Airfoil: S834 Builder: Y. Tinel Comment: 'clean' Number of Reynolds #'s: 5 Average Reynolds #: 99982 Number of angles of attack: 23 alpha / Cl / Cd / Spanwise Cd's >>> -10.13 -0.763 0.0364 0.0385 0.0375 0.0381 0.0358 0.0355 0.0350 0.0351 0.0361 -9.15 -0.762 0.0317 0.0337 0.0332 0.0329 0.0311 0.0301 0.0311 0.0308 0.0312 -8.21 -0.732 0.0278 0.0297 0.0291 0.0285 0.0267 0.0268 0.0270 0.0274 0.0276 -7.16 -0.680 0.0245 0.0264 0.0249 0.0251 0.0234 0.0227 0.0244 0.0244 0.0246 -6.14 -0.595 0.0225 0.0242 0.0218 0.0211 0.0253 0.0223 0.0215 0.0214 0.0223 -5.16 -0.503 0.0212 0.0240 0.0188 0.0207 0.0233 0.0202 0.0205 0.0202 0.0221 -4.14 -0.406 0.0221 0.0275 0.0193 0.0184 0.0237 0.0225 0.0195 0.0212 0.0248 -3.10 -0.317 0.0232 0.0264 0.0202 0.0205 0.0243 0.0217 0.0210 0.0230 0.0282 -2.07 -0.241 0.0248 0.0285 0.0244 0.0230 0.0242 0.0245 0.0229 0.0221 0.0287 -1.07 -0.221 0.0241 0.0240 0.0234 0.0256 0.0237 0.0238 0.0262 0.0248 0.0214 -0.02 -0.115 0.0242 0.0235 0.0218 0.0236 0.0229 0.0233 0.0247 0.0261 0.0275 1.01 -0.009 0.0291 0.0305 0.0310 0.0296 0.0273 0.0264 0.0288 0.0298 0.0294 2.02 0.073 0.0312 0.0320 0.0315 0.0315 0.0313 0.0316 0.0307 0.0304 0.0310 3.04 0.168 0.0354 0.0364 0.0349 0.0351 0.0364 0.0348 0.0354 0.0350 0.0354 4.09 0.295 0.0403 0.0406 0.0403 0.0402 0.0404 0.0411 0.0404 0.0396 0.0397 5.12 0.467 0.0388 0.0390 0.0390 0.0399 0.0400 0.0400 0.0372 0.0368 0.0387 6.17 0.795 0.0227 0.0230 0.0231 0.0219 0.0232 0.0223 0.0222 0.0232 0.0229 7.21 0.891 0.0188 0.0183 0.0188 0.0182 0.0178 0.0197 0.0193 0.0187 0.0197 8.28 0.969 0.0205 0.0192 0.0216 0.0201 0.0217 0.0200 0.0220 0.0201 0.0191 9.28 1.013 0.0261 0.0254 0.0253 0.0268 0.0270 0.0263 0.0250 0.0286 0.0242 10.26 1.030 0.0329 0.0322 0.0321 0.0327 0.0339 0.0351 0.0329 0.0322 0.0324 11.22 1.049 0.0405 0.0363 0.0371 0.0391 0.0424 0.0432 0.0439 0.0436 0.0386 12.27 1.063 0.0534 0.0444 0.0480 0.0507 0.0570 0.0620 0.0604 0.0547 0.0502 Tabulated from data in file bm05037.dat & reduced using program C10.20 Average Reynolds #: 149734 Number of angles of attack: 24 alpha / Cl / Cd / Spanwise Cd's >>> -10.21 -0.818 0.0313 0.0324 0.0319 0.0321 0.0308 0.0300 0.0309 0.0310 0.0316 -9.17 -0.817 0.0276 0.0282 0.0278 0.0283 0.0273 0.0264 0.0272 0.0276 0.0275 -8.18 -0.780 0.0240 0.0251 0.0234 0.0247 0.0242 0.0225 0.0248 0.0238 0.0234 -7.21 -0.721 0.0220 0.0220 0.0216 0.0218 0.0212 0.0217 0.0219 0.0218 0.0238 -6.17 -0.622 0.0197 0.0201 0.0201 0.0193 0.0212 0.0182 0.0196 0.0187 0.0206 -5.16 -0.503 