Airfoil: FX 63-137 (C) Builder: Y. Tinel Comment: 'u.s.t. located at 2% chord, l.s.t. located at 5% chord' Number of Reynolds #'s: 5 Average Reynolds #: 100069 Number of angles of attack: 21 alpha / Cl / Cd / Spanwise Cd's >>> -7.26 -0.323 0.1440 0.1399 0.1443 0.1444 0.1463 0.1473 0.1463 0.1426 0.1409 -6.23 -0.301 0.1257 0.1288 0.1272 0.1258 0.1242 0.1256 0.1253 0.1230 0.1255 -5.17 -0.025 0.0434 0.0463 0.0445 0.0446 0.0430 0.0414 0.0405 0.0433 0.0441 -4.13 0.112 0.0368 0.0370 0.0374 0.0377 0.0367 0.0358 0.0371 0.0364 0.0362 -3.07 0.258 0.0357 0.0361 0.0357 0.0361 0.0361 0.0351 0.0353 0.0362 0.0351 -2.04 0.378 0.0362 0.0366 0.0364 0.0366 0.0371 0.0360 0.0362 0.0354 0.0356 -1.00 0.473 0.0403 0.0410 0.0397 0.0405 0.0409 0.0407 0.0411 0.0398 0.0392 -0.01 0.547 0.0456 0.0459 0.0456 0.0458 0.0467 0.0462 0.0451 0.0445 0.0452 1.04 0.613 0.0532 0.0524 0.0524 0.0543 0.0542 0.0547 0.0532 0.0525 0.0518 2.02 0.673 0.0592 0.0585 0.0590 0.0611 0.0602 0.0594 0.0606 0.0593 0.0552 3.07 0.878 0.0405 0.0399 0.0401 0.0424 0.0401 0.0405 0.0389 0.0410 0.0409 4.08 1.046 0.0283 0.0300 0.0282 0.0261 0.0271 0.0281 0.0276 0.0292 0.0298 5.16 1.171 0.0246 0.0257 0.0253 0.0237 0.0231 0.0238 0.0243 0.0249 0.0259 6.13 1.263 0.0235 0.0253 0.0261 0.0238 0.0195 0.0209 0.0236 0.0244 0.0243 7.23 1.359 0.0242 0.0248 0.0274 0.0232 0.0234 0.0225 0.0265 0.0224 0.0233 8.20 1.429 0.0260 0.0239 0.0286 0.0264 0.0267 0.0266 0.0284 0.0222 0.0250 9.24 1.489 0.0295 0.0290 0.0296 0.0289 0.0314 0.0326 0.0288 0.0278 0.0278 10.22 1.523 0.0350 0.0350 0.0341 0.0333 0.0399 0.0399 0.0337 0.0310 0.0331 11.29 1.519 0.0505 0.0426 0.0414 0.0512 0.0726 0.0717 0.0497 0.0366 0.0377 12.24 1.494 0.0744 0.0499 0.0599 0.0861 0.1089 0.1058 0.0884 0.0533 0.0427 13.23 1.462 0.1096 0.0708 0.0982 0.1246 0.1472 0.1471 0.1244 0.0975 0.0668 Tabulated from data in file bm05007.dat & reduced using program C10.20 Average Reynolds #: 150199 Number of angles of attack: 21 alpha / Cl / Cd / Spanwise Cd's >>> -7.20 -0.145 0.1164 0.1192 0.1188 0.1168 0.1136 0.1113 0.1133 0.1166 0.1213 -6.13 0.037 0.0460 0.0486 0.0464 0.0455 0.0450 0.0433 0.0449 0.0464 0.0481 -5.10 0.198 0.0281 0.0293 0.0282 0.0284 0.0286 0.0274 0.0273 0.0272 0.0285 -4.08 0.330 0.0229 0.0236 0.0231 0.0228 0.0239 0.0222 0.0216 0.0232 0.0227 -3.04 0.457 0.0205 0.0215 0.0207 0.0199 0.0212 0.0210 0.0191 0.0207 0.0195 -2.02 0.573 0.0194 0.0198 0.0194 0.0195 0.0202 0.0195 0.0183 0.0199 0.0190 -0.99 0.678 0.0197 0.0199 0.0196 0.0202 0.0206 0.0197 0.0185 0.0199 0.0191 -0.01 0.774 0.0206 0.0206 0.0210 0.0210 0.0218 0.0202 0.0197 0.0205 0.0202 1.05 0.880 0.0203 0.0218 0.0221 0.0208 0.0208 0.0185 0.0197 0.0177 0.0209 2.11 0.988 0.0185 0.0211 0.0225 0.0175 0.0162 0.0147 0.0189 0.0155 0.0216 3.11 1.079 0.0178 