Airfoil: SD7037 (D) Builder: H. Stokely / B. Williams Comment: clean Number of Reynolds #'s: 4 Average Reynolds #: 59200 Number of angles of attack: 16 alpha / Cl / Cd / Spanwise Cd's >>> -5.06 -0.258 0.0409 0.0390 0.0392 0.0386 0.0466 -4.02 -0.182 0.0271 0.0262 0.0277 0.0250 0.0294 -2.94 -0.099 0.0208 0.0223 0.0198 0.0203 0.0209 -1.97 -0.023 0.0162 0.0168 0.0155 0.0168 0.0158 -0.95 0.074 0.0200 0.0190 0.0197 0.0185 0.0228 0.13 0.181 0.0173 0.0193 0.0124 0.0170 0.0205 1.15 0.334 0.0262 0.0330 0.0236 0.0213 0.0270 2.19 0.490 0.0307 0.0391 0.0265 0.0283 0.0288 3.18 0.610 0.0279 0.0363 0.0256 0.0230 0.0267 4.26 0.703 0.0279 0.0329 0.0240 0.0265 0.0284 5.29 0.789 0.0301 0.0288 0.0330 0.0248 0.0339 6.31 0.883 0.0355 0.0397 0.0319 0.0365 0.0339 7.26 0.961 0.0374 0.0454 0.0307 0.0363 0.0371 8.28 1.036 0.0370 0.0418 0.0287 0.0406 0.0370 9.33 1.112 0.0397 0.0398 0.0401 0.0362 0.0426 10.31 1.167 0.0464 0.0565 0.0457 0.0413 0.0421 Tabulated from data in file AB01100.DAT & reduced using program Q05.01D Average Reynolds #: 98500 Number of angles of attack: 16 alpha / Cl / Cd / Spanwise Cd's >>> -5.07 -0.326 0.0316 0.0337 0.0323 0.0286 0.0316 -3.99 -0.237 0.0222 0.0222 0.0221 0.0217 0.0228 -2.94 -0.132 0.0181 0.0174 0.0175 0.0177 0.0197 -2.00 -0.022 0.0153 0.0140 0.0153 0.0146 0.0171 -0.97 0.117 0.0147 0.0158 0.0143 0.0141 0.0149 0.04 0.280 0.0158 0.0165 0.0157 0.0155 0.0157 1.10 0.419 0.0165 0.0186 0.0163 0.0159 0.0151 2.29 0.530 0.0166 0.0173 0.0165 0.0161 0.0163 3.27 0.618 0.0164 0.0169 0.0178 0.0154 0.0157 4.15 0.693 0.0160 0.0167 0.0161 0.0158 0.0153 5.33 0.799 0.0173 0.0163 0.0176 0.0192 0.0160 6.21 0.875 0.0188 0.0190 0.0202 0.0184 0.0176 7.32 0.974 0.0211 0.0215 0.0213 0.0216 0.0198 8.19 1.054 0.0237 0.0253 0.0232 0.0256 0.0206 9.39 1.138 0.0286 0.0302 0.0276 0.0286 0.0280 10.40 1.188 0.0339 0.0352 0.0353 0.0320 0.0329 Tabulated from data in file AB01102.DAT & reduced using program Q05.01D Average Reynolds #: 196600 Number of angles of attack: 16 alpha / Cl / Cd / Spanwise Cd's >>> -4.72 -0.247 0.0209 0.0251 0.0201 0.0189 0.0193 -4.07 -0.174 0.0180 0.0183 0.0176 0.0168 0.0193 -2.96 -0.007 0.0132 0.0138 0.0136 0.0127 0.0126 -1.64 0.130 0.0101 0.0105 0.0093 0.0098 0.0107 -0.99 0.189 0.0095 0.0101 0.0082 0.0100 0.0097 0.21 0.299 0.0096 0.0082 0.0097 0.0118 0.0088 1.11 0.400 0.0094 0.0075 0.0099 0.0101 0.0102 2.22 0.529 0.0092 0.0092 0.0090 0.0089 0.0098 3.32 0.661 0.0103 0.0101 0.0108 0.0095 0.0108 4.14 0.744 0.0114 0.0111 0.0115 0.0110 0.0119 5.29 0.853 0.0130 0.0125 0.0125 0.0130 0.0139 6.33 0.949 0.0147 0.0144 0.0142 0.0149 0.0152 7.24 1.031 0.0167 0.0162 0.0166 0.0164 0.0176 8.18 1.113 0.0188 0.0186 0.0190 0.0186 0.0191 9.31 1.194 0.0223 0.0215 0.0227 0.0220 0.0231 10.32 1.246 0.0275 0.0277 0.0280 0.0268 0.0275 Tabulated from data in file PG01104.DAT & reduced using program Q05.01D Average Reynolds #: 295100 Number of angles of attack: 16 alpha / Cl / Cd / Spanwise Cd's >>> -5.09 -0.251 0.0207 0.0225 0.0199 0.0207 0.0197 -3.95 -0.113 0.0143 0.0152 0.0138 0.0122 0.0162 -3.00 -0.008 0.0118 0.0129 0.0115 0.0104 0.0125 -1.92 0.087 0.0096 0.0106 0.0090 0.0091 0.0097 -0.90 0.198 0.0080 0.0085 0.0071 0.0074 0.0090 0.17 0.323 0.0071 0.0062 0.0060 0.0077 0.0086 1.23 0.443 0.0074 0.0068 0.0066 0.0078 0.0083 2.33 0.564 0.0079 0.0075 0.0078 0.0077 0.0085 3.30 0.668 0.0090 0.0084 0.0092 0.0088 0.0096 4.46 0.789 0.0104 0.0097 0.0105 0.0102 0.0111 5.48 0.895 0.0118 0.0110 0.0117 0.0114 0.0130 6.63 1.010 0.0134 0.0131 0.0134 0.0128 0.0143 7.21 1.062 0.0145 0.0141 0.0143 0.0144 0.0152 8.25 1.148 0.0169 0.0164 0.0169 0.0168 0.0174 9.45 1.238 0.0210 0.0206 0.0213 0.0211 0.0210 10.30 1.281 0.0261 0.0257 0.0273 0.0272 0.0244 Tabulated from data in file PG01106.DAT & reduced using program Q05.01D File SD7037D.DRG created on 09-12-1997 at 13:39:50 using program FORMAT