Airfoil: SD2030 (B) Builder: Y. Tinel Comment: 'clean' Number of Reynolds #'s: 7 Average Reynolds #: 100002 Number of angles of attack: 18 alpha / Cl / Cd / Spanwise Cd's >>> -6.02 -0.414 0.0531 0.0529 0.0531 0.0560 0.0558 0.0541 0.0521 0.0506 0.0505 -4.95 -0.339 0.0321 0.0313 0.0318 0.0339 0.0342 0.0323 0.0317 0.0312 0.0305 -3.98 -0.262 0.0238 0.0226 0.0228 0.0240 0.0248 0.0249 0.0239 0.0234 0.0238 -2.99 -0.170 0.0189 0.0185 0.0186 0.0180 0.0189 0.0188 0.0193 0.0190 0.0202 -1.90 -0.074 0.0136 0.0132 0.0133 0.0137 0.0144 0.0135 0.0126 0.0138 0.0146 -0.93 0.011 0.0138 0.0151 0.0126 0.0114 0.0125 0.0143 0.0133 0.0147 0.0162 0.11 0.122 0.0154 0.0190 0.0160 0.0149 0.0151 0.0159 0.0148 0.0132 0.0142 1.14 0.231 0.0163 0.0163 0.0167 0.0143 0.0159 0.0157 0.0176 0.0170 0.0171 2.17 0.403 0.0188 0.0195 0.0185 0.0181 0.0188 0.0189 0.0190 0.0187 0.0188 3.17 0.574 0.0171 0.0175 0.0162 0.0166 0.0166 0.0166 0.0179 0.0172 0.0186 4.26 0.693 0.0154 0.0154 0.0150 0.0148 0.0140 0.0155 0.0160 0.0156 0.0170 5.29 0.784 0.0147 0.0153 0.0139 0.0144 0.0151 0.0144 0.0148 0.0144 0.0157 6.32 0.873 0.0170 0.0153 0.0156 0.0157 0.0160 0.0175 0.0179 0.0180 0.0198 7.33 0.945 0.0215 0.0218 0.0215 0.0198 0.0217 0.0206 0.0211 0.0217 0.0235 8.34 1.000 0.0269 0.0275 0.0255 0.0246 0.0260 0.0259 0.0274 0.0276 0.0306 9.36 1.051 0.0351 0.0353 0.0345 0.0335 0.0337 0.0346 0.0360 0.0361 0.0372 10.34 1.090 0.0437 0.0405 0.0392 0.0393 0.0415 0.0440 0.0464 0.0486 0.0499 11.39 1.105 0.0679 0.0691 0.0660 0.0665 0.0669 0.0681 0.0685 0.0682 0.0698 Tabulated from data in file bm05077.dat & reduced using program C10.20 Average Reynolds #: 199829 Number of angles of attack: 18 alpha / Cl / Cd / Spanwise Cd's >>> -6.04 -0.447 0.0550 0.0575 0.0573 0.0558 0.0546 0.0527 0.0535 0.0535 0.0551 -4.98 -0.336 0.0286 0.0304 0.0295 0.0289 0.0279 0.0269 0.0278 0.0287 0.0288 -3.95 -0.235 0.0194 0.0203 0.0199 0.0193 0.0194 0.0186 0.0189 0.0193 0.0198 -2.98 -0.126 0.0163 0.0180 0.0154 0.0156 0.0159 0.0163 0.0159 0.0158 0.0174 -1.87 0.006 0.0131 0.0145 0.0119 0.0125 0.0139 0.0131 0.0128 0.0132 0.0128 -0.88 0.115 0.0116 0.0083 0.0160 0.0077 0.0143 0.0107 0.0160 0.0108 0.0088 0.15 0.252 0.0118 0.0115 0.0135 0.0096 0.0124 0.0115 0.0131 0.0103 0.0129 1.17 0.391 0.0111 0.0109 0.0121 0.0103 0.0112 0.0110 0.0118 0.0105 0.0113 2.23 0.499 0.0104 0.0101 0.0104 0.0093 0.0111 0.0114 0.0098 0.0100 