Airfoil: S822 (B) Builder: Y. Tinel Comment: 'clean' Number of Reynolds #'s: 5 Average Reynolds #: 100174 Number of angles of attack: 25 alpha / Cl / Cd / Spanwise Cd's >>> -10.25 -0.782 0.0374 0.0386 0.0383 0.0383 0.0369 0.0360 0.0359 0.0370 0.0380 -9.30 -0.772 0.0324 0.0333 0.0327 0.0330 0.0322 0.0307 0.0316 0.0328 0.0329 -8.20 -0.715 0.0269 0.0272 0.0275 0.0258 0.0262 0.0261 0.0269 0.0268 0.0289 -7.24 -0.623 0.0245 0.0278 0.0254 0.0209 0.0255 0.0254 0.0234 0.0218 0.0260 -6.24 -0.532 0.0242 0.0255 0.0265 0.0220 0.0248 0.0238 0.0221 0.0237 0.0252 -5.21 -0.443 0.0240 0.0252 0.0236 0.0213 0.0247 0.0248 0.0240 0.0238 0.0248 -4.14 -0.353 0.0244 0.0258 0.0245 0.0255 0.0242 0.0235 0.0239 0.0235 0.0241 -3.14 -0.283 0.0283 0.0308 0.0291 0.0270 0.0281 0.0274 0.0276 0.0291 0.0277 -2.11 -0.239 0.0302 0.0334 0.0315 0.0299 0.0285 0.0285 0.0280 0.0300 0.0322 -1.10 -0.203 0.0279 0.0296 0.0279 0.0286 0.0261 0.0281 0.0268 0.0278 0.0286 -0.09 -0.106 0.0305 0.0320 0.0337 0.0311 0.0284 0.0294 0.0301 0.0314 0.0281 0.93 0.011 0.0347 0.0333 0.0351 0.0353 0.0347 0.0350 0.0363 0.0356 0.0321 1.97 0.071 0.0360 0.0380 0.0371 0.0361 0.0354 0.0346 0.0360 0.0357 0.0354 2.96 0.159 0.0422 0.0444 0.0426 0.0432 0.0408 0.0415 0.0412 0.0412 0.0426 4.01 0.251 0.0497 0.0517 0.0511 0.0507 0.0502 0.0484 0.0487 0.0485 0.0488 5.02 0.349 0.0567 0.0572 0.0572 0.0581 0.0582 0.0555 0.0560 0.0551 0.0559 6.08 0.573 0.0419 0.0429 0.0413 0.0398 0.0425 0.0435 0.0442 0.0409 0.0403 7.19 0.919 0.0221 0.0217 0.0218 0.0213 0.0224 0.0213 0.0227 0.0230 0.0222 8.20 1.004 0.0201 0.0196 0.0208 0.0200 0.0202 0.0181 0.0223 0.0204 0.0196 9.20 1.058 0.0242 0.0225 0.0246 0.0246 0.0242 0.0255 0.0251 0.0241 0.0231 10.24 1.055 0.0335 0.0347 0.0316 0.0312 0.0341 0.0325 0.0344 0.0341 0.0351 11.20 1.060 0.0433 0.0441 0.0427 0.0428 0.0458 0.0414 0.0432 0.0434 0.0429 12.23 1.073 0.0530 0.0491 0.0521 0.0554 0.0568 0.0560 0.0536 0.0521 0.0493 13.21 1.086 0.0640 0.0627 0.0636 0.0661 0.0694 0.0691 0.0654 0.0591 0.0571 14.19 1.085 0.0811 0.0793 0.0814 0.0826 0.0859 0.0872 0.0836 0.0759 0.0727 Tabulated from data in file bm05017.dat & reduced using program C10.20 Average Reynolds #: 150045 Number of angles of attack: 25 alpha / Cl / Cd / Spanwise Cd's >>> -10.27 -0.820 0.0341 0.0351 0.0341 0.0347 0.0340 0.0340 0.0331 0.0339 0.0341 -9.30 -0.797 0.0294 0.0309 0.0296 0.0307 0.0286 0.0276 0.0284 0.0302 0.0290 -8.24 -0.717 0.0250 0.0261 0.0257 0.0262 0.0251 0.0242 0.0246 0.0245 0.0236 -7.21 -0.614 0.0227 0.0226 0.0234 0.0234 0.0233 0.0218 0.0218 0.0229 0.0226 -6.13 -0.507 0.0213 0.0211 0.0216 0.0222 0.0206 0.0206 0.0217 0.0217 