Airfoil: S834 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 #: 100159 Number of angles of attack: 24 alpha / Cl / Cd / Spanwise Cd's >>> -10.18 -0.830 0.0361 0.0382 0.0373 0.0374 0.0353 0.0349 0.0348 0.0355 0.0353 -9.17 -0.828 0.0313 0.0315 0.0321 0.0325 0.0308 0.0300 0.0314 0.0308 0.0313 -8.19 -0.798 0.0272 0.0278 0.0270 0.0280 0.0268 0.0261 0.0266 0.0273 0.0281 -7.20 -0.742 0.0248 0.0261 0.0246 0.0260 0.0240 0.0236 0.0240 0.0250 0.0252 -6.11 -0.641 0.0224 0.0225 0.0221 0.0224 0.0225 0.0215 0.0223 0.0219 0.0243 -5.16 -0.535 0.0221 0.0255 0.0237 0.0185 0.0230 0.0201 0.0189 0.0241 0.0233 -4.11 -0.420 0.0219 0.0266 0.0201 0.0204 0.0243 0.0198 0.0172 0.0232 0.0238 -3.04 -0.307 0.0208 0.0221 0.0189 0.0209 0.0237 0.0212 0.0190 0.0212 0.0196 -2.06 -0.231 0.0217 0.0241 0.0213 0.0206 0.0217 0.0212 0.0191 0.0203 0.0252 -1.04 -0.186 0.0235 0.0236 0.0216 0.0234 0.0236 0.0245 0.0248 0.0242 0.0221 -0.05 -0.121 0.0247 0.0283 0.0257 0.0227 0.0234 0.0244 0.0240 0.0221 0.0266 1.05 -0.020 0.0276 0.0269 0.0274 0.0279 0.0253 0.0282 0.0296 0.0290 0.0268 2.02 0.061 0.0318 0.0328 0.0317 0.0324 0.0319 0.0317 0.0307 0.0311 0.0319 3.06 0.191 0.0340 0.0347 0.0330 0.0332 0.0345 0.0335 0.0344 0.0340 0.0344 4.16 0.564 0.0230 0.0231 0.0237 0.0226 0.0235 0.0231 0.0226 0.0224 0.0229 5.17 0.665 0.0179 0.0184 0.0211 0.0171 0.0160 0.0169 0.0179 0.0164 0.0197 6.20 0.723 0.0174 0.0160 0.0196 0.0168 0.0172 0.0176 0.0178 0.0166 0.0173 7.22 0.760 0.0195 0.0186 0.0199 0.0194 0.0211 0.0197 0.0195 0.0180 0.0199 8.17 0.786 0.0237 0.0245 0.0240 0.0236 0.0247 0.0242 0.0231 0.0224 0.0229 9.23 0.838 0.0286 0.0281 0.0284 0.0295 0.0290 0.0298 0.0285 0.0280 0.0272 10.23 0.908 0.0337 0.0326 0.0336 0.0337 0.0343 0.0347 0.0347 0.0333 0.0327 11.26 0.963 0.0400 0.0371 0.0374 0.0386 0.0411 0.0404 0.0426 0.0431 0.0397 12.31 0.982 0.0537 0.0459 0.0480 0.0513 0.0576 0.0608 0.0615 0.0548 0.0500 13.26 0.984 0.0701 0.0564 0.0616 0.0681 0.0747 0.0819 0.0821 0.0722 0.0641 Tabulated from data in file bm05047.dat & reduced using program C10.20 Average Reynolds #: 150195 Number of angles of attack: 24 alpha / Cl / Cd / Spanwise Cd's >>> -10.19 -0.798 0.0304 0.0314 0.0306 0.0314 0.0300 0.0299 0.0304 0.0291 0.0302 -9.22 -0.786 0.0266 0.0283 0.0252 0.0271 0.0261 0.0252 0.0271 0.0280 0.0262 -8.18 -0.741 0.0237 0.0246 0.0231 0.0243 0.0238 0.0229 0.0232 0.0240 0.0240 -7.18 -0.665 0.0226 0.0225 0.0221 0.0229 0.0221 0.0221 0.0215 0.0215 0.0257 -6.15 -0.575 0.0211 0.0228 0.0227 0.0185 0.0193 0.0206 0.0239 0.0210 