Airfoil: SD7080 Builder: P. Illick Comment: clean Number of Reynolds #'s: 4 Average Reynolds #: 99943 Number of angles of attack: 18 alpha / Cl / Cd / Spanwise Cd's >>> -6.02 -0.413 0.0437 0.0427 0.0448 0.0443 0.0432 -4.93 -0.346 0.0292 0.0280 0.0293 0.0300 0.0294 -3.91 -0.269 0.0246 0.0297 0.0231 0.0225 0.0231 -2.97 -0.176 0.0191 0.0206 0.0168 0.0174 0.0214 -1.95 -0.053 0.0143 0.0157 0.0130 0.0132 0.0154 -0.76 0.124 0.0138 0.0150 0.0119 0.0123 0.0161 0.18 0.245 0.0149 0.0149 0.0138 0.0137 0.0171 1.22 0.355 0.0150 0.0143 0.0140 0.0143 0.0173 2.28 0.446 0.0156 0.0148 0.0148 0.0154 0.0174 3.25 0.526 0.0151 0.0150 0.0153 0.0147 0.0156 4.21 0.633 0.0151 0.0160 0.0147 0.0142 0.0154 5.26 0.734 0.0170 0.0179 0.0159 0.0166 0.0176 6.32 0.827 0.0193 0.0197 0.0187 0.0194 0.0193 7.29 0.905 0.0224 0.0222 0.0216 0.0220 0.0239 8.32 0.986 0.0242 0.0237 0.0249 0.0219 0.0264 9.34 1.024 0.0292 0.0289 0.0260 0.0310 0.0310 10.32 1.052 0.0372 0.0385 0.0358 0.0369 0.0374 11.24 1.076 0.0441 0.0468 0.0435 0.0427 0.0432 Tabulated from data in file ag02588.dat & reduced using program C06.01 Average Reynolds #: 149842 Number of angles of attack: 18 alpha / Cl / Cd / Spanwise Cd's >>> -6.01 -0.410 0.0433 0.0425 0.0434 0.0434 0.0437 -4.81 -0.284 0.0255 0.0266 0.0248 0.0250 0.0258 -3.90 -0.189 0.0201 0.0198 0.0197 0.0190 0.0220 -2.86 -0.061 0.0160 0.0156 0.0143 0.0153 0.0189 -1.81 0.041 0.0125 0.0121 0.0118 0.0122 0.0140 -0.71 0.172 0.0114 0.0114 0.0108 0.0112 0.0120 0.40 0.273 0.0113 0.0097 0.0115 0.0122 0.0120 1.21 0.346 0.0118 0.0112 0.0129 0.0110 0.0120 2.24 0.457 0.0125 0.0110 0.0133 0.0112 0.0148 3.25 0.567 0.0116 0.0106 0.0111 0.0124 0.0122 4.21 0.660 0.0121 0.0123 0.0115 0.0124 0.0124 5.31 0.755 0.0151 0.0156 0.0153 0.0148 0.0149 6.22 0.836 0.0170 0.0170 0.0169 0.0171 0.0171 7.26 0.928 0.0194 0.0195 0.0185 0.0196 0.0200 8.34 1.005 0.0228 0.0237 0.0216 0.0227 0.0233 9.29 1.036 0.0295 0.0308 0.0283 0.0297 0.0294 10.42 1.069 0.0376 0.0396 0.0376 0.0365 0.0368 11.22 1.083 0.0463 0.0514 0.0441 0.0459 0.0438 Tabulated from data in file ag02590.dat & reduced using program C06.01 Average Reynolds #: 199879 Number of angles of attack: 18 alpha / Cl / Cd / Spanwise Cd's >>> -5.94 -0.379 0.0376 0.0376 0.0372 0.0377 0.0381 -5.34 -0.306 0.0277 0.0273 0.0267 0.0286 0.0280 -3.84 -0.139 0.0175 0.0190 0.0152 0.0173 0.0184 -2.75 -0.028 0.0150 0.0175 0.0126 0.0138 0.0160 -1.71 0.056 0.0113 0.0116 0.0107 0.0107 0.0122 -0.75 0.152 0.0099 0.0096 0.0086 0.0119 0.0096 0.24 0.259 0.0094 0.0089 0.0095 0.0100 0.0092 1.41 0.379 0.0098 0.0093 0.0092 0.0099 0.0108 2.27 0.474 0.0096 0.0088 0.0095 0.0100 0.0102 3.24 0.573 0.0102 0.0100 0.0103 0.0105 0.0101 4.40 0.688 0.0120 0.0125 0.0120 0.0120 0.0118 5.09 0.753 0.0132 0.0138 0.0135 0.0129 0.0127 6.31 0.866 0.0153 0.0153 0.0149 0.0152 0.0158 7.25 0.953 0.0173 0.0170 0.0165 0.0174 0.0182 8.28 1.013 0.0224 0.0225 0.0201 0.0235 0.0234 9.34 1.056 0.0285 0.0287 0.0274 0.0295 0.0285 10.23 1.085 0.0352 0.0360 0.0340 0.0357 0.0351 11.26 1.101 0.0456 0.0457 0.0448 0.0470 0.0448 Tabulated from data in file ag02592.dat & reduced using program C06.01 Average Reynolds #: 299767 Number of angles of attack: 18 alpha / Cl / Cd / Spanwise Cd's >>> -6.19 -0.390 0.0412 0.0415 0.0405 0.0416 0.0410 -5.06 -0.265 0.0226 0.0226 0.0220 0.0237 0.0222 -4.10 -0.169 0.0168 0.0171 0.0158 0.0166 0.0175 -3.04 -0.071 0.0132 0.0143 0.0134 0.0107 0.0144 -1.96 0.025 0.0101 0.0100 0.0093 0.0100 0.0112 -0.77 0.135 0.0083 0.0082 0.0080 0.0085 0.0085 0.21 0.266 0.0075 0.0075 0.0077 0.0072 0.0078 1.26 0.376 0.0076 0.0076 0.0078 0.0077 0.0075 2.16 0.470 0.0082 0.0079 0.0082 0.0088 0.0078 2.86 0.538 0.0087 0.0087 0.0087 0.0090 0.0085 4.35 0.689 0.0106 0.0108 0.0107 0.0108 0.0103 5.19 0.774 0.0119 0.0120 0.0121 0.0118 0.0116 6.17 0.870 0.0135 0.0133 0.0135 0.0134 0.0139 7.29 0.970 0.0156 0.0152 0.0148 0.0166 0.0156 8.34 1.030 0.0217 0.0215 0.0209 0.0223 0.0222 9.35 1.078 0.0265 0.0261 0.0256 0.0271 0.0272 10.23 1.110 0.0325 0.0323 0.0315 0.0327 0.0335 11.26 1.128 0.0432 0.0433 0.0442 0.0439 0.0415 Tabulated from data in file ag02594.dat & reduced using program C06.01 File sd7080.drg created using program C06.01 on Mon Feb 02 15:11:43 1998