Airfoil: S822 (B) 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 #: 99847 Number of angles of attack: 25 alpha / Cl / Cd / Spanwise Cd's >>> -10.24 -0.800 0.0373 0.0387 0.0371 0.0377 0.0358 0.0360 0.0372 0.0374 0.0383 -9.25 -0.797 0.0309 0.0328 0.0329 0.0305 0.0282 0.0311 0.0302 0.0302 0.0314 -8.29 -0.747 0.0278 0.0281 0.0273 0.0268 0.0271 0.0275 0.0279 0.0277 0.0300 -7.23 -0.671 0.0253 0.0256 0.0260 0.0245 0.0254 0.0254 0.0243 0.0251 0.0261 -6.24 -0.598 0.0243 0.0248 0.0256 0.0230 0.0243 0.0239 0.0245 0.0242 0.0238 -5.19 -0.490 0.0232 0.0233 0.0223 0.0235 0.0237 0.0223 0.0233 0.0231 0.0238 -4.20 -0.398 0.0225 0.0239 0.0231 0.0221 0.0214 0.0222 0.0217 0.0221 0.0233 -3.16 -0.301 0.0253 0.0264 0.0272 0.0273 0.0235 0.0233 0.0247 0.0248 0.0252 -2.13 -0.225 0.0275 0.0262 0.0251 0.0249 0.0266 0.0302 0.0283 0.0280 0.0310 -1.12 -0.174 0.0304 0.0330 0.0307 0.0298 0.0294 0.0299 0.0299 0.0295 0.0314 -0.10 -0.114 0.0297 0.0314 0.0304 0.0294 0.0284 0.0291 0.0290 0.0298 0.0296 0.91 -0.048 0.0334 0.0341 0.0356 0.0338 0.0326 0.0330 0.0323 0.0328 0.0328 1.94 0.030 0.0353 0.0372 0.0363 0.0355 0.0347 0.0351 0.0339 0.0347 0.0351 2.98 0.132 0.0414 0.0432 0.0416 0.0423 0.0415 0.0410 0.0406 0.0400 0.0407 3.97 0.269 0.0416 0.0421 0.0410 0.0408 0.0419 0.0428 0.0418 0.0411 0.0415 5.12 0.692 0.0283 0.0279 0.0294 0.0288 0.0293 0.0284 0.0269 0.0273 0.0283 6.18 0.837 0.0199 0.0204 0.0214 0.0204 0.0202 0.0189 0.0213 0.0172 0.0192 7.19 0.900 0.0191 0.0191 0.0197 0.0197 0.0195 0.0183 0.0203 0.0178 0.0184 8.23 0.942 0.0229 0.0219 0.0226 0.0240 0.0248 0.0234 0.0229 0.0207 0.0226 9.13 0.953 0.0288 0.0266 0.0289 0.0310 0.0305 0.0303 0.0293 0.0267 0.0273 10.16 0.993 0.0328 0.0300 0.0315 0.0341 0.0332 0.0350 0.0350 0.0328 0.0308 11.15 1.045 0.0401 0.0368 0.0403 0.0432 0.0438 0.0417 0.0406 0.0380 0.0369 12.20 1.067 0.0501 0.0492 0.0523 0.0542 0.0505 0.0497 0.0505 0.0493 0.0448 13.20 1.082 0.0633 0.0602 0.0655 0.0717 0.0705 0.0657 0.0610 0.0575 0.0545 14.22 1.085 0.0800 0.0828 0.0860 0.0878 0.0890 0.0831 0.0758 0.0684 0.0667 Tabulated from data in file bm05027.dat & reduced using program C10.20 Average Reynolds #: 150122 Number of angles of attack: 25 alpha / Cl / Cd / Spanwise Cd's >>> -10.33 -0.855 0.0320 0.0342 0.0334 0.0338 0.0320 0.0307 0.0305 0.0310 0.0303 -9.27 -0.823 0.0281 0.0312 0.0292 0.0291 0.0266 0.0264 0.0265 0.0282 0.0275 -8.24 -0.741 0.0253 0.0257 0.0252 0.0262 0.0253 0.0245 0.0253 0.0252 0.0248 -7.23 -0.638 0.0243 0.0248 0.0245 0.0253 0.0247 0.0232 0.0233 0.0243 0.0239 -6.27 -0.546 0.0232 0.0234 