0.0109 3.21 0.593 0.0099 0.0097 0.0105 0.0103 0.0106 0.0103 0.0086 0.0087 0.0106 4.22 0.690 0.0096 0.0088 0.0089 0.0098 0.0099 0.0104 0.0101 0.0092 0.0095 5.26 0.784 0.0113 0.0105 0.0110 0.0110 0.0115 0.0118 0.0117 0.0110 0.0116 6.30 0.869 0.0142 0.0131 0.0139 0.0140 0.0149 0.0148 0.0147 0.0141 0.0143 7.34 0.945 0.0178 0.0177 0.0169 0.0178 0.0199 0.0177 0.0171 0.0183 0.0172 8.35 1.012 0.0221 0.0220 0.0206 0.0209 0.0227 0.0223 0.0222 0.0225 0.0233 9.34 1.070 0.0278 0.0275 0.0274 0.0269 0.0278 0.0277 0.0285 0.0280 0.0285 10.37 1.112 0.0344 0.0336 0.0335 0.0334 0.0343 0.0349 0.0358 0.0347 0.0349 11.38 1.138 0.0472 0.0441 0.0450 0.0459 0.0481 0.0489 0.0490 0.0488 0.0481 Tabulated from data in file bm05079.dat & reduced using program C10.20 Average Reynolds #: 204098 Number of angles of attack: 2 alpha / Cl / Cd / Spanwise Cd's >>> 12.41 1.072 0.1847 0.1799 0.1885 0.1900 0.1901 0.1879 0.1889 0.1797 0.1727 13.39 0.996 0.2214 0.2130 0.2141 0.2190 0.2271 0.2355 0.2316 0.2198 0.2114 Tabulated from data in file bm05133.dat & reduced using program C10.20 Average Reynolds #: 349889 Number of angles of attack: 18 alpha / Cl / Cd / Spanwise Cd's >>> -6.53 -0.486 0.0698 0.0729 0.0706 0.0696 0.0672 0.0665 0.0669 0.0701 0.0746 -5.48 -0.361 0.0371 0.0391 0.0375 0.0380 0.0359 0.0343 0.0362 0.0369 0.0386 -4.50 -0.246 0.0186 0.0203 0.0202 0.0186 0.0144 0.0179 0.0180 0.0197 0.0197 -3.44 -0.115 0.0142 0.0151 0.0146 0.0156 0.0158 0.0121 0.0129 0.0134 0.0143 -2.44 0.024 0.0105 0.0090 0.0108 0.0117 0.0133 0.0076 0.0096 0.0104 0.0114 -1.36 0.140 0.0085 0.0064 0.0087 0.0092 0.0096 0.0069 0.0073 0.0081 0.0115 -0.35 0.229 0.0075 0.0070 0.0075 0.0077 0.0065 0.0069 0.0072 0.0065 0.0111 0.67 0.332 0.0081 0.0099 0.0072 0.0077 0.0071 0.0076 0.0080 0.0071 0.0103 1.68 0.444 0.0071 0.0064 0.0071 0.0067 0.0073 0.0061 0.0079 0.0065 0.0087 2.72 0.552 0.0070 0.0066 0.0071 0.0072 0.0067 0.0061 0.0077 0.0067 0.0080 3.74 0.661 0.0074 0.0073 0.0076 0.0080 0.0074 0.0075 0.0072 0.0070 0.0071 4.85 0.757 0.0094 0.0094 0.0095 0.0101 0.0098 0.0097 0.0091 0.0090 0.0088 5.81 0.843 0.0117 0.0117 0.0116 0.0123 0.0122 0.0119 0.0117 0.0112 0.0110 6.83 0.930 0.0144 0.0147 0.0140 0.0150 0.0150 0.0143 0.0149 0.0139 0.0134 7.78 1.003 0.0170 0.0174 0.0165 0.0171 0.0171 0.0169 0.0176 0.0171 0.0165 8.85 1.075 0.0212 0.0217 0.0205 0.0208 0.0216 0.0212 0.0217 0.0215 0.0205 9.87 