0.0210 -5.15 -0.406 0.0214 0.0214 0.0218 0.0231 0.0211 0.0201 0.0218 0.0215 0.0208 -4.13 -0.314 0.0224 0.0222 0.0224 0.0237 0.0224 0.0218 0.0222 0.0221 0.0221 -3.10 -0.222 0.0245 0.0250 0.0254 0.0256 0.0239 0.0237 0.0243 0.0239 0.0240 -2.09 -0.147 0.0265 0.0276 0.0272 0.0274 0.0259 0.0257 0.0264 0.0263 0.0257 -1.09 -0.090 0.0286 0.0299 0.0297 0.0297 0.0282 0.0273 0.0281 0.0282 0.0279 -0.04 -0.041 0.0301 0.0313 0.0308 0.0308 0.0305 0.0291 0.0292 0.0293 0.0299 0.93 0.015 0.0318 0.0322 0.0332 0.0333 0.0316 0.0311 0.0315 0.0307 0.0307 1.94 0.119 0.0340 0.0355 0.0362 0.0360 0.0341 0.0325 0.0335 0.0319 0.0323 2.98 0.256 0.0353 0.0361 0.0353 0.0359 0.0352 0.0353 0.0342 0.0352 0.0348 4.04 0.457 0.0324 0.0317 0.0328 0.0329 0.0327 0.0328 0.0326 0.0320 0.0320 5.13 0.780 0.0213 0.0205 0.0228 0.0226 0.0217 0.0213 0.0202 0.0213 0.0204 6.13 0.868 0.0178 0.0172 0.0189 0.0186 0.0184 0.0173 0.0174 0.0176 0.0169 7.16 0.938 0.0162 0.0149 0.0168 0.0157 0.0159 0.0159 0.0169 0.0167 0.0165 8.23 0.998 0.0178 0.0171 0.0172 0.0172 0.0193 0.0173 0.0188 0.0179 0.0173 9.21 1.040 0.0223 0.0215 0.0216 0.0225 0.0235 0.0221 0.0238 0.0223 0.0212 10.21 1.050 0.0298 0.0288 0.0260 0.0277 0.0315 0.0287 0.0325 0.0322 0.0307 11.22 1.051 0.0399 0.0418 0.0393 0.0367 0.0405 0.0416 0.0429 0.0413 0.0352 12.19 1.065 0.0501 0.0470 0.0508 0.0546 0.0575 0.0551 0.0479 0.0443 0.0432 13.20 1.078 0.0621 0.0613 0.0636 0.0684 0.0707 0.0682 0.0601 0.0539 0.0506 14.21 1.081 0.0787 0.0820 0.0840 0.0861 0.0854 0.0802 0.0748 0.0684 0.0686 Tabulated from data in file bm05019.dat & reduced using program C10.20 Average Reynolds #: 200410 Number of angles of attack: 25 alpha / Cl / Cd / Spanwise Cd's >>> -10.29 -0.777 0.0297 0.0303 0.0296 0.0304 0.0289 0.0285 0.0291 0.0302 0.0310 -9.24 -0.698 0.0244 0.0260 0.0236 0.0252 0.0238 0.0231 0.0245 0.0242 0.0248 -8.20 -0.610 0.0209 0.0208 0.0213 0.0222 0.0204 0.0203 0.0205 0.0209 0.0207 -7.18 -0.500 0.0191 0.0185 0.0194 0.0207 0.0187 0.0185 0.0190 0.0192 0.0188 -6.16 -0.405 0.0181 0.0180 0.0185 0.0194 0.0177 0.0177 0.0180 0.0181 0.0179 -5.17 -0.313 0.0177 0.0176 0.0182 0.0189 0.0172 0.0170 0.0177 0.0176 0.0170 -4.13 -0.216 0.0184 0.0186 0.0188 0.0195 0.0179 0.0178 0.0183 0.0186 0.0176 -3.08 -0.120 0.0190 0.0191 0.0199 0.0197 0.0188 0.0185 0.0186 0.0192 0.0184 -2.08 -0.032 0.0202 0.0207 0.0213 0.0206 0.0199 0.0196 0.0199 0.0203 0.0196 -1.01 0.061 0.0217 0.0222 0.0225 0.0218 0.0214 0.0211 0.0214 0.0220 0.0209 0.01 0.154 0.0224 0.0229 0.0232 0.0228 0.0222 0.0217 0.0220 0.0223 0.0220 1.03 0.245 0.0230 0.0238 0.0234 0.0234 0.0230 0.0225 0.0224 0.0224 0.0231 2.04 0.347 