0.0233 0.0235 0.0229 0.0230 0.0234 0.0230 0.0229 -5.18 -0.436 0.0222 0.0227 0.0220 0.0235 0.0216 0.0215 0.0221 0.0223 0.0219 -4.16 -0.330 0.0224 0.0228 0.0229 0.0235 0.0221 0.0219 0.0222 0.0219 0.0216 -3.13 -0.237 0.0231 0.0238 0.0238 0.0239 0.0222 0.0229 0.0226 0.0226 0.0225 -2.08 -0.140 0.0249 0.0255 0.0251 0.0253 0.0261 0.0236 0.0251 0.0242 0.0245 -1.10 -0.063 0.0270 0.0272 0.0274 0.0274 0.0280 0.0262 0.0271 0.0261 0.0271 -0.07 0.037 0.0286 0.0299 0.0289 0.0292 0.0280 0.0280 0.0284 0.0278 0.0286 1.02 0.242 0.0240 0.0251 0.0251 0.0242 0.0242 0.0235 0.0238 0.0216 0.0246 2.03 0.349 0.0190 0.0230 0.0234 0.0183 0.0169 0.0149 0.0184 0.0153 0.0218 3.07 0.449 0.0164 0.0172 0.0200 0.0154 0.0159 0.0144 0.0178 0.0136 0.0171 4.08 0.569 0.0154 0.0150 0.0166 0.0141 0.0167 0.0169 0.0154 0.0139 0.0143 5.13 0.709 0.0171 0.0151 0.0196 0.0185 0.0178 0.0180 0.0150 0.0170 0.0155 6.11 0.713 0.0188 0.0184 0.0192 0.0195 0.0205 0.0207 0.0181 0.0173 0.0168 7.12 0.772 0.0213 0.0202 0.0213 0.0219 0.0228 0.0224 0.0208 0.0205 0.0209 8.13 0.845 0.0245 0.0238 0.0241 0.0247 0.0266 0.0256 0.0239 0.0236 0.0237 9.21 0.908 0.0276 0.0261 0.0269 0.0288 0.0296 0.0281 0.0282 0.0268 0.0264 10.15 0.971 0.0312 0.0295 0.0303 0.0339 0.0340 0.0320 0.0309 0.0298 0.0295 11.21 1.027 0.0383 0.0353 0.0379 0.0428 0.0439 0.0400 0.0371 0.0349 0.0343 12.23 1.044 0.0488 0.0428 0.0475 0.0547 0.0608 0.0516 0.0467 0.0443 0.0419 13.26 1.056 0.0606 0.0574 0.0622 0.0691 0.0714 0.0669 0.0580 0.0504 0.0494 14.19 1.064 0.0773 0.0778 0.0804 0.0842 0.0840 0.0805 0.0745 0.0691 0.0675 Tabulated from data in file bm05029.dat & reduced using program C10.20 Average Reynolds #: 200042 Number of angles of attack: 24 alpha / Cl / Cd / Spanwise Cd's >>> -10.24 -0.810 0.0285 0.0280 0.0279 0.0282 0.0271 0.0275 0.0287 0.0297 0.0311 -9.30 -0.733 0.0245 0.0259 0.0243 0.0253 0.0241 0.0235 0.0242 0.0240 0.0248 -8.20 -0.623 0.0222 0.0226 0.0218 0.0234 0.0219 0.0215 0.0217 0.0224 0.0223 -7.18 -0.517 0.0212 0.0212 0.0215 0.0225 0.0208 0.0207 0.0210 0.0209 0.0209 -6.18 -0.409 0.0207 0.0209 0.0210 0.0219 0.0203 0.0206 0.0205 0.0204 0.0202 -5.14 -0.305 0.0207 0.0213 0.0210 0.0218 0.0204 0.0202 0.0206 0.0204 0.0197 -4.10 -0.202 0.0209 0.0216 0.0215 0.0215 0.0209 0.0205 0.0206 0.0206 0.0202 -3.12 -0.111 0.0210 0.0217 0.0217 0.0211 0.0208 0.0204 0.0207 0.0211 0.0204 -2.07 -0.018 0.0216 0.0226 0.0224 0.0214 0.0215 0.0216 0.0213 0.0209 0.0214 -1.04 0.089 0.0187 0.0225 0.0220 0.0184 0.0180 0.0173 0.0166 0.0143 0.0203 -0.02 0.206 0.0145 0.0134 0.0197 0.0136 0.0134 0.0121 0.0163 