1.129 0.0271 0.0272 0.0265 0.0261 0.0278 0.0275 0.0284 0.0268 0.0266 10.90 1.167 0.0392 0.0378 0.0379 0.0372 0.0392 0.0418 0.0419 0.0394 0.0381 Tabulated from data in file bm05081.dat & reduced using program C10.20 Average Reynolds #: 355456 Number of angles of attack: 2 alpha / Cl / Cd / Spanwise Cd's >>> 11.87 1.152 0.1079 0.1125 0.1153 0.1163 0.1147 0.1120 0.1056 0.0974 0.0893 12.88 1.094 0.1997 0.2045 0.2117 0.2151 0.2138 0.2045 0.1922 0.1810 0.1744 Tabulated from data in file bm05134.dat & reduced using program C10.20 Average Reynolds #: 499053 Number of angles of attack: 18 alpha / Cl / Cd / Spanwise Cd's >>> -6.00 -0.368 0.0445 0.0450 0.0466 0.0463 0.0434 0.0414 0.0424 0.0440 0.0470 -4.93 -0.238 0.0164 0.0153 0.0186 0.0186 0.0131 0.0165 0.0176 0.0144 0.0172 -3.95 -0.122 0.0119 0.0111 0.0133 0.0132 0.0115 0.0100 0.0128 0.0112 0.0122 -2.91 -0.009 0.0105 0.0112 0.0113 0.0109 0.0106 0.0096 0.0102 0.0098 0.0107 -1.88 0.099 0.0090 0.0111 0.0076 0.0082 0.0112 0.0063 0.0098 0.0068 0.0114 -0.86 0.186 0.0064 0.0064 0.0053 0.0052 0.0075 0.0059 0.0068 0.0054 0.0090 0.20 0.291 0.0058 0.0056 0.0051 0.0056 0.0065 0.0048 0.0060 0.0053 0.0076 1.16 0.410 0.0053 0.0049 0.0052 0.0056 0.0053 0.0049 0.0056 0.0050 0.0063 2.23 0.525 0.0057 0.0056 0.0060 0.0055 0.0054 0.0058 0.0058 0.0059 0.0057 3.24 0.628 0.0064 0.0064 0.0068 0.0063 0.0067 0.0066 0.0063 0.0063 0.0062 4.28 0.725 0.0084 0.0085 0.0085 0.0087 0.0087 0.0086 0.0082 0.0079 0.0080 5.28 0.814 0.0103 0.0102 0.0103 0.0109 0.0106 0.0106 0.0101 0.0098 0.0098 6.30 0.909 0.0125 0.0126 0.0123 0.0130 0.0130 0.0126 0.0127 0.0121 0.0117 7.34 0.993 0.0149 0.0151 0.0143 0.0153 0.0153 0.0149 0.0155 0.0143 0.0141 8.36 1.068 0.0178 0.0181 0.0171 0.0178 0.0181 0.0177 0.0190 0.0176 0.0170 9.39 1.134 0.0220 0.0218 0.0211 0.0212 0.0223 0.0222 0.0236 0.0220 0.0214 10.42 1.176 0.0273 0.0263 0.0262 0.0256 0.0276 0.0286 0.0295 0.0278 0.0271 11.40 1.199 0.0356 0.0323 0.0323 0.0323 0.0355 0.0411 0.0412 0.0367 0.0337 Tabulated from data in file bm05083.dat & reduced using program C10.20 Average Reynolds #: 501810 Number of angles of attack: 1 alpha / Cl / Cd / Spanwise Cd's >>> 12.40 1.205 0.0594 0.0398 0.0412 0.0537 0.0721 0.0791 0.0777 0.0627 0.0487 Tabulated from data in file bm05135.dat & reduced using program C10.20 File sd2030_c.drg created using program C10.20 on Thu May 22 17:01:36 2003