Airfoil: SD2030 (B) Builder: Y. Tinel Comment: 'u.s.t. located at 2% chord, l.s.t. located at 5% chord' Number of Reynolds #'s: 4 Average Reynolds #: 100118 Number of angles of attack: 19 alpha / Cl / Cd / Spanwise Cd's >>> -5.95 -0.391 0.0523 0.0536 0.0541 0.0566 0.0543 0.0519 0.0503 0.0482 0.0493 -4.96 -0.319 0.0315 0.0312 0.0317 0.0326 0.0320 0.0314 0.0311 0.0313 0.0309 -3.96 -0.250 0.0236 0.0232 0.0233 0.0237 0.0239 0.0235 0.0236 0.0236 0.0241 -2.94 -0.166 0.0187 0.0193 0.0188 0.0189 0.0189 0.0182 0.0185 0.0187 0.0182 -1.92 -0.072 0.0154 0.0161 0.0150 0.0138 0.0171 0.0152 0.0153 0.0155 0.0156 -0.87 0.006 0.0141 0.0152 0.0136 0.0147 0.0154 0.0138 0.0113 0.0138 0.0154 0.10 0.105 0.0148 0.0145 0.0145 0.0144 0.0145 0.0151 0.0153 0.0150 0.0148 1.21 0.267 0.0165 0.0166 0.0161 0.0164 0.0160 0.0169 0.0164 0.0159 0.0173 2.18 0.438 0.0157 0.0167 0.0151 0.0149 0.0155 0.0158 0.0156 0.0154 0.0167 3.25 0.557 0.0146 0.0140 0.0134 0.0125 0.0137 0.0154 0.0157 0.0159 0.0161 4.27 0.659 0.0137 0.0151 0.0144 0.0133 0.0123 0.0130 0.0137 0.0135 0.0146 5.31 0.736 0.0157 0.0151 0.0154 0.0150 0.0157 0.0153 0.0163 0.0161 0.0167 6.29 0.804 0.0193 0.0194 0.0202 0.0182 0.0192 0.0186 0.0196 0.0191 0.0204 7.30 0.879 0.0228 0.0213 0.0223 0.0224 0.0222 0.0227 0.0238 0.0233 0.0246 8.32 0.958 0.0269 0.0269 0.0267 0.0260 0.0259 0.0264 0.0265 0.0271 0.0294 9.32 1.015 0.0334 0.0335 0.0333 0.0321 0.0322 0.0319 0.0338 0.0342 0.0365 10.37 1.060 0.0443 0.0460 0.0466 0.0443 0.0427 0.0430 0.0437 0.0434 0.0448 11.39 1.080 0.0709 0.0656 0.0652 0.0661 0.0677 0.0703 0.0758 0.0771 0.0794 12.40 0.999 0.1818 0.1663 0.1712 0.1791 0.1798 0.1809 0.1882 0.1934 0.1954 Tabulated from data in file bm05085.dat & reduced using program C10.20 Average Reynolds #: 200033 Number of angles of attack: 19 alpha / Cl / Cd / Spanwise Cd's >>> -6.02 -0.440 0.0546 0.0573 0.0559 0.0560 0.0522 0.0497 0.0522 0.0554 0.0579 -5.02 -0.351 0.0295 0.0308 0.0307 0.0299 0.0290 0.0283 0.0283 0.0295 0.0295 -3.98 -0.252 0.0186 0.0196 0.0190 0.0188 0.0191 0.0178 0.0178 0.0182 0.0189 -2.93 -0.139 0.0164 0.0194 0.0151 0.0145 0.0170 0.0166 0.0157 0.0155 0.0177 -1.90 0.012 0.0137 0.0165 0.0166 0.0104 0.0111 0.0109 0.0125 0.0164 0.0150 -0.89 0.159 0.0112 0.0118 0.0120 0.0105 0.0107 0.0107 0.0095 0.0107 0.0137 0.18 0.253 0.0110 0.0125 0.0110 0.0110 0.0119 0.0120 0.0103 0.0103 0.0090 1.14 0.336 0.0123 0.0130 0.0127 0.0124 0.0121 0.0126 0.0124 0.0117 0.0115 2.19 0.437 0.0130 0.0130 0.0135 0.0130 0.0129 0.0135 0.0129 0.0127 0.0125 3.16 0.535 0.0136 0.0134 0.0136 0.0137 0.0139 0.0140 0.0133 0.0132 0.0134 4.27 0.635 0.0148 0.0141 0.0150 0.0152 0.0155 0.0155 0.0145 0.0142 0.0144 5.29 0.735 0.0162 0.0158 0.0159 0.0165 0.0167 0.0169 0.0164 0.0157 0.0158 6.30 0.824 0.0174 0.0165 0.0174 0.0178 0.0180 0.0177 0.0176 0.0170 0.0168 7.36 0.917 0.0193 0.0188 0.0189 0.0197 0.0197 0.0195 0.0201 0.0179 0.0198 8.31 0.999 0.0218 0.0214 0.0215 0.0216 0.0223 0.0217 0.0222 0.0213 0.0225 9.37 1.062 0.0285 0.0283 0.0279 0.0277 0.0288 0.0290 0.0288 0.0283 0.0290 10.37 1.108 0.0329 0.0337 0.0348 0.0330 0.0323 0.0329 0.0324 0.0320 0.0323 11.42 1.145 0.0416 0.0387 0.0396 0.0394 0.0405 0.0434 0.0451 0.0431 0.0431 12.36 1.067 0.1738 0.1664 0.1749 0.1816 0.1796 0.1753 0.1773 0.1700 0.1652 Tabulated from data in file bm05087.dat & reduced using program C10.20 Average Reynolds #: 350702 Number of angles of attack: 19 alpha / Cl / Cd / Spanwise Cd's >>> -6.02 -0.406 0.0482 0.0527 0.0524 0.0481 0.0420 0.0418 0.0470 0.0491 0.0522 -4.97 -0.260 0.0187 0.0175 0.0244 0.0184 0.0173 0.0160 0.0167 0.0183 0.0212 -3.95 -0.146 0.0141 0.0142 0.0141 0.0140 0.0151 0.0130 0.0129 0.0154 0.0140 -2.94 -0.056 0.0132 0.0134 0.0138 0.0134 0.0138 0.0123 0.0124 0.0137 0.0127 -1.89 0.047 0.0130 0.0134 0.0132 0.0123 0.0139 0.0127 0.0124 0.0129 0.0128 -0.82 0.150 0.0129 0.0130 0.0130 0.0125 0.0138 0.0129 0.0127 0.0128 0.0129 0.12 0.248 0.0132 0.0131 0.0132 0.0132 0.0133 0.0133 0.0132 0.0132 0.0133 1.18 0.360 0.0135 0.0132 0.0137 0.0137 0.0133 0.0138 0.0135 0.0135 0.0134 2.21 0.459 0.0138 0.0133 0.0142 0.0140 0.0139 0.0142 0.0136 0.0137 0.0135 3.27 0.565 0.0145 0.0140 0.0147 0.0145 0.0150 0.0148 0.0143 0.0143 0.0142 4.21 0.666 0.0152 0.0150 0.0154 0.0158 0.0159 0.0156 0.0148 0.0145 0.0148 5.28 0.769 0.0162 0.0158 0.0160 0.0171 0.0166 0.0168 0.0161 0.0153 0.0155 6.31 0.868 0.0170 0.0170 0.0169 0.0176 0.0176 0.0173 0.0174 0.0163 0.0159 7.27 0.953 0.0174 0.0176 0.0170 0.0178 0.0181 0.0174 0.0182 0.0167 0.0166 8.35 1.044 0.0190 0.0191 0.0184 0.0187 0.0195 0.0186 0.0200 0.0190 0.0190 9.32 1.111 0.0237 0.0221 0.0214 0.0220 0.0240 0.0247 0.0257 0.0250 0.0244 10.39 1.149 0.0315 0.0287 0.0281 0.0296 0.0320 0.0332 0.0352 0.0327 0.0325 11.37 1.164 0.0426 0.0393 0.0394 0.0399 0.0437 0.0464 0.0470 0.0437 0.0414 12.29 1.117 0.1592 0.1541 0.1630 0.1717 0.1671 0.1655 0.1609 0.1493 0.1417 Tabulated from data in file bm05089.dat & reduced using program C10.20 Average Reynolds #: 499335 Number of angles of attack: 19 alpha / Cl / Cd / Spanwise Cd's >>> -5.98 -0.340 0.0411 0.0415 0.0417 0.0425 0.0400 0.0381 0.0390 0.0417 0.0443 -5.02 -0.256 0.0180 0.0179 0.0184 0.0189 0.0184 0.0166 0.0165 0.0187 0.0186 -3.92 -0.149 0.0144 0.0153 0.0151 0.0147 0.0145 0.0136 0.0133 0.0150 0.0140 -2.91 -0.056 0.0129 0.0136 0.0134 0.0129 0.0134 0.0123 0.0124 0.0129 0.0121 -1.92 0.046 0.0122 0.0128 0.0126 0.0119 0.0131 0.0116 0.0119 0.0122 0.0118 -0.86 0.149 0.0123 0.0125 0.0123 0.0119 0.0131 0.0121 0.0120 0.0120 0.0121 0.17 0.251 0.0124 0.0123 0.0122 0.0123 0.0127 0.0124 0.0122 0.0124 0.0125 1.21 0.366 0.0127 0.0122 0.0127 0.0131 0.0124 0.0129 0.0127 0.0126 0.0127 2.21 0.474 0.0131 0.0125 0.0133 0.0133 0.0130 0.0134 0.0131 0.0131 0.0130 3.27 0.576 0.0134 0.0127 0.0137 0.0134 0.0136 0.0137 0.0133 0.0133 0.0134 4.27 0.675 0.0142 0.0138 0.0143 0.0145 0.0147 0.0147 0.0139 0.0137 0.0139 5.30 0.777 0.0149 0.0148 0.0150 0.0158 0.0154 0.0153 0.0147 0.0141 0.0145 6.28 0.874 0.0161 0.0160 0.0159 0.0171 0.0165 0.0163 0.0161 0.0152 0.0155 7.37 0.975 0.0173 0.0174 0.0168 0.0179 0.0178 0.0172 0.0182 0.0166 0.0167 8.35 1.059 0.0198 0.0191 0.0181 0.0194 0.0204 0.0200 0.0219 0.0200 0.0193 9.40 1.108 0.0247 0.0240 0.0233 0.0232 0.0254 0.0259 0.0270 0.0249 0.0239 10.39 1.149 0.0299 0.0293 0.0282 0.0288 0.0302 0.0317 0.0325 0.0297 0.0290 11.42 1.171 0.0392 0.0357 0.0360 0.0369 0.0409 0.0448 0.0437 0.0392 0.0366 12.41 1.159 0.0675 0.0430 0.0476 0.0625 0.0804 0.0900 0.0870 0.0722 0.0574 Tabulated from data in file bm05091.dat & reduced using program C10.20 File sd2030_tf.drg created using program C10.20 on Thu May 22 17:01:36 2003