0.0223 0.0227 0.0224 0.0228 0.0223 0.0221 0.0220 0.0221 0.0220 3.08 0.449 0.0209 0.0210 0.0211 0.0212 0.0214 0.0209 0.0199 0.0212 0.0200 4.09 0.589 0.0188 0.0179 0.0185 0.0195 0.0189 0.0196 0.0177 0.0206 0.0172 5.16 0.751 0.0159 0.0149 0.0167 0.0170 0.0160 0.0159 0.0153 0.0165 0.0154 6.16 0.887 0.0141 0.0125 0.0151 0.0156 0.0143 0.0133 0.0141 0.0152 0.0127 7.19 0.941 0.0138 0.0129 0.0136 0.0143 0.0143 0.0131 0.0148 0.0137 0.0136 8.15 0.988 0.0169 0.0160 0.0162 0.0170 0.0188 0.0163 0.0181 0.0167 0.0163 9.17 1.027 0.0215 0.0207 0.0208 0.0219 0.0221 0.0218 0.0227 0.0213 0.0205 10.21 1.040 0.0295 0.0295 0.0275 0.0255 0.0283 0.0283 0.0355 0.0332 0.0283 11.26 1.049 0.0390 0.0398 0.0416 0.0373 0.0362 0.0450 0.0431 0.0360 0.0332 12.21 1.062 0.0492 0.0441 0.0476 0.0538 0.0604 0.0572 0.0485 0.0422 0.0399 13.19 1.077 0.0614 0.0587 0.0653 0.0726 0.0726 0.0692 0.0581 0.0490 0.0461 14.17 1.084 0.0779 0.0806 0.0841 0.0880 0.0869 0.0827 0.0760 0.0646 0.0600 Tabulated from data in file bm05021.dat & reduced using program C10.20 Average Reynolds #: 349965 Number of angles of attack: 25 alpha / Cl / Cd / Spanwise Cd's >>> -10.21 -0.657 0.0204 0.0203 0.0201 0.0222 0.0192 0.0193 0.0201 0.0211 0.0206 -9.22 -0.612 0.0173 0.0176 0.0170 0.0187 0.0164 0.0167 0.0169 0.0177 0.0171 -8.20 -0.538 0.0151 0.0151 0.0153 0.0165 0.0144 0.0148 0.0151 0.0149 0.0145 -7.14 -0.459 0.0138 0.0133 0.0139 0.0153 0.0133 0.0137 0.0136 0.0135 0.0136 -6.17 -0.373 0.0127 0.0122 0.0132 0.0143 0.0121 0.0128 0.0124 0.0124 0.0124 -5.15 -0.279 0.0121 0.0118 0.0125 0.0132 0.0120 0.0118 0.0117 0.0121 0.0115 -4.17 -0.190 0.0115 0.0115 0.0117 0.0123 0.0116 0.0111 0.0110 0.0117 0.0110 -3.04 -0.079 0.0113 0.0116 0.0117 0.0115 0.0113 0.0110 0.0109 0.0116 0.0108 -2.03 0.020 0.0113 0.0120 0.0118 0.0114 0.0114 0.0112 0.0109 0.0113 0.0108 -1.06 0.117 0.0114 0.0119 0.0121 0.0110 0.0118 0.0109 0.0109 0.0114 0.0111 -0.06 0.222 0.0117 0.0119 0.0122 0.0113 0.0121 0.0116 0.0113 0.0114 0.0117 1.01 0.334 0.0115 0.0116 0.0116 0.0114 0.0115 0.0118 0.0115 0.0112 0.0118 2.07 0.450 0.0118 0.0116 0.0117 0.0119 0.0115 0.0121 0.0118 0.0117 0.0120 3.10 0.553 0.0114 0.0109 0.0115 0.0115 0.0114 0.0121 0.0113 0.0116 0.0111 4.11 0.657 0.0111 0.0103 0.0114 0.0112 0.0112 0.0118 0.0107 0.0111 0.0107 5.15 0.755 0.0107 0.0099 0.0112 0.0111 0.0108 0.0110 0.0104 0.0106 0.0105 6.15 0.840 0.0105 0.0100 0.0108 0.0122 0.0103 0.0106 0.0104 0.0102 0.0099 7.22 0.915 0.0123 0.0117 0.0128 0.0136 0.0131 0.0117 0.0122 0.0117 0.0115 8.12 0.965 0.0154 0.0153 0.0152 0.0162 0.0164 0.0156 0.0155 0.0146 0.0142 9.23 1.008 0.0201 0.0197 0.0191 0.0202 