0.0117 0.0156 1.01 0.294 0.0128 0.0131 0.0144 0.0122 0.0124 0.0127 0.0138 0.0116 0.0126 2.04 0.353 0.0149 0.0150 0.0147 0.0145 0.0175 0.0131 0.0198 0.0120 0.0127 3.04 0.416 0.0160 0.0149 0.0152 0.0135 0.0199 0.0144 0.0209 0.0127 0.0163 4.05 0.480 0.0166 0.0143 0.0153 0.0178 0.0176 0.0167 0.0189 0.0172 0.0152 5.07 0.589 0.0182 0.0162 0.0167 0.0209 0.0201 0.0202 0.0157 0.0194 0.0163 6.10 0.661 0.0192 0.0185 0.0194 0.0191 0.0196 0.0204 0.0188 0.0188 0.0188 7.12 0.749 0.0211 0.0206 0.0210 0.0212 0.0221 0.0227 0.0208 0.0203 0.0205 8.15 0.830 0.0239 0.0229 0.0235 0.0244 0.0261 0.0252 0.0238 0.0231 0.0225 9.17 0.900 0.0266 0.0250 0.0260 0.0271 0.0292 0.0284 0.0270 0.0255 0.0248 10.15 0.964 0.0298 0.0268 0.0283 0.0323 0.0359 0.0310 0.0288 0.0275 0.0275 11.21 1.022 0.0361 0.0336 0.0343 0.0371 0.0402 0.0389 0.0380 0.0347 0.0324 12.20 1.048 0.0462 0.0439 0.0450 0.0452 0.0471 0.0509 0.0525 0.0455 0.0399 13.21 1.060 0.0583 0.0537 0.0594 0.0673 0.0701 0.0655 0.0558 0.0476 0.0467 Tabulated from data in file bm05031.dat & reduced using program C10.20 Average Reynolds #: 350505 Number of angles of attack: 24 alpha / Cl / Cd / Spanwise Cd's >>> -10.24 -0.651 0.0224 0.0218 0.0220 0.0242 0.0212 0.0211 0.0224 0.0233 0.0236 -9.20 -0.610 0.0180 0.0185 0.0178 0.0191 0.0171 0.0174 0.0176 0.0183 0.0180 -8.20 -0.531 0.0169 0.0168 0.0172 0.0183 0.0161 0.0167 0.0170 0.0169 0.0164 -7.18 -0.448 0.0164 0.0162 0.0167 0.0178 0.0158 0.0164 0.0161 0.0159 0.0159 -6.18 -0.355 0.0155 0.0153 0.0160 0.0167 0.0152 0.0154 0.0152 0.0153 0.0152 -5.10 -0.251 0.0151 0.0151 0.0157 0.0160 0.0152 0.0146 0.0146 0.0149 0.0146 -4.11 -0.159 0.0143 0.0144 0.0159 0.0145 0.0146 0.0119 0.0156 0.0130 0.0147 -3.06 -0.074 0.0137 0.0124 0.0162 0.0136 0.0141 0.0131 0.0124 0.0146 0.0129 -2.07 -0.007 0.0144 0.0139 0.0147 0.0147 0.0152 0.0141 0.0136 0.0150 0.0144 -1.02 0.084 0.0148 0.0152 0.0156 0.0143 0.0152 0.0147 0.0141 0.0147 0.0145 -0.04 0.180 0.0150 0.0153 0.0153 0.0144 0.0157 0.0151 0.0145 0.0147 0.0150 0.98 0.269 0.0154 0.0154 0.0154 0.0150 0.0158 0.0156 0.0153 0.0152 0.0154 2.01 0.361 0.0159 0.0156 0.0157 0.0158 0.0158 0.0163 0.0162 0.0156 0.0159 3.07 0.456 0.0164 0.0158 0.0162 0.0165 0.0161 0.0169 0.0166 0.0161 0.0166 4.12 0.550 0.0175 0.0169 0.0174 0.0175 0.0178 0.0181 0.0175 0.0171 0.0174 5.10 0.632 0.0184 0.0176 0.0185 0.0185 0.0188 0.0199 0.0181 0.0178 0.0182 6.10 0.714 0.0188 0.0187 0.0187 0.0186 0.0192 0.0206 0.0185 0.0180 0.0186 7.14 0.790 0.0200 0.0200 0.0200 0.0206 0.0205 0.0221 0.0201 0.0191 0.0177 8.13 0.854 0.0221 0.0210 0.0219 