0.0189 0.0230 0.0189 0.0156 0.0181 0.0188 0.0214 0.0176 0.0181 -4.06 -0.391 0.0196 0.0201 0.0203 0.0186 0.0238 0.0192 0.0158 0.0179 0.0211 -3.05 -0.299 0.0194 0.0207 0.0198 0.0197 0.0191 0.0182 0.0207 0.0194 0.0177 -2.08 -0.196 0.0210 0.0213 0.0214 0.0216 0.0210 0.0203 0.0211 0.0215 0.0197 -1.02 -0.104 0.0232 0.0235 0.0236 0.0234 0.0235 0.0225 0.0230 0.0236 0.0226 -0.01 -0.038 0.0241 0.0247 0.0247 0.0244 0.0237 0.0234 0.0237 0.0243 0.0236 1.03 0.072 0.0252 0.0261 0.0260 0.0257 0.0256 0.0247 0.0239 0.0250 0.0246 2.10 0.293 0.0256 0.0259 0.0259 0.0261 0.0266 0.0251 0.0247 0.0253 0.0255 3.15 0.524 0.0225 0.0221 0.0233 0.0227 0.0227 0.0231 0.0216 0.0233 0.0212 4.14 0.676 0.0182 0.0175 0.0187 0.0183 0.0189 0.0187 0.0173 0.0191 0.0174 5.17 0.757 0.0156 0.0153 0.0154 0.0155 0.0165 0.0163 0.0145 0.0161 0.0150 6.18 0.829 0.0152 0.0145 0.0157 0.0147 0.0158 0.0148 0.0152 0.0163 0.0148 7.24 0.893 0.0150 0.0138 0.0150 0.0156 0.0156 0.0147 0.0160 0.0153 0.0140 8.30 0.943 0.0185 0.0169 0.0182 0.0184 0.0205 0.0182 0.0199 0.0187 0.0177 9.26 0.989 0.0236 0.0235 0.0225 0.0233 0.0259 0.0243 0.0233 0.0240 0.0221 10.27 1.013 0.0305 0.0288 0.0288 0.0294 0.0314 0.0331 0.0315 0.0313 0.0294 11.23 1.039 0.0379 0.0342 0.0343 0.0356 0.0387 0.0421 0.0429 0.0393 0.0359 12.25 1.047 0.0514 0.0386 0.0398 0.0445 0.0531 0.0640 0.0683 0.0558 0.0468 13.28 1.045 0.0692 0.0474 0.0539 0.0657 0.0790 0.0923 0.0874 0.0713 0.0567 Tabulated from data in file bm05039.dat & reduced using program C10.20 Average Reynolds #: 199914 Number of angles of attack: 23 alpha / Cl / Cd / Spanwise Cd's >>> -10.20 -0.840 0.0274 0.0282 0.0270 0.0286 0.0273 0.0265 0.0272 0.0273 0.0274 -9.22 -0.834 0.0250 0.0254 0.0247 0.0258 0.0253 0.0241 0.0247 0.0247 0.0249 -8.17 -0.782 0.0221 0.0231 0.0221 0.0224 0.0225 0.0213 0.0223 0.0223 0.0212 -7.20 -0.700 0.0204 0.0210 0.0196 0.0224 0.0202 0.0196 0.0204 0.0205 0.0193 -6.15 -0.582 0.0186 0.0192 0.0186 0.0200 0.0175 0.0184 0.0182 0.0185 0.0181 -5.10 -0.458 0.0180 0.0185 0.0179 0.0184 0.0179 0.0184 0.0172 0.0175 0.0184 -4.10 -0.342 0.0183 0.0181 0.0184 0.0193 0.0181 0.0180 0.0180 0.0183 0.0178 -3.04 -0.221 0.0185 0.0187 0.0187 0.0196 0.0184 0.0179 0.0185 0.0186 0.0177 -1.95 -0.092 0.0191 0.0194 0.0198 0.0194 0.0190 0.0187 0.0190 0.0192 0.0183 -1.00 0.012 0.0191 0.0197 0.0195 0.0191 0.0193 0.0186 0.0188 0.0195 0.0184 0.03 0.130 0.0194 0.0200 0.0198 0.0192 0.0200 0.0191 0.0191 0.0194 0.0186 1.05 0.229 0.0190 0.0197 0.0190 0.0186 0.0196 