0.0212 0.0205 0.0211 0.0198 0.0188 10.18 1.034 0.0261 0.0274 0.0249 0.0226 0.0245 0.0281 0.0323 0.0264 0.0230 11.19 1.058 0.0344 0.0356 0.0335 0.0280 0.0302 0.0385 0.0434 0.0356 0.0308 12.21 1.080 0.0439 0.0432 0.0412 0.0417 0.0465 0.0505 0.0514 0.0431 0.0341 13.25 1.101 0.0550 0.0556 0.0544 0.0559 0.0617 0.0627 0.0572 0.0502 0.0425 14.23 1.114 0.0696 0.0716 0.0697 0.0714 0.0739 0.0744 0.0719 0.0643 0.0594 Tabulated from data in file bm05023.dat & reduced using program C10.20 Average Reynolds #: 499867 Number of angles of attack: 25 alpha / Cl / Cd / Spanwise Cd's >>> -10.18 -0.696 0.0191 0.0192 0.0186 0.0200 0.0184 0.0180 0.0190 0.0200 0.0195 -9.23 -0.646 0.0164 0.0166 0.0159 0.0173 0.0157 0.0155 0.0163 0.0172 0.0163 -8.21 -0.575 0.0141 0.0140 0.0138 0.0151 0.0136 0.0138 0.0143 0.0142 0.0137 -7.15 -0.480 0.0124 0.0122 0.0125 0.0137 0.0119 0.0122 0.0124 0.0122 0.0121 -6.16 -0.391 0.0113 0.0109 0.0114 0.0126 0.0110 0.0112 0.0110 0.0110 0.0112 -5.17 -0.287 0.0104 0.0101 0.0106 0.0115 0.0104 0.0102 0.0101 0.0103 0.0102 -4.11 -0.185 0.0097 0.0096 0.0099 0.0104 0.0098 0.0093 0.0092 0.0097 0.0094 -3.08 -0.082 0.0093 0.0098 0.0096 0.0096 0.0093 0.0091 0.0088 0.0094 0.0088 -2.05 0.032 0.0091 0.0097 0.0096 0.0090 0.0094 0.0089 0.0087 0.0090 0.0086 -1.03 0.137 0.0090 0.0095 0.0095 0.0085 0.0098 0.0088 0.0089 0.0088 0.0086 0.03 0.246 0.0090 0.0090 0.0094 0.0082 0.0097 0.0092 0.0091 0.0085 0.0090 1.00 0.345 0.0090 0.0086 0.0090 0.0086 0.0091 0.0094 0.0092 0.0086 0.0093 2.00 0.458 0.0089 0.0084 0.0089 0.0091 0.0087 0.0090 0.0093 0.0086 0.0091 3.07 0.576 0.0087 0.0079 0.0089 0.0089 0.0087 0.0090 0.0088 0.0090 0.0086 4.13 0.687 0.0088 0.0082 0.0093 0.0088 0.0087 0.0089 0.0088 0.0087 0.0087 5.09 0.783 0.0090 0.0086 0.0095 0.0094 0.0090 0.0091 0.0090 0.0084 0.0090 6.17 0.871 0.0102 0.0101 0.0105 0.0109 0.0103 0.0104 0.0097 0.0093 0.0103 7.16 0.923 0.0132 0.0133 0.0141 0.0130 0.0135 0.0137 0.0131 0.0118 0.0133 8.19 0.972 0.0164 0.0166 0.0165 0.0166 0.0168 0.0164 0.0168 0.0156 0.0158 9.17 1.008 0.0202 0.0195 0.0194 0.0189 0.0208 0.0213 0.0232 0.0197 0.0190 10.19 1.042 0.0263 0.0275 0.0253 0.0226 0.0239 0.0283 0.0346 0.0263 0.0222 11.19 1.075 0.0350 0.0372 0.0338 0.0304 0.0282 0.0360 0.0463 0.0379 0.0303 12.22 1.105 0.0448 0.0466 0.0440 0.0441 0.0493 0.0527 0.0475 0.0401 0.0342 13.23 1.129 0.0571 0.0605 0.0600 0.0605 0.0621 0.0655 0.0594 0.0475 0.0411 14.23 1.142 0.0751 0.0767 0.0773 0.0801 0.0831 0.0843 0.0772 0.0674 0.0550 Tabulated from data in file bm05025.dat & reduced using program C10.20 File S822_c.drg created using program C10.20 on Thu May 22 17:01:35 2003