0.0199 -5.13 -0.469 0.0211 0.0202 0.0206 0.0200 0.0219 0.0220 0.0196 0.0207 0.0235 -4.08 -0.352 0.0201 0.0206 0.0201 0.0214 0.0200 0.0197 0.0209 0.0193 0.0192 -3.05 -0.250 0.0203 0.0218 0.0213 0.0205 0.0196 0.0196 0.0200 0.0210 0.0186 -2.02 -0.144 0.0211 0.0223 0.0216 0.0213 0.0212 0.0205 0.0207 0.0207 0.0209 -1.01 -0.049 0.0227 0.0234 0.0231 0.0228 0.0230 0.0221 0.0227 0.0228 0.0217 0.01 0.090 0.0232 0.0238 0.0235 0.0236 0.0232 0.0232 0.0232 0.0228 0.0227 1.08 0.262 0.0195 0.0205 0.0203 0.0192 0.0192 0.0192 0.0191 0.0180 0.0209 2.07 0.367 0.0156 0.0173 0.0173 0.0145 0.0148 0.0140 0.0150 0.0125 0.0197 3.13 0.509 0.0143 0.0131 0.0145 0.0137 0.0152 0.0155 0.0140 0.0128 0.0158 4.16 0.654 0.0158 0.0146 0.0169 0.0153 0.0167 0.0168 0.0138 0.0168 0.0152 5.15 0.663 0.0174 0.0169 0.0173 0.0173 0.0181 0.0184 0.0170 0.0174 0.0170 6.21 0.701 0.0191 0.0185 0.0190 0.0191 0.0202 0.0204 0.0186 0.0185 0.0187 7.23 0.780 0.0210 0.0206 0.0208 0.0210 0.0219 0.0223 0.0208 0.0204 0.0205 8.20 0.862 0.0235 0.0224 0.0232 0.0241 0.0249 0.0242 0.0233 0.0233 0.0227 9.25 0.936 0.0267 0.0256 0.0266 0.0273 0.0276 0.0273 0.0269 0.0264 0.0255 10.25 1.002 0.0307 0.0301 0.0303 0.0312 0.0320 0.0313 0.0319 0.0305 0.0288 11.25 1.054 0.0367 0.0332 0.0343 0.0353 0.0381 0.0393 0.0402 0.0379 0.0353 12.24 1.069 0.0507 0.0375 0.0387 0.0438 0.0538 0.0639 0.0683 0.0558 0.0438 13.28 1.071 0.0676 0.0466 0.0538 0.0652 0.0788 0.0879 0.0831 0.0687 0.0566 Tabulated from data in file bm05049.dat & reduced using program C10.20 Average Reynolds #: 199613 Number of angles of attack: 24 alpha / Cl / Cd / Spanwise Cd's >>> -10.21 -0.862 0.0268 0.0269 0.0273 0.0285 0.0271 0.0260 0.0262 0.0262 0.0259 -9.17 -0.843 0.0240 0.0246 0.0239 0.0245 0.0243 0.0230 0.0239 0.0239 0.0236 -8.21 -0.787 0.0218 0.0222 0.0215 0.0225 0.0219 0.0205 0.0218 0.0226 0.0216 -7.18 -0.700 0.0212 0.0216 0.0203 0.0229 0.0209 0.0207 0.0211 0.0212 0.0210 -6.18 -0.589 0.0209 0.0217 0.0206 0.0216 0.0209 0.0206 0.0207 0.0203 0.0204 -5.09 -0.458 0.0209 0.0208 0.0214 0.0217 0.0211 0.0204 0.0204 0.0208 0.0205 -4.06 -0.329 0.0212 0.0212 0.0214 0.0224 0.0210 0.0211 0.0211 0.0209 0.0207 -3.01 -0.202 0.0212 0.0214 0.0220 0.0219 0.0212 0.0211 0.0210 0.0209 0.0204 -2.03 -0.091 0.0216 0.0222 0.0223 0.0219 0.0216 0.0211 0.0213 0.0215 0.0206 -0.97 0.054 0.0202 0.0219 0.0213 0.0204 0.0199 0.0202 0.0193 0.0168 0.0221 0.06 0.219 0.0137 0.0120 0.0181 0.0129 0.0137 0.0121 0.0139 0.0108 0.0161 1.07 0.299 0.0122 0.0122 0.0128 0.0110 0.0128 0.0124 0.0121 