0.0187 0.0187 0.0188 0.0189 2.06 0.332 0.0175 0.0175 0.0178 0.0169 0.0179 0.0177 0.0169 0.0175 0.0176 3.12 0.478 0.0158 0.0155 0.0161 0.0156 0.0168 0.0158 0.0146 0.0155 0.0163 4.18 0.651 0.0137 0.0116 0.0159 0.0142 0.0126 0.0144 0.0125 0.0159 0.0126 5.19 0.784 0.0129 0.0114 0.0132 0.0134 0.0135 0.0126 0.0130 0.0142 0.0122 6.23 0.864 0.0127 0.0112 0.0130 0.0135 0.0132 0.0124 0.0139 0.0130 0.0117 7.17 0.890 0.0139 0.0124 0.0136 0.0145 0.0145 0.0137 0.0152 0.0140 0.0130 8.22 0.936 0.0173 0.0161 0.0170 0.0175 0.0187 0.0174 0.0185 0.0171 0.0161 9.23 0.985 0.0213 0.0205 0.0208 0.0214 0.0223 0.0223 0.0223 0.0211 0.0201 10.27 1.023 0.0286 0.0277 0.0264 0.0278 0.0292 0.0300 0.0306 0.0299 0.0269 11.26 1.055 0.0354 0.0316 0.0327 0.0334 0.0364 0.0385 0.0416 0.0367 0.0321 12.27 1.064 0.0505 0.0329 0.0339 0.0407 0.0524 0.0665 0.0729 0.0599 0.0446 Tabulated from data in file bm05041.dat & reduced using program C10.20 Average Reynolds #: 349949 Number of angles of attack: 24 alpha / Cl / Cd / Spanwise Cd's >>> -10.21 -0.885 0.0238 0.0245 0.0237 0.0255 0.0235 0.0228 0.0234 0.0240 0.0231 -9.22 -0.797 0.0209 0.0213 0.0205 0.0216 0.0214 0.0201 0.0206 0.0212 0.0205 -8.12 -0.674 0.0182 0.0185 0.0181 0.0189 0.0183 0.0177 0.0181 0.0185 0.0179 -7.15 -0.549 0.0164 0.0167 0.0164 0.0176 0.0162 0.0160 0.0162 0.0162 0.0160 -6.08 -0.423 0.0148 0.0147 0.0150 0.0160 0.0144 0.0147 0.0146 0.0146 0.0146 -5.08 -0.299 0.0136 0.0133 0.0139 0.0141 0.0136 0.0134 0.0132 0.0135 0.0133 -4.04 -0.189 0.0125 0.0127 0.0125 0.0129 0.0127 0.0122 0.0120 0.0126 0.0122 -3.03 -0.083 0.0116 0.0121 0.0120 0.0119 0.0117 0.0114 0.0112 0.0119 0.0109 -2.00 0.024 0.0110 0.0118 0.0111 0.0107 0.0111 0.0108 0.0107 0.0111 0.0104 -0.98 0.130 0.0104 0.0111 0.0106 0.0099 0.0111 0.0101 0.0100 0.0101 0.0100 0.08 0.238 0.0099 0.0105 0.0098 0.0092 0.0104 0.0102 0.0096 0.0095 0.0101 1.07 0.337 0.0099 0.0098 0.0099 0.0094 0.0099 0.0100 0.0097 0.0098 0.0102 2.11 0.441 0.0101 0.0099 0.0103 0.0102 0.0098 0.0103 0.0102 0.0101 0.0103 3.14 0.535 0.0102 0.0095 0.0104 0.0102 0.0101 0.0107 0.0101 0.0102 0.0101 4.22 0.624 0.0099 0.0087 0.0105 0.0099 0.0097 0.0105 0.0097 0.0096 0.0103 5.16 0.707 0.0099 0.0086 0.0111 0.0095 0.0095 0.0109 0.0096 0.0094 0.0104 6.18 0.806 0.0106 0.0083 0.0118 0.0100 0.0119 0.0122 0.0100 0.0098 0.0110 7.17 0.863 0.0125 0.0117 0.0128 0.0130 0.0129 0.0130 0.0127 0.0118 0.0119 8.27 0.926 0.0164 0.0160 0.0157 0.0167 0.0173 0.0169 0.0171 0.0159 0.0158 9.25 0.988 0.0201 0.0190 