0.0189 0.6500 -0.0242 3.1102 -0.1160 -0.0184 0.6750 -0.0233 3.2299 -0.1114 -0.0179 0.7000 -0.0222 3.3495 -0.1063 -0.0173 0.7250 -0.0211 3.4691 -0.1008 -0.0165 0.7500 -0.0198 3.5888 -0.0946 -0.0156 0.7750 -0.0183 3.7084 -0.0876 -0.0146 0.8000 -0.0167 3.8280 -0.0798 -0.0134 0.8250 -0.0149 3.9476 -0.0711 -0.0120 0.8500 -0.0129 4.0673 -0.0616 -0.0104 0.8750 -0.0108 4.1869 -0.0515 -0.0087 0.9000 -0.0086 4.3065 -0.0410 -0.0069 0.9250 -0.0064 4.4261 -0.0304 -0.0051 0.9500 -0.0042 4.5458 -0.0200 -0.0034 0.9750 -0.0021 4.6654 -0.0099 -0.0017 1.0000 0.0000 4.7850 0.0000 0.0000 1 y= -7.0317 y/(b/2) = -0.7032 chord= 5.4994 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.0616 0.1094 0.0403 0.1719 0.0263 0.2344 0.0154 0.2969 0.0061 0.3594 -0.0022 0.4219 -0.0100 0.4844 -0.0176 0.5469 -0.0251 0.6094 -0.0330 0.6719 -0.0415 0.7344 -0.0517 0.7969 -0.0677 0.8594 -0.0826 0.9219 -0.0865 0.9844 -0.0812 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0196 0.0000 -0.1080 0.0000 0.0250 -0.0212 0.1375 -0.1166 -0.0020 0.0500 -0.0228 0.2750 -0.1251 -0.0041 0.0750 -0.0242 0.4125 -0.1331 -0.0060 0.1000 -0.0254 0.5499 -0.1398 -0.0077 0.1250 -0.0264 0.6874 -0.1452 -0.0092 0.1500 -0.0272 0.8249 -0.1497 -0.0105 0.1750 -0.0279 0.9624 -0.1535 -0.0117 0.2000 -0.0285 1.0999 -0.1568 -0.0128 0.2250 -0.0290 1.2374 -0.1594 -0.0138 0.2500 -0.0294 1.3748 -0.1614 -0.0146 0.2750 -0.0296 1.5123 -0.1630 -0.0154 0.3000 -0.0298 1.6498 -0.1640 -0.0161 0.3250 -0.0299 1.7873 -0.1645 -0.0167 0.3500 -0.0299 1.9248 -0.1646 -0.0172 0.3750 -0.0299 2.0623 -0.1643 -0.0176 0.4000 -0.0297 2.1997 -0.1635 -0.0179 0.4250 -0.0295 2.3372 -0.1622 -0.0182 0.4500 -0.0292 2.4747 -0.1606 -0.0184 0.4750 -0.0288 2.6122 -0.1585 -0.0185 0.5000 -0.0284 2.7497 -0.1561 -0.0186 0.5250 -0.0279 2.8872 -0.1532 -0.0185 0.5500 -0.0273 3.0247 -0.1499 -0.0184 0.5750 -0.0266 3.1621 -0.1462 -0.0182 0.6000 -0.0258 3.2996 -0.1420 -0.0180 0.6250 -0.0250 3.4371 -0.1374 -0.0176 0.6500 -0.0241 3.5746 -0.1324 -0.0172 0.6750 -0.0231 3.7121 -0.1268 -0.0167 0.7000 -0.0220 3.8496 -0.1208 -0.0161 0.7250 -0.0208 3.9870 -0.1143 -0.0154 0.7500 -0.0195 4.1245 -0.1071 -0.0146 0.7750 -0.0180 4.2620 -0.0990 -0.0136 0.8000 -0.0164 4.3995 -0.0901 -0.0125 0.8250 -0.0146 4.5370 -0.0802 -0.0111 0.8500 -0.0126 4.6745 -0.0694 -0.0097 0.8750 -0.0106 4.8119 -0.0580 -0.0081 0.9000 -0.0084 4.9494 -0.0462 -0.0064 0.9250 -0.0062 5.0869 -0.0343 -0.0048 0.9500 -0.0041 5.2244 -0.0225 -0.0031 0.9750 -0.0020 5.3619 -0.0112 -0.0015 1.0000 0.0000 5.4994 0.0000 0.0000 1 y= -6.3967 y/(b/2) = -0.6397 chord= 6.2138 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.0459 0.1094 0.0264 0.1719 0.0137 0.2344 0.0039 0.2969 -0.0043 0.3594 -0.0117 0.4219 -0.0185 0.4844 -0.0250 0.5469 -0.0315 0.6094 -0.0383 0.6719 -0.0457 0.7344 -0.0547 0.7969 -0.0689 0.8594 -0.0823 0.9219 -0.0856 0.9844 -0.0806 