0.0121 0.0118 2.10 0.350 0.0144 0.0132 0.0134 0.0133 0.0167 0.0131 0.0208 0.0128 0.0117 3.14 0.405 0.0154 0.0149 0.0135 0.0143 0.0173 0.0157 0.0158 0.0155 0.0158 4.14 0.530 0.0165 0.0160 0.0157 0.0185 0.0174 0.0184 0.0151 0.0153 0.0153 5.16 0.618 0.0170 0.0165 0.0171 0.0172 0.0173 0.0180 0.0163 0.0171 0.0168 6.17 0.677 0.0185 0.0179 0.0185 0.0188 0.0191 0.0197 0.0179 0.0180 0.0181 7.17 0.767 0.0203 0.0199 0.0204 0.0206 0.0210 0.0212 0.0199 0.0198 0.0196 8.20 0.847 0.0225 0.0219 0.0220 0.0226 0.0235 0.0234 0.0227 0.0218 0.0218 9.22 0.926 0.0252 0.0245 0.0242 0.0255 0.0267 0.0261 0.0255 0.0247 0.0242 10.22 0.992 0.0285 0.0275 0.0278 0.0287 0.0298 0.0291 0.0302 0.0284 0.0268 11.28 1.048 0.0339 0.0320 0.0325 0.0339 0.0332 0.0339 0.0380 0.0355 0.0320 12.30 1.082 0.0432 0.0362 0.0346 0.0365 0.0486 0.0564 0.0520 0.0432 0.0385 13.27 1.092 0.0622 0.0364 0.0417 0.0534 0.0682 0.0843 0.0859 0.0717 0.0558 Tabulated from data in file bm05051.dat & reduced using program C10.20 Average Reynolds #: 350082 Number of angles of attack: 24 alpha / Cl / Cd / Spanwise Cd's >>> -10.20 -0.855 0.0256 0.0264 0.0259 0.0267 0.0254 0.0248 0.0247 0.0258 0.0251 -9.24 -0.798 0.0214 0.0219 0.0217 0.0224 0.0220 0.0205 0.0208 0.0213 0.0207 -8.18 -0.670 0.0192 0.0195 0.0190 0.0200 0.0193 0.0185 0.0190 0.0194 0.0188 -7.16 -0.540 0.0182 0.0182 0.0182 0.0195 0.0179 0.0180 0.0179 0.0180 0.0179 -6.11 -0.407 0.0175 0.0173 0.0179 0.0187 0.0172 0.0174 0.0170 0.0173 0.0174 -5.10 -0.282 0.0165 0.0164 0.0170 0.0175 0.0165 0.0163 0.0161 0.0165 0.0160 -4.04 -0.159 0.0154 0.0158 0.0163 0.0164 0.0159 0.0153 0.0156 0.0130 0.0145 -3.00 -0.063 0.0134 0.0139 0.0160 0.0121 0.0136 0.0124 0.0140 0.0122 0.0134 -2.02 0.008 0.0131 0.0128 0.0136 0.0129 0.0143 0.0123 0.0118 0.0140 0.0127 -1.06 0.073 0.0146 0.0154 0.0151 0.0144 0.0144 0.0143 0.0142 0.0147 0.0141 0.03 0.175 0.0146 0.0147 0.0149 0.0139 0.0156 0.0144 0.0142 0.0142 0.0145 1.08 0.262 0.0151 0.0150 0.0151 0.0146 0.0156 0.0152 0.0152 0.0149 0.0151 2.12 0.359 0.0153 0.0151 0.0151 0.0152 0.0153 0.0157 0.0156 0.0152 0.0154 3.11 0.452 0.0159 0.0155 0.0159 0.0160 0.0156 0.0165 0.0162 0.0156 0.0160 4.17 0.546 0.0167 0.0161 0.0166 0.0167 0.0168 0.0174 0.0168 0.0164 0.0167 5.17 0.634 0.0176 0.0170 0.0175 0.0175 0.0180 0.0188 0.0175 0.0169 0.0175 6.20 0.718 0.0180 0.0175 0.0180 0.0181 0.0179 0.0199 0.0179 0.0173 0.0171 7.26 0.777 0.0185 0.0186 0.0173 0.0191 0.0191 0.0195 0.0193 0.0171 0.0181 8.22 0.850 0.0204 0.0199 0.0197 0.0205 0.0211 0.0220 0.0200 0.0196 