0.0144 0.0238 0.0157 0.0178 0.0160 0.0201 0.0157 0.0187 4.12 1.169 0.0174 0.0163 0.0180 0.0160 0.0183 0.0171 0.0181 0.0178 0.0174 5.16 1.243 0.0202 0.0212 0.0208 0.0202 0.0207 0.0207 0.0183 0.0192 0.0202 6.18 1.313 0.0233 0.0233 0.0229 0.0217 0.0243 0.0236 0.0234 0.0235 0.0240 7.19 1.366 0.0273 0.0282 0.0269 0.0262 0.0284 0.0291 0.0270 0.0254 0.0270 8.20 1.413 0.0322 0.0337 0.0320 0.0314 0.0324 0.0345 0.0318 0.0307 0.0312 9.21 1.443 0.0396 0.0417 0.0392 0.0392 0.0416 0.0454 0.0389 0.0351 0.0357 10.23 1.465 0.0516 0.0525 0.0537 0.0540 0.0598 0.0629 0.0497 0.0395 0.0410 11.22 1.476 0.0740 0.0588 0.0667 0.0814 0.0949 0.0986 0.0833 0.0612 0.0473 12.23 1.484 0.0943 0.0786 0.0889 0.1032 0.1139 0.1130 0.1034 0.0866 0.0670 13.22 1.486 0.1105 0.1047 0.1122 0.1129 0.1177 0.1182 0.1167 0.1091 0.0926 Tabulated from data in file bm05009.dat & reduced using program C10.20 Average Reynolds #: 199966 Number of angles of attack: 18 alpha / Cl / Cd / Spanwise Cd's >>> -7.18 -0.079 0.0892 0.0898 0.0878 0.0868 0.0872 0.0876 0.0853 0.0908 0.0986 -6.07 0.114 0.0287 0.0301 0.0291 0.0280 0.0291 0.0270 0.0277 0.0278 0.0310 -5.10 0.235 0.0204 0.0210 0.0211 0.0206 0.0207 0.0197 0.0194 0.0195 0.0211 -4.06 0.352 0.0169 0.0166 0.0180 0.0169 0.0169 0.0161 0.0164 0.0173 0.0171 -3.00 0.462 0.0155 0.0158 0.0159 0.0153 0.0160 0.0159 0.0143 0.0160 0.0148 -2.05 0.561 0.0152 0.0154 0.0155 0.0152 0.0159 0.0160 0.0144 0.0142 0.0149 -1.00 0.670 0.0147 0.0155 0.0158 0.0152 0.0157 0.0141 0.0144 0.0123 0.0149 0.08 0.787 0.0139 0.0120 0.0201 0.0129 0.0134 0.0122 0.0158 0.0106 0.0145 1.06 0.883 0.0146 0.0125 0.0185 0.0154 0.0143 0.0141 0.0158 0.0134 0.0130 2.13 0.971 0.0155 0.0138 0.0154 0.0170 0.0182 0.0153 0.0147 0.0145 0.0153 3.11 1.040 0.0186 0.0186 0.0179 0.0188 0.0194 0.0182 0.0188 0.0184 0.0186 4.12 1.119 0.0200 0.0199 0.0195 0.0193 0.0206 0.0202 0.0199 0.0206 0.0205 5.13 1.197 0.0221 0.0218 0.0222 0.0213 0.0225 0.0225 0.0210 0.0235 0.0216 6.16 1.263 0.0251 0.0257 0.0250 0.0241 0.0249 0.0257 0.0252 0.0248 0.0257 7.17 1.325 0.0284 0.0291 0.0286 0.0274 0.0278 0.0294 0.0285 0.0275 0.0286 8.17 1.376 0.0328 0.0341 0.0326 0.0316 0.0326 0.0361 0.0330 0.0314 0.0314 9.23 1.413 0.0416 0.0385 0.0387 0.0397 0.0483 0.0543 0.0436 0.0352 0.0347 10.20 1.437 0.0562 0.0452 0.0459 0.0522 0.0721 0.0809 0.0669 0.0463 0.0404 Tabulated from data in file bm05011.dat & reduced using program C10.20 Average Reynolds #: 350058 Number of angles of attack: 18 alpha / Cl / Cd / Spanwise Cd's >>> -7.15 -0.033 0.0711 0.0717 0.0701 0.0697 0.0698 0.0682 0.0697 0.0715 0.0781 -6.07 0.139 0.0158 0.0169 0.0171 0.0156 0.0166 0.0143 0.0155 0.0152 0.0151 -5.09 0.248 0.0142 0.0143 0.0144 0.0145 0.0145 0.0138 0.0141 0.0138 0.0144 -4.07 0.364 0.0121 0.0118 0.0127 0.0131 