0.0191 0.0202 0.0213 0.0210 0.0214 0.0197 0.0189 10.25 1.037 0.0255 0.0231 0.0230 0.0242 0.0265 0.0280 0.0293 0.0260 0.0239 11.22 1.069 0.0322 0.0256 0.0261 0.0279 0.0366 0.0445 0.0391 0.0302 0.0278 12.32 1.081 0.0492 0.0280 0.0297 0.0415 0.0536 0.0692 0.0712 0.0585 0.0423 13.31 1.076 0.0722 0.0383 0.0577 0.0736 0.0909 0.0992 0.0896 0.0723 0.0558 Tabulated from data in file bm05043.dat & reduced using program C10.20 Average Reynolds #: 499497 Number of angles of attack: 24 alpha / Cl / Cd / Spanwise Cd's >>> -10.17 -0.811 0.0203 0.0204 0.0200 0.0216 0.0205 0.0194 0.0198 0.0207 0.0201 -9.14 -0.706 0.0174 0.0173 0.0171 0.0184 0.0177 0.0166 0.0171 0.0179 0.0172 -8.14 -0.584 0.0151 0.0151 0.0149 0.0163 0.0147 0.0148 0.0150 0.0154 0.0147 -7.11 -0.475 0.0135 0.0133 0.0135 0.0147 0.0131 0.0134 0.0133 0.0134 0.0132 -6.06 -0.374 0.0121 0.0118 0.0122 0.0133 0.0118 0.0121 0.0118 0.0119 0.0117 -5.06 -0.276 0.0108 0.0104 0.0111 0.0118 0.0108 0.0105 0.0107 0.0108 0.0103 -4.00 -0.173 0.0099 0.0097 0.0100 0.0106 0.0101 0.0096 0.0095 0.0102 0.0094 -3.01 -0.073 0.0091 0.0092 0.0094 0.0092 0.0093 0.0089 0.0087 0.0095 0.0084 -1.96 0.039 0.0085 0.0092 0.0088 0.0083 0.0087 0.0083 0.0080 0.0090 0.0078 -0.98 0.140 0.0081 0.0087 0.0083 0.0077 0.0088 0.0079 0.0078 0.0083 0.0077 0.07 0.246 0.0078 0.0080 0.0078 0.0071 0.0086 0.0078 0.0075 0.0077 0.0078 1.04 0.345 0.0077 0.0075 0.0075 0.0071 0.0080 0.0080 0.0073 0.0077 0.0082 2.14 0.461 0.0078 0.0073 0.0081 0.0080 0.0076 0.0080 0.0073 0.0079 0.0082 3.15 0.566 0.0081 0.0070 0.0086 0.0084 0.0080 0.0085 0.0077 0.0081 0.0081 4.17 0.662 0.0085 0.0077 0.0090 0.0086 0.0087 0.0091 0.0084 0.0085 0.0083 5.20 0.747 0.0094 0.0085 0.0098 0.0094 0.0097 0.0100 0.0093 0.0092 0.0091 6.19 0.808 0.0111 0.0089 0.0134 0.0108 0.0122 0.0126 0.0103 0.0104 0.0100 7.24 0.868 0.0131 0.0115 0.0136 0.0137 0.0140 0.0134 0.0133 0.0131 0.0124 8.26 0.937 0.0159 0.0150 0.0155 0.0160 0.0169 0.0169 0.0163 0.0154 0.0152 9.25 1.003 0.0191 0.0177 0.0180 0.0185 0.0201 0.0208 0.0206 0.0186 0.0184 10.24 1.056 0.0235 0.0202 0.0214 0.0218 0.0245 0.0261 0.0273 0.0241 0.0226 11.27 1.097 0.0315 0.0241 0.0237 0.0254 0.0367 0.0451 0.0400 0.0300 0.0268 12.36 1.119 0.0456 0.0253 0.0257 0.0323 0.0461 0.0602 0.0701 0.0612 0.0441 13.24 1.119 0.0682 0.0321 0.0442 0.0593 0.0766 0.0909 0.0941 0.0817 0.0666 Tabulated from data in file bm05045.dat & reduced using program C10.20 File s834_c.drg created using program C10.20 on Thu May 22 17:01:35 2003