0.0221 0.0243 0.0245 0.0213 0.0205 0.0210 9.18 0.921 0.0251 0.0234 0.0241 0.0247 0.0289 0.0297 0.0248 0.0227 0.0223 10.20 0.986 0.0282 0.0246 0.0256 0.0285 0.0357 0.0343 0.0287 0.0248 0.0235 11.16 1.048 0.0326 0.0309 0.0302 0.0323 0.0369 0.0387 0.0356 0.0289 0.0275 12.22 1.095 0.0402 0.0372 0.0332 0.0363 0.0460 0.0473 0.0441 0.0396 0.0379 13.25 1.126 0.0543 0.0454 0.0498 0.0616 0.0743 0.0704 0.0552 0.0409 0.0371 Tabulated from data in file bm05033.dat & reduced using program C10.20 Average Reynolds #: 499806 Number of angles of attack: 24 alpha / Cl / Cd / Spanwise Cd's >>> -10.25 -0.666 0.0214 0.0213 0.0215 0.0228 0.0208 0.0202 0.0212 0.0220 0.0217 -9.22 -0.620 0.0178 0.0179 0.0171 0.0188 0.0165 0.0164 0.0179 0.0190 0.0184 -8.17 -0.549 0.0155 0.0156 0.0157 0.0167 0.0149 0.0155 0.0156 0.0154 0.0150 -7.14 -0.452 0.0146 0.0143 0.0151 0.0160 0.0141 0.0146 0.0145 0.0142 0.0142 -6.23 -0.365 0.0141 0.0137 0.0146 0.0153 0.0135 0.0140 0.0137 0.0138 0.0138 -5.14 -0.267 0.0131 0.0125 0.0145 0.0131 0.0136 0.0124 0.0126 0.0127 0.0132 -4.12 -0.187 0.0134 0.0129 0.0141 0.0144 0.0138 0.0126 0.0124 0.0139 0.0132 -3.09 -0.097 0.0136 0.0140 0.0144 0.0141 0.0136 0.0132 0.0125 0.0137 0.0132 -2.03 0.001 0.0137 0.0143 0.0144 0.0136 0.0140 0.0133 0.0128 0.0142 0.0131 -1.06 0.087 0.0140 0.0145 0.0146 0.0137 0.0147 0.0136 0.0135 0.0142 0.0135 -0.03 0.184 0.0143 0.0144 0.0146 0.0138 0.0151 0.0142 0.0141 0.0142 0.0141 1.04 0.281 0.0148 0.0148 0.0147 0.0142 0.0152 0.0150 0.0149 0.0148 0.0148 2.00 0.369 0.0150 0.0151 0.0147 0.0145 0.0147 0.0149 0.0153 0.0142 0.0164 3.06 0.446 0.0156 0.0158 0.0157 0.0153 0.0162 0.0159 0.0154 0.0161 0.0148 4.06 0.523 0.0166 0.0166 0.0162 0.0160 0.0175 0.0170 0.0163 0.0170 0.0159 5.17 0.605 0.0178 0.0171 0.0174 0.0170 0.0194 0.0185 0.0175 0.0181 0.0172 6.10 0.686 0.0188 0.0183 0.0178 0.0180 0.0214 0.0194 0.0183 0.0189 0.0183 7.18 0.760 0.0211 0.0199 0.0191 0.0202 0.0250 0.0228 0.0204 0.0205 0.0204 8.15 0.879 0.0233 0.0215 0.0225 0.0223 0.0251 0.0298 0.0225 0.0210 0.0217 9.20 0.933 0.0246 0.0219 0.0239 0.0240 0.0278 0.0312 0.0239 0.0222 0.0218 10.15 0.993 0.0278 0.0249 0.0251 0.0262 0.0327 0.0347 0.0289 0.0246 0.0250 11.19 1.051 0.0351 0.0305 0.0305 0.0348 0.0450 0.0455 0.0357 0.0300 0.0291 12.25 1.085 0.0477 0.0370 0.0399 0.0537 0.0683 0.0660 0.0506 0.0348 0.0316 13.19 1.096 0.0664 0.0592 0.0683 0.0786 0.0850 0.0793 0.0688 0.0513 0.0405 Tabulated from data in file bm05035.dat & reduced using program C10.20 File s822_tf.drg created using program C10.20 on Thu May 22 17:01:35 2003