0.0123 0.0116 0.0123 0.0113 0.0121 -3.05 0.479 0.0119 0.0125 0.0151 0.0115 0.0121 0.0109 0.0123 0.0100 0.0109 -2.00 0.581 0.0115 0.0113 0.0134 0.0110 0.0124 0.0115 0.0116 0.0106 0.0106 -1.00 0.666 0.0129 0.0124 0.0136 0.0145 0.0142 0.0127 0.0112 0.0121 0.0127 0.03 0.759 0.0149 0.0148 0.0152 0.0159 0.0150 0.0154 0.0137 0.0144 0.0147 1.07 0.855 0.0160 0.0158 0.0159 0.0171 0.0165 0.0162 0.0154 0.0152 0.0156 2.11 0.950 0.0173 0.0173 0.0168 0.0182 0.0181 0.0170 0.0174 0.0169 0.0168 3.12 1.042 0.0188 0.0188 0.0179 0.0190 0.0193 0.0186 0.0196 0.0186 0.0188 4.13 1.129 0.0207 0.0208 0.0196 0.0205 0.0212 0.0204 0.0214 0.0206 0.0213 5.14 1.205 0.0225 0.0228 0.0220 0.0217 0.0224 0.0227 0.0225 0.0223 0.0235 6.16 1.289 0.0248 0.0255 0.0246 0.0234 0.0244 0.0255 0.0248 0.0244 0.0259 7.19 1.348 0.0278 0.0287 0.0274 0.0269 0.0273 0.0296 0.0279 0.0270 0.0280 8.19 1.388 0.0335 0.0333 0.0312 0.0319 0.0353 0.0403 0.0343 0.0311 0.0309 9.23 1.422 0.0440 0.0412 0.0403 0.0408 0.0508 0.0586 0.0494 0.0358 0.0348 10.22 1.448 0.0607 0.0480 0.0456 0.0555 0.0774 0.0863 0.0764 0.0565 0.0401 Tabulated from data in file bm05013.dat & reduced using program C10.20 Average Reynolds #: 499532 Number of angles of attack: 18 alpha / Cl / Cd / Spanwise Cd's >>> -7.21 -0.027 0.0675 0.0682 0.0682 0.0667 0.0653 0.0649 0.0663 0.0663 0.0745 -6.13 0.142 0.0144 0.0135 0.0144 0.0136 0.0158 0.0140 0.0148 0.0145 0.0146 -5.09 0.260 0.0115 0.0108 0.0113 0.0112 0.0123 0.0112 0.0124 0.0112 0.0116 -4.07 0.366 0.0111 0.0100 0.0118 0.0112 0.0119 0.0109 0.0112 0.0113 0.0105 -3.09 0.463 0.0112 0.0106 0.0116 0.0119 0.0116 0.0111 0.0107 0.0116 0.0108 -2.02 0.572 0.0121 0.0113 0.0124 0.0126 0.0130 0.0124 0.0116 0.0120 0.0115 -0.99 0.667 0.0133 0.0128 0.0135 0.0138 0.0140 0.0138 0.0127 0.0126 0.0130 -0.02 0.749 0.0145 0.0143 0.0144 0.0153 0.0151 0.0151 0.0140 0.0139 0.0142 1.07 0.853 0.0158 0.0158 0.0154 0.0166 0.0161 0.0162 0.0157 0.0153 0.0154 2.08 0.943 0.0171 0.0172 0.0164 0.0176 0.0175 0.0172 0.0174 0.0168 0.0165 3.06 1.032 0.0183 0.0187 0.0174 0.0185 0.0186 0.0181 0.0191 0.0181 0.0180 4.16 1.135 0.0201 0.0202 0.0192 0.0195 0.0204 0.0201 0.0208 0.0200 0.0205 5.18 1.218 0.0221 0.0222 0.0216 0.0207 0.0218 0.0228 0.0224 0.0222 0.0232 6.16 1.287 0.0248 0.0251 0.0243 0.0227 0.0238 0.0262 0.0249 0.0250 0.0263 7.21 1.350 0.0294 0.0302 0.0284 0.0266 0.0278 0.0324 0.0310 0.0298 0.0292 8.22 1.395 0.0362 0.0360 0.0330 0.0325 0.0376 0.0474 0.0407 0.0318 0.0310 9.23 1.431 0.0486 0.0433 0.0408 0.0410 0.0564 0.0690 0.0623 0.0410 0.0352 10.22 1.456 0.0667 0.0509 0.0488 0.0562 0.0775 0.0919 0.0892 0.0713 0.0481 Tabulated from data in file bm05015.dat & reduced using program C10.20 File fx63137_tf.drg created using program C10.20 on Thu May 22 17:01:35 2003