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0266 0.0000 -0.1655 0.0000 0.0250 -0.0278 0.1553 -0.1727 -0.0018 0.0500 -0.0289 0.3107 -0.1799 -0.0037 0.0750 -0.0300 0.4660 -0.1865 -0.0054 0.1000 -0.0309 0.6214 -0.1918 -0.0069 0.1250 -0.0315 0.7767 -0.1957 -0.0082 0.1500 -0.0320 0.9321 -0.1987 -0.0094 0.1750 -0.0324 1.0874 -0.2011 -0.0104 0.2000 -0.0326 1.2428 -0.2028 -0.0113 0.2250 -0.0328 1.3981 -0.2040 -0.0122 0.2500 -0.0329 1.5534 -0.2045 -0.0129 0.2750 -0.0329 1.7088 -0.2045 -0.0136 0.3000 -0.0328 1.8641 -0.2040 -0.0142 0.3250 -0.0327 2.0195 -0.2030 -0.0147 0.3500 -0.0324 2.1748 -0.2016 -0.0151 0.3750 -0.0321 2.3302 -0.1997 -0.0155 0.4000 -0.0318 2.4855 -0.1975 -0.0158 0.4250 -0.0313 2.6408 -0.1947 -0.0160 0.4500 -0.0308 2.7962 -0.1916 -0.0162 0.4750 -0.0303 2.9515 -0.1881 -0.0163 0.5000 -0.0296 3.1069 -0.1841 -0.0163 0.5250 -0.0289 3.2622 -0.1798 -0.0163 0.5500 -0.0282 3.4176 -0.1751 -0.0162 0.5750 -0.0273 3.5729 -0.1699 -0.0160 0.6000 -0.0264 3.7283 -0.1643 -0.0158 0.6250 -0.0255 3.8836 -0.1583 -0.0155 0.6500 -0.0244 4.0389 -0.1519 -0.0151 0.6750 -0.0233 4.1943 -0.1449 -0.0147 0.7000 -0.0221 4.3496 -0.1375 -0.0141 0.7250 -0.0209 4.5050 -0.1296 -0.0135 0.7500 -0.0195 4.6603 -0.1210 -0.0128 0.7750 -0.0180 4.8157 -0.1116 -0.0120 0.8000 -0.0163 4.9710 -0.1013 -0.0110 0.8250 -0.0145 5.1263 -0.0900 -0.0098 0.8500 -0.0125 5.2817 -0.0778 -0.0085 0.8750 -0.0105 5.4370 -0.0650 -0.0071 0.9000 -0.0083 5.5924 -0.0517 -0.0057 0.9250 -0.0062 5.7477 -0.0384 -0.0042 0.9500 -0.0041 5.9031 -0.0253 -0.0027 0.9750 -0.0020 6.0584 -0.0125 -0.0014 1.0000 0.0000 6.2138 0.0000 0.0000 1 y= -5.7300 y/(b/2) = -0.5730 chord= 6.9637 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.0290 0.1094 0.0115 0.1719 0.0002 0.2344 -0.0083 0.2969 -0.0154 0.3594 -0.0216 0.4219 -0.0273 0.4844 -0.0328 0.5469 -0.0382 0.6094 -0.0439 0.6719 -0.0501 0.7344 -0.0577 0.7969 -0.0702 0.8594 -0.0820 0.9219 -0.0847 0.9844 -0.0799 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0340 0.0000 -0.2370 0.0000 0.0250 -0.0348 0.1741 -0.2421 -0.0016 0.0500 -0.0355 0.3482 -0.2473 -0.0032 0.0750 -0.0362 0.5223 -0.2518 -0.0047 0.1000 -0.0366 0.6964 -0.2550 -0.0060 0.1250 -0.0369 0.8705 -0.2569 -0.0071 0.1500 -0.0370 1.0446 -0.2578 -0.0081 0.1750 -0.0371 1.2187 -0.2581 -0.0090 0.2000 -0.0370 1.3927 -0.2577 -0.0098 0.2250 -0.0369 1.5668 -0.2568 -0.0105 0.2500 -0.0367 1.7409 -0.2553 -0.0111 0.2750 -0.0364 1.9150 -0.2532 -0.0117 0.3000 -0.0360 2.0891 -0.2507 -0.0122 0.3250 -0.0356 2.2632 -0.2478 -0.0126 0.3500 -0.0351 2.4373 -0.2444 -0.0130 0.3750 -0.0345 2.6114 -0.2406 -0.0133 0.4000 -0.0339 2.7855 -0.2363 -0.0135 0.4250 -0.0333 2.9596 -0.2317 -0.0137 0.4500 -0.0326 3.1337 -0.2267 -0.0138 0.4750 -0.0318 3.3078 -0.2214 -0.0139 0.5000 -0.0310 3.4819 -0.2156 -0.0139 0.5250 -0.0301 3.6560 -0.2095 -0.0139 0.5500 -0.0291 3.8301 -0.2030 -0.0138 0.5750 -0.0282 4.0042 -0.1961 -0.0137 0.6000 -0.0271 4.1783 -0.1888 -0.0135 0.6250 -0.0260 4.3523 -0.1811 -0.0132 0.6500 -0.0248 4.5264 -0.1730 -0.0129 0.6750 -0.0236 4.7005 -0.1644 -0.0125 0.7000 -0.0223 4.8746 -0.1554 -0.0121 0.7250 -0.0210 5.0487 -0.1459 -0.0116 0.7500 -0.0195 5.2228 -0.1357 -0.0110 0.7750 -0.0179 5.3969 -0.1248 -0.0103 0.8000 -0.0162 5.5710 -0.1129 -0.0094 0.8250 -0.0144 5.7451 -0.1001 -0.0084 0.8500 -0.0124 5.9192 -0.0865 -0.0073 0.8750 -0.0104 6.0933 -0.0721 -0.0061 0.9000 -0.0082 6.2674 -0.0574 -0.0048 0.9250 -0.0061 6.4415 -0.0426 -0.0036 0.9500 -0.0040 6.6156 -0.0281 -0.0023 0.9750 -0.0020 6.7897 -0.0139 -0.0011 1.0000 0.0000 6.9637 0.0000 0.0000 1 y= -5.0633 y/(b/2) = -0.5063 chord= 7.7138 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.0167 0.1094 0.0009 0.1719 -0.0092 0.2344 -0.0168 0.2969 -0.0230 0.3594 -0.0284 0.4219 -0.0334 0.4844 -0.0381 0.5469 -0.0427 0.6094 -0.0475 0.6719 -0.0529 0.7344 -0.0596 0.7969 -0.0707 0.8594 -0.0812 0.9219 -0.0835 0.9844 -0.0789 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0391 0.0000 -0.3012 0.0000 0.0250 -0.0395 0.1928 -0.3045 -0.0014 0.0500 -0.0399 0.3857 -0.3078 -0.0028 0.0750 -0.0403 0.5785 -0.3105 -0.0041 0.1000 -0.0404 0.7714 -0.3119 -0.0053 0.1250 -0.0404 0.9642 -0.3119 -0.0063 0.1500 -0.0403 1.1571 -0.3110 -0.0071 0.1750 -0.0401 1.3499 -0.3095 -0.0079 0.2000 -0.0398 1.5428 -0.3073 -0.0086 0.2250 -0.0395 1.7356 -0.3046 -0.0092 0.2500 -0.0391 1.9284 -0.3013 -0.0098 0.2750 -0.0386 2.1213 -0.2975 -0.0102 0.3000 -0.0380 2.3141 -0.2932 -0.0107 0.3250 -0.0374 2.5070 -0.2885 -0.0110 0.3500 -0.0367 2.6998 -0.2833 -0.0113 0.3750 -0.0360 2.8927 -0.2778 -0.0116 0.4000 -0.0352 3.0855 -0.2719 -0.0118 0.4250 -0.0344 3.2783 -0.2656 -0.0120 0.4500 -0.0336 3.4712 -0.2589 -0.0121 0.4750 -0.0327 3.6640 -0.2519 -0.0122 0.5000 -0.0317 3.8569 -0.2445 -0.0122 0.5250 -0.0307 4.0497 -0.2368 -0.0121 0.5500 -0.0296 4.2426 -0.2287 -0.0121 0.5750 -0.0285 4.4354 -0.2202 -0.0119 0.6000 -0.0274 4.6283 -0.2114 -0.0118 0.6250 -0.0262 4.8211 -0.2022 -0.0116 0.6500 -0.0250 5.0139 -0.1925 -0.0113 0.6750 -0.0237 5.2068 -0.1825 -0.0110 0.7000 -0.0223 5.3996 -0.1720 -0.0106 0.7250 -0.0209 5.5925 -0.1610 -0.0101 0.7500 -0.0194 5.7853 -0.1494 -0.0096 0.7750 -0.0178 5.9782 -0.1371 -0.0090 0.8000 -0.0160 6.1710 -0.1238 -0.0082 0.8250 -0.0142 6.3638 -0.1096 -0.0074 0.8500 -0.0123 6.5567 -0.0945 -0.0064 0.8750 -0.0102 6.7495 -0.0788 -0.0053 0.9000 -0.0081 6.9424 -0.0627 -0.0042 0.9250 -0.0060 7.1352 -0.0466 -0.0031 0.9500 -0.0040 7.3281 -0.0307 -0.0020 0.9750 -0.0020 7.5209 -0.0152 -0.0010 1.0000 0.0000 7.7138 0.0000 0.0000 1 y= -4.3967 y/(b/2) = -0.4397 chord= 8.4637 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.0079 0.1094 -0.0065 0.1719 -0.0157 0.2344 -0.0226 0.2969 -0.0282 0.3594 -0.0330 0.4219 -0.0374 0.4844 -0.0416 0.5469 -0.0457 0.6094 -0.0500 0.6719 -0.0548 0.7344 -0.0607 0.7969 -0.0708 0.8594 -0.0803 0.9219 -0.0823 0.9844 -0.0780 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0424 0.0000 -0.3589 0.0000 0.0250 -0.0426 0.2116 -0.3607 -0.0013 0.0500 -0.0428 0.4232 -0.3625 -0.0025 0.0750 -0.0430 0.6348 -0.3636 -0.0037 0.1000 -0.0429 0.8464 -0.3634 -0.0048 0.1250 -0.0428 1.0580 -0.3619 -0.0057 0.1500 -0.0425 1.2696 -0.3594 -0.0064 0.1750 -0.0421 1.4812 -0.3563 -0.0071 0.2000 -0.0417 1.6927 -0.3527 -0.0077 0.2250 -0.0412 1.9043 -0.3484 -0.0083 0.2500 -0.0406 2.1159 -0.3435 -0.0088 0.2750 -0.0400 2.3275 -0.3382 -0.0092 0.3000 -0.0393 2.5391 -0.3324 -0.0096 0.3250 -0.0385 2.7507 -0.3262 -0.0099 0.3500 -0.0378 2.9623 -0.3195 -0.0102 0.3750 -0.0369 3.1739 -0.3125 -0.0104 0.4000 -0.0360 3.3855 -0.3051 -0.0106 0.4250 -0.0351 3.5971 -0.2973 -0.0107 0.4500 -0.0342 3.8087 -0.2892 -0.0108 0.4750 -0.0332 4.0203 -0.2807 -0.0109 0.5000 -0.0321 4.2319 -0.2718 -0.0109 0.5250 -0.0310 4.4435 -0.2626 -0.0109 0.5500 -0.0299 4.6551 -0.2531 -0.0108 0.5750 -0.0287 4.8667 -0.2432 -0.0107 0.6000 -0.0275 5.0782 -0.2330 -0.0106 0.6250 -0.0263 5.2898 -0.2223 -0.0104 0.6500 -0.0250 5.5014 -0.2113 -0.0101 0.6750 -0.0236 5.7130 -0.1999 -0.0098 0.7000 -0.0222 5.9246 -0.1880 -0.0095 0.7250 -0.0208 6.1362 -0.1757 -0.0091 0.7500 -0.0192 6.3478 -0.1627 -0.0086 0.7750 -0.0176 6.5594 -0.1490 -0.0081 0.8000 -0.0159 6.7710 -0.1344 -0.0074 0.8250 -0.0140 6.9826 -0.1188 -0.0066 0.8500 -0.0121 7.1942 -0.1024 -0.0057 0.8750 -0.0101 7.4058 -0.0854 -0.0048 0.9000 -0.0080 7.6174 -0.0679 -0.0038 0.9250 -0.0060 7.8290 -0.0505 -0.0028 0.9500 -0.0039 8.0406 -0.0333 -0.0018 0.9750 -0.0020 8.2522 -0.0165 -0.0009 1.0000 0.0000 8.4637 0.0000 0.0000 1 y= -3.7300 y/(b/2) = -0.3730 chord= 9.2137 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 0.0011 0.1094 -0.0122 0.1719 -0.0206 0.2344 -0.0269 0.2969 -0.0320 0.3594 -0.0364 0.4219 -0.0404 0.4844 -0.0441 0.5469 -0.0478 0.6094 -0.0517 0.6719 -0.0560 0.7344 -0.0615 0.7969 -0.0707 0.8594 -0.0794 0.9219 -0.0812 0.9844 -0.0772 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0449 0.0000 -0.4134 0.0000 0.0250 -0.0449 0.2303 -0.4137 -0.0012 0.0500 -0.0449 0.4607 -0.4140 -0.0023 0.0750 -0.0449 0.6910 -0.4137 -0.0034 0.1000 -0.0447 0.9214 -0.4121 -0.0044 0.1250 -0.0444 1.1517 -0.4092 -0.0052 0.1500 -0.0440 1.3821 -0.4053 -0.0059 0.1750 -0.0435 1.6124 -0.4008 -0.0065 0.2000 -0.0429 1.8427 -0.3957 -0.0071 0.2250 -0.0423 2.0731 -0.3900 -0.0076 0.2500 -0.0416 2.3034 -0.3837 -0.0080 0.2750 -0.0409 2.5338 -0.3769 -0.0084 0.3000 -0.0401 2.7641 -0.3697 -0.0087 0.3250 -0.0393 2.9945 -0.3621 -0.0090 0.3500 -0.0384 3.2248 -0.3540 -0.0093 0.3750 -0.0375 3.4552 -0.3456 -0.0095 0.4000 -0.0366 3.6855 -0.3368 -0.0096 0.4250 -0.0356 3.9158 -0.3276 -0.0098 0.4500 -0.0345 4.1462 -0.3181 -0.0098 0.4750 -0.0335 4.3765 -0.3082 -0.0099 0.5000 -0.0323 4.6069 -0.2980 -0.0099 0.5250 -0.0312 4.8372 -0.2875 -0.0099 0.5500 -0.0300 5.0676 -0.2766 -0.0098 0.5750 -0.0288 5.2979 -0.2653 -0.0097 0.6000 -0.0275 5.5282 -0.2537 -0.0096 0.6250 -0.0262 5.7586 -0.2418 -0.0094 0.6500 -0.0249 5.9889 -0.2294 -0.0092 0.6750 -0.0235 6.2193 -0.2167 -0.0089 0.7000 -0.0221 6.4496 -0.2035 -0.0086 0.7250 -0.0206 6.6800 -0.1899 -0.0083 0.7500 -0.0191 6.9103 -0.1756 -0.0078 0.7750 -0.0174 7.1407 -0.1606 -0.0073 0.8000 -0.0157 7.3710 -0.1446 -0.0067 0.8250 -0.0139 7.6013 -0.1278 -0.0060 0.8500 -0.0119 7.8317 -0.1101 -0.0052 0.8750 -0.0100 8.0620 -0.0917 -0.0043 0.9000 -0.0079 8.2924 -0.0730 -0.0034 0.9250 -0.0059 8.5227 -0.0543 -0.0025 0.9500 -0.0039 8.7531 -0.0358 -0.0016 0.9750 -0.0019 8.9834 -0.0178 -0.0008 1.0000 0.0000 9.2137 0.0000 0.0000 1 y= -3.0633 y/(b/2) = -0.3063 chord= 9.9637 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 -0.0047 0.1094 -0.0170 0.1719 -0.0248 0.2344 -0.0305 0.2969 -0.0352 0.3594 -0.0392 0.4219 -0.0428 0.4844 -0.0462 0.5469 -0.0496 0.6094 -0.0531 0.6719 -0.0570 0.7344 -0.0620 0.7969 -0.0704 0.8594 -0.0785 0.9219 -0.0801 0.9844 -0.0762 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0469 0.0000 -0.4669 0.0000 0.0250 -0.0468 0.2491 -0.4658 -0.0011 0.0500 -0.0466 0.4982 -0.4647 -0.0021 0.0750 -0.0465 0.7473 -0.4630 -0.0031 0.1000 -0.0462 0.9964 -0.4600 -0.0040 0.1250 -0.0457 1.2455 -0.4556 -0.0047 0.1500 -0.0452 1.4946 -0.4503 -0.0054 0.1750 -0.0446 1.7437 -0.4443 -0.0059 0.2000 -0.0439 1.9927 -0.4378 -0.0065 0.2250 -0.0432 2.2418 -0.4307 -0.0069 0.2500 -0.0425 2.4909 -0.4230 -0.0073 0.2750 -0.0416 2.7400 -0.4149 -0.0077 0.3000 -0.0408 2.9891 -0.4062 -0.0080 0.3250 -0.0399 3.2382 -0.3972 -0.0082 0.3500 -0.0389 3.4873 -0.3878 -0.0085 0.3750 -0.0379 3.7364 -0.3780 -0.0086 0.4000 -0.0369 3.9855 -0.3678 -0.0088 0.4250 -0.0359 4.2346 -0.3572 -0.0089 0.4500 -0.0348 4.4837 -0.3463 -0.0090 0.4750 -0.0336 4.7328 -0.3351 -0.0090 0.5000 -0.0325 4.9819 -0.3236 -0.0090 0.5250 -0.0313 5.2310 -0.3117 -0.0090 0.5500 -0.0301 5.4801 -0.2995 -0.0090 0.5750 -0.0288 5.7292 -0.2869 -0.0089 0.6000 -0.0275 5.9783 -0.2740 -0.0088 0.6250 -0.0262 6.2273 -0.2607 -0.0086 0.6500 -0.0248 6.4764 -0.2471 -0.0084 0.6750 -0.0234 6.7255 -0.2330 -0.0082 0.7000 -0.0219 6.9746 -0.2186 -0.0079 0.7250 -0.0204 7.2237 -0.2036 -0.0076 0.7500 -0.0189 7.4728 -0.1881 -0.0072 0.7750 -0.0172 7.7219 -0.1718 -0.0067 0.8000 -0.0155 7.9710 -0.1546 -0.0061 0.8250 -0.0137 8.2201 -0.1365 -0.0055 0.8500 -0.0118 8.4692 -0.1175 -0.0048 0.8750 -0.0098 8.7183 -0.0979 -0.0040 0.9000 -0.0078 8.9674 -0.0779 -0.0031 0.9250 -0.0058 9.2165 -0.0579 -0.0023 0.9500 -0.0038 9.4656 -0.0382 -0.0015 0.9750 -0.0019 9.7147 -0.0190 -0.0007 1.0000 0.0000 9.9637 0.0000 0.0000 1 y= -2.3967 y/(b/2) = -0.2397 chord= 10.7137 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 -0.0101 0.1094 -0.0215 0.1719 -0.0287 0.2344 -0.0340 0.2969 -0.0382 0.3594 -0.0419 0.4219 -0.0451 0.4844 -0.0482 0.5469 -0.0512 0.6094 -0.0543 0.6719 -0.0578 0.7344 -0.0623 0.7969 -0.0702 0.8594 -0.0776 0.9219 -0.0789 0.9844 -0.0753 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0487 0.0000 -0.5218 0.0000 0.0250 -0.0485 0.2678 -0.5192 -0.0010 0.0500 -0.0482 0.5357 -0.5165 -0.0019 0.0750 -0.0479 0.8035 -0.5133 -0.0029 0.1000 -0.0475 1.0714 -0.5087 -0.0037 0.1250 -0.0469 1.3392 -0.5028 -0.0043 0.1500 -0.0463 1.6071 -0.4960 -0.0049 0.1750 -0.0456 1.8749 -0.4886 -0.0054 0.2000 -0.0449 2.1427 -0.4805 -0.0059 0.2250 -0.0440 2.4106 -0.4719 -0.0063 0.2500 -0.0432 2.6784 -0.4627 -0.0067 0.2750 -0.0423 2.9463 -0.4531 -0.0070 0.3000 -0.0414 3.2141 -0.4430 -0.0073 0.3250 -0.0404 3.4820 -0.4325 -0.0075 0.3500 -0.0394 3.7498 -0.4216 -0.0077 0.3750 -0.0383 4.0177 -0.4104 -0.0079 0.4000 -0.0372 4.2855 -0.3988 -0.0080 0.4250 -0.0361 4.5533 -0.3868 -0.0081 0.4500 -0.0350 4.8212 -0.3745 -0.0082 0.4750 -0.0338 5.0890 -0.3619 -0.0082 0.5000 -0.0326 5.3569 -0.3489 -0.0082 0.5250 -0.0313 5.6247 -0.3357 -0.0082 0.5500 -0.0301 5.8926 -0.3221 -0.0081 0.5750 -0.0288 6.1604 -0.3082 -0.0081 0.6000 -0.0274 6.4282 -0.2939 -0.0080 0.6250 -0.0261 6.6961 -0.2793 -0.0078 0.6500 -0.0247 6.9639 -0.2644 -0.0076 0.6750 -0.0232 7.2318 -0.2490 -0.0074 0.7000 -0.0218 7.4996 -0.2333 -0.0072 0.7250 -0.0203 7.7675 -0.2171 -0.0069 0.7500 -0.0187 8.0353 -0.2003 -0.0065 0.7750 -0.0171 8.3032 -0.1827 -0.0061 0.8000 -0.0153 8.5710 -0.1643 -0.0056 0.8250 -0.0135 8.8388 -0.1449 -0.0050 0.8500 -0.0116 9.1067 -0.1247 -0.0043 0.8750 -0.0097 9.3745 -0.1039 -0.0036 0.9000 -0.0077 9.6424 -0.0827 -0.0029 0.9250 -0.0057 9.9102 -0.0615 -0.0021 0.9500 -0.0038 10.1781 -0.0406 -0.0014 0.9750 -0.0019 10.4459 -0.0202 -0.0007 1.0000 0.0000 10.7137 0.0000 0.0000 1 y= -1.7300 y/(b/2) = -0.1730 chord= 11.4637 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 -0.0157 0.1094 -0.0263 0.1719 -0.0329 0.2344 -0.0377 0.2969 -0.0416 0.3594 -0.0448 0.4219 -0.0477 0.4844 -0.0504 0.5469 -0.0530 0.6094 -0.0557 0.6719 -0.0588 0.7344 -0.0628 0.7969 -0.0699 0.8594 -0.0767 0.9219 -0.0779 0.9844 -0.0744 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0507 0.0000 -0.5816 0.0000 0.0250 -0.0503 0.2866 -0.5772 -0.0009 0.0500 -0.0500 0.5732 -0.5728 -0.0018 0.0750 -0.0495 0.8598 -0.5677 -0.0026 0.1000 -0.0490 1.1464 -0.5614 -0.0033 0.1250 -0.0483 1.4330 -0.5537 -0.0039 0.1500 -0.0476 1.7196 -0.5452 -0.0044 0.1750 -0.0468 2.0062 -0.5359 -0.0049 0.2000 -0.0459 2.2927 -0.5262 -0.0053 0.2250 -0.0450 2.5793 -0.5158 -0.0057 0.2500 -0.0440 2.8659 -0.5050 -0.0060 0.2750 -0.0431 3.1525 -0.4936 -0.0063 0.3000 -0.0420 3.4391 -0.4819 -0.0065 0.3250 -0.0410 3.7257 -0.4697 -0.0067 0.3500 -0.0399 4.0123 -0.4572 -0.0069 0.3750 -0.0388 4.2989 -0.4443 -0.0070 0.4000 -0.0376 4.5855 -0.4310 -0.0072 0.4250 -0.0364 4.8721 -0.4175 -0.0072 0.4500 -0.0352 5.1587 -0.4036 -0.0073 0.4750 -0.0340 5.4453 -0.3894 -0.0073 0.5000 -0.0327 5.7319 -0.3750 -0.0073 0.5250 -0.0314 6.0185 -0.3602 -0.0073 0.5500 -0.0301 6.3051 -0.3451 -0.0073 0.5750 -0.0288 6.5917 -0.3298 -0.0072 0.6000 -0.0274 6.8782 -0.3141 -0.0071 0.6250 -0.0260 7.1648 -0.2981 -0.0070 0.6500 -0.0246 7.4514 -0.2818 -0.0068 0.6750 -0.0231 7.7380 -0.2650 -0.0066 0.7000 -0.0216 8.0246 -0.2480 -0.0064 0.7250 -0.0201 8.3112 -0.2305 -0.0062 0.7500 -0.0185 8.5978 -0.2124 -0.0058 0.7750 -0.0169 8.8844 -0.1935 -0.0055 0.8000 -0.0152 9.1710 -0.1738 -0.0050 0.8250 -0.0134 9.4576 -0.1532 -0.0045 0.8500 -0.0115 9.7442 -0.1318 -0.0039 0.8750 -0.0096 10.0308 -0.1098 -0.0032 0.9000 -0.0076 10.3174 -0.0874 -0.0025 0.9250 -0.0057 10.6040 -0.0650 -0.0019 0.9500 -0.0037 10.8906 -0.0429 -0.0012 0.9750 -0.0019 11.1772 -0.0213 -0.0006 1.0000 0.0000 11.4637 0.0000 0.0000 1 y= -1.0633 y/(b/2) = -0.1063 chord= 12.2137 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 -0.0224 0.1094 -0.0324 0.1719 -0.0385 0.2344 -0.0429 0.2969 -0.0463 0.3594 -0.0490 0.4219 -0.0514 0.4844 -0.0535 0.5469 -0.0555 0.6094 -0.0577 0.6719 -0.0602 0.7344 -0.0635 0.7969 -0.0699 0.8594 -0.0760 0.9219 -0.0768 0.9844 -0.0734 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0536 0.0000 -0.6541 0.0000 0.0250 -0.0530 0.3053 -0.6473 -0.0008 0.0500 -0.0524 0.6107 -0.6406 -0.0016 0.0750 -0.0518 0.9160 -0.6332 -0.0023 0.1000 -0.0511 1.2214 -0.6245 -0.0029 0.1250 -0.0503 1.5267 -0.6144 -0.0034 0.1500 -0.0494 1.8321 -0.6035 -0.0039 0.1750 -0.0485 2.1374 -0.5919 -0.0043 0.2000 -0.0475 2.4427 -0.5798 -0.0046 0.2250 -0.0464 2.7481 -0.5672 -0.0049 0.2500 -0.0454 3.0534 -0.5540 -0.0052 0.2750 -0.0442 3.3588 -0.5404 -0.0054 0.3000 -0.0431 3.6641 -0.5265 -0.0056 0.3250 -0.0419 3.9695 -0.5121 -0.0058 0.3500 -0.0407 4.2748 -0.4974 -0.0059 0.3750 -0.0395 4.5802 -0.4824 -0.0060 0.4000 -0.0382 4.8855 -0.4671 -0.0061 0.4250 -0.0370 5.1908 -0.4515 -0.0062 0.4500 -0.0357 5.4962 -0.4357 -0.0062 0.4750 -0.0344 5.8015 -0.4196 -0.0062 0.5000 -0.0330 6.1069 -0.4032 -0.0062 0.5250 -0.0317 6.4122 -0.3866 -0.0062 0.5500 -0.0303 6.7176 -0.3698 -0.0062 0.5750 -0.0289 7.0229 -0.3526 -0.0061 0.6000 -0.0275 7.3283 -0.3353 -0.0060 0.6250 -0.0260 7.6336 -0.3176 -0.0059 0.6500 -0.0245 7.9389 -0.2997 -0.0058 0.6750 -0.0230 8.2443 -0.2814 -0.0056 0.7000 -0.0215 8.5496 -0.2629 -0.0055 0.7250 -0.0200 8.8550 -0.2439 -0.0052 0.7500 -0.0184 9.1603 -0.2244 -0.0050 0.7750 -0.0167 9.4657 -0.2042 -0.0047 0.8000 -0.0150 9.7710 -0.1832 -0.0043 0.8250 -0.0132 10.0763 -0.1613 -0.0038 0.8500 -0.0114 10.3817 -0.1387 -0.0033 0.8750 -0.0094 10.6870 -0.1154 -0.0028 0.9000 -0.0075 10.9924 -0.0918 -0.0022 0.9250 -0.0056 11.2977 -0.0683 -0.0016 0.9500 -0.0037 11.6031 -0.0451 -0.0010 0.9750 -0.0018 11.9084 -0.0224 -0.0005 1.0000 