0.0201 9.26 0.928 0.0230 0.0226 0.0225 0.0227 0.0244 0.0240 0.0232 0.0222 0.0222 10.26 1.001 0.0258 0.0249 0.0251 0.0258 0.0281 0.0264 0.0274 0.0248 0.0240 11.28 1.041 0.0379 0.0248 0.0251 0.0320 0.0501 0.0596 0.0480 0.0343 0.0288 12.30 1.051 0.0573 0.0296 0.0406 0.0605 0.0767 0.0854 0.0715 0.0551 0.0390 13.25 1.043 0.0845 0.0474 0.0684 0.0860 0.1047 0.1140 0.1046 0.0857 0.0650 Tabulated from data in file bm05053.dat & reduced using program C10.20 Average Reynolds #: 499211 Number of angles of attack: 24 alpha / Cl / Cd / Spanwise Cd's >>> -10.13 -0.794 0.0226 0.0231 0.0225 0.0244 0.0228 0.0221 0.0216 0.0226 0.0220 -9.14 -0.695 0.0189 0.0189 0.0191 0.0206 0.0190 0.0183 0.0183 0.0188 0.0180 -8.13 -0.571 0.0166 0.0166 0.0165 0.0181 0.0161 0.0164 0.0165 0.0166 0.0162 -7.09 -0.454 0.0155 0.0152 0.0155 0.0170 0.0149 0.0155 0.0153 0.0154 0.0152 -6.10 -0.356 0.0147 0.0143 0.0150 0.0160 0.0143 0.0147 0.0146 0.0146 0.0142 -5.03 -0.261 0.0134 0.0132 0.0148 0.0129 0.0132 0.0121 0.0133 0.0138 0.0135 -4.01 -0.180 0.0125 0.0126 0.0123 0.0119 0.0131 0.0122 0.0122 0.0137 0.0122 -3.01 -0.103 0.0131 0.0133 0.0139 0.0138 0.0135 0.0124 0.0120 0.0136 0.0127 -2.08 -0.021 0.0134 0.0138 0.0141 0.0138 0.0136 0.0130 0.0126 0.0140 0.0127 -0.93 0.083 0.0137 0.0140 0.0143 0.0134 0.0144 0.0136 0.0132 0.0139 0.0132 0.01 0.172 0.0140 0.0141 0.0144 0.0134 0.0148 0.0139 0.0137 0.0139 0.0137 1.03 0.271 0.0144 0.0143 0.0143 0.0141 0.0150 0.0147 0.0144 0.0142 0.0143 2.12 0.366 0.0146 0.0144 0.0145 0.0144 0.0146 0.0151 0.0150 0.0145 0.0148 3.09 0.457 0.0152 0.0148 0.0149 0.0154 0.0149 0.0156 0.0155 0.0149 0.0155 4.13 0.554 0.0159 0.0154 0.0158 0.0158 0.0156 0.0167 0.0161 0.0155 0.0161 5.11 0.640 0.0166 0.0161 0.0165 0.0164 0.0167 0.0176 0.0164 0.0163 0.0168 6.19 0.734 0.0178 0.0172 0.0175 0.0177 0.0181 0.0194 0.0176 0.0169 0.0180 7.21 0.818 0.0193 0.0188 0.0186 0.0194 0.0198 0.0212 0.0191 0.0179 0.0196 8.23 0.899 0.0202 0.0196 0.0198 0.0205 0.0213 0.0223 0.0200 0.0191 0.0189 9.27 0.960 0.0221 0.0216 0.0214 0.0215 0.0233 0.0234 0.0227 0.0213 0.0216 10.24 1.018 0.0266 0.0221 0.0224 0.0237 0.0314 0.0365 0.0301 0.0238 0.0226 11.25 1.049 0.0367 0.0248 0.0261 0.0322 0.0440 0.0497 0.0465 0.0379 0.0323 12.29 1.060 0.0504 0.0321 0.0334 0.0435 0.0602 0.0708 0.0658 0.0559 0.0417 13.26 1.060 0.0800 0.0401 0.0554 0.0738 0.0879 0.1012 0.1056 0.0966 0.0797 Tabulated from data in file bm05055.dat & reduced using program C10.20 File s834_tf.drg created using program C10.20 on Thu May 22 17:01:35 2003