0.0000 12.2137 0.0000 0.0000 1 y= -0.3650 y/(b/2) = -0.0365 chord= 12.9994 slopes, dz/dx, at control points, from front to rear x/c dz/dx 0.0469 -0.0362 0.1094 -0.0460 0.1719 -0.0514 0.2344 -0.0548 0.2969 -0.0571 0.3594 -0.0588 0.4219 -0.0599 0.4844 -0.0608 0.5469 -0.0616 0.6094 -0.0624 0.6719 -0.0636 0.7344 -0.0657 0.7969 -0.0705 0.8594 -0.0754 0.9219 -0.0756 0.9844 -0.0722 mean camber shape (interpolated to 41 points) x/c z/c delta x delta z (z-zle)/c 0.0000 -0.0602 0.0000 -0.7826 0.0000 0.0250 -0.0593 0.3250 -0.7709 -0.0006 0.0500 -0.0584 0.6500 -0.7592 -0.0012 0.0750 -0.0575 0.9750 -0.7468 -0.0018 0.1000 -0.0564 1.2999 -0.7331 -0.0022 0.1250 -0.0552 1.6249 -0.7181 -0.0026 0.1500 -0.0540 1.9499 -0.7021 -0.0028 0.1750 -0.0527 2.2749 -0.6856 -0.0031 0.2000 -0.0514 2.5999 -0.6686 -0.0033 0.2250 -0.0501 2.9249 -0.6512 -0.0034 0.2500 -0.0487 3.2498 -0.6333 -0.0036 0.2750 -0.0473 3.5748 -0.6151 -0.0037 0.3000 -0.0459 3.8998 -0.5966 -0.0038 0.3250 -0.0445 4.2248 -0.5779 -0.0038 0.3500 -0.0430 4.5498 -0.5590 -0.0039 0.3750 -0.0415 4.8748 -0.5399 -0.0039 0.4000 -0.0400 5.1998 -0.5206 -0.0039 0.4250 -0.0386 5.5247 -0.5012 -0.0039 0.4500 -0.0371 5.8497 -0.4816 -0.0039 0.4750 -0.0355 6.1747 -0.4620 -0.0039 0.5000 -0.0340 6.4997 -0.4422 -0.0039 0.5250 -0.0325 6.8247 -0.4223 -0.0039 0.5500 -0.0310 7.1497 -0.4024 -0.0039 0.5750 -0.0294 7.4746 -0.3823 -0.0038 0.6000 -0.0279 7.7996 -0.3621 -0.0038 0.6250 -0.0263 8.1246 -0.3418 -0.0037 0.6500 -0.0247 8.4496 -0.3214 -0.0037 0.6750 -0.0231 8.7746 -0.3008 -0.0036 0.7000 -0.0215 9.0996 -0.2800 -0.0035 0.7250 -0.0199 9.4246 -0.2589 -0.0034 0.7500 -0.0183 9.7495 -0.2375 -0.0032 0.7750 -0.0166 10.0745 -0.2156 -0.0030 0.8000 -0.0148 10.3995 -0.1929 -0.0028 0.8250 -0.0130 10.7245 -0.1695 -0.0025 0.8500 -0.0112 11.0495 -0.1455 -0.0022 0.8750 -0.0093 11.3745 -0.1210 -0.0018 0.9000 -0.0074 11.6994 -0.0962 -0.0014 0.9250 -0.0055 12.0244 -0.0715 -0.0010 0.9500 -0.0036 12.3494 -0.0472 -0.0006 0.9750 -0.0018 12.6744 -0.0235 -0.0003 1.0000 0.0000 12.9994 0.0000 0.0000 1 twist table i y y/(b/2) twist 1 -6.39667 -0.63967 -1.36802 2 -5.73000 -0.57300 -0.01207 3 -5.06333 -0.50633 0.35997 4 -4.39667 -0.43967 0.61278 5 -3.73000 -0.37300 0.80696 6 -3.06333 -0.30633 0.96491 7 -2.39667 -0.23967 1.11046 8 -1.73000 -0.17300 1.27246 9 -1.06333 -0.10633 1.49747 10 -0.36500 -0.03650 2.04737 11 -9.66667 -0.96667 -0.58534 12 -9.00000 -0.90000 0.60385 13 -8.33333 -0.83333 0.83171 14 -7.66667 -0.76667 0.94837 15 -7.03167 -0.70317 1.12539 16 -6.39667 -0.63967 1.52525 17 -5.73000 -0.57300 1.94924 18 -5.06333 -0.50633 2.23634 19 -4.39667 -0.43967 2.42836 20 -3.73000 -0.37300 2.56886 21 -3.06333 -0.30633 2.68309 22 -2.39667 -0.23967 2.78831 23 -1.73000 -0.17300 2.90416 24 -1.06333 -0.10633 3.06546 25 -0.36500 -0.03650 3.44503 calculation complete williams-imac:LAMDESfolder williamhmason$