Airfoil: E387 (E) 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 #: 100062 Number of angles of attack: 18 alpha / Cl / Cd / Spanwise Cd's >>> -6.21 -0.338 0.0754 0.0796 0.0762 0.0755 0.0731 0.0712 0.0732 0.0750 0.0797 -5.25 -0.262 0.0495 0.0516 0.0510 0.0502 0.0481 0.0457 0.0482 0.0493 0.0523 -4.17 -0.111 0.0276 0.0279 0.0270 0.0264 0.0281 0.0266 0.0271 0.0262 0.0317 -3.18 0.034 0.0218 0.0232 0.0231 0.0205 0.0210 0.0202 0.0213 0.0219 0.0231 -2.10 0.187 0.0197 0.0217 0.0203 0.0207 0.0190 0.0181 0.0182 0.0189 0.0202 -1.07 0.280 0.0178 0.0206 0.0171 0.0167 0.0173 0.0175 0.0171 0.0173 0.0187 -0.05 0.381 0.0205 0.0217 0.0202 0.0201 0.0202 0.0208 0.0200 0.0200 0.0210 0.93 0.474 0.0229 0.0232 0.0224 0.0224 0.0225 0.0235 0.0226 0.0226 0.0237 1.97 0.583 0.0235 0.0240 0.0240 0.0236 0.0240 0.0229 0.0227 0.0232 0.0235 3.05 0.688 0.0220 0.0229 0.0226 0.0221 0.0223 0.0212 0.0207 0.0213 0.0227 4.05 0.785 0.0198 0.0208 0.0201 0.0200 0.0201 0.0190 0.0191 0.0186 0.0208 5.10 0.885 0.0190 0.0205 0.0199 0.0186 0.0190 0.0157 0.0195 0.0179 0.0206 6.06 0.981 0.0186 0.0192 0.0206 0.0185 0.0176 0.0165 0.0206 0.0162 0.0198 7.14 1.075 0.0193 0.0193 0.0202 0.0195 0.0192 0.0186 0.0199 0.0179 0.0197 8.13 1.136 0.0253 0.0256 0.0258 0.0253 0.0244 0.0258 0.0259 0.0245 0.0250 9.15 1.183 0.0300 0.0308 0.0293 0.0300 0.0292 0.0297 0.0301 0.0301 0.0305 10.16 1.220 0.0381 0.0405 0.0401 0.0387 0.0378 0.0379 0.0372 0.0360 0.0366 11.14 1.228 0.0510 0.0511 0.0518 0.0525 0.0528 0.0540 0.0508 0.0474 0.0477 Tabulated from data in file bm04989.dat & reduced using program C10.20 Average Reynolds #: 199800 Number of angles of attack: 19 alpha / Cl / Cd / Spanwise Cd's >>> -6.22 -0.346 0.0754 0.0786 0.0768 0.0747 0.0727 0.0713 0.0725 0.0759 0.0803 -5.18 -0.150 0.0370 0.0378 0.0385 0.0372 0.0376 0.0341 0.0350 0.0373 0.0383 -4.17 -0.026 0.0180 0.0189 0.0182 0.0173 0.0183 0.0169 0.0172 0.0184 0.0188 -3.15 0.062 0.0154 0.0158 0.0154 0.0148 0.0159 0.0144 0.0150 0.0156 0.0163 -2.12 0.162 0.0130 0.0136 0.0127 0.0125 0.0131 0.0127 0.0125 0.0122 0.0143 -1.09 0.263 0.0124 0.0126 0.0123 0.0126 0.0122 0.0124 0.0122 0.0101 0.0149 -0.02 0.369 0.0113 0.0099 0.0153 0.0104 0.0103 0.0106 0.0119 0.0088 0.0128 0.96 0.465 0.0102 0.0090 0.0140 0.0099 0.0097 0.0097 0.0101 0.0093 0.0102 1.96 0.558 0.0115 0.0110 0.0115 0.0115 0.0124 0.0123 0.0107 0.0113 0.0114 3.00 0.646 0.0131 0.0125 0.0133 0.0135 0.0133 0.0140 0.0128 0.0123 0.0131 4.00 0.748 0.0149 0.0144 0.0147 0.0152 0.0152 0.0155 0.0146 0.0145 0.0147 5.03 0.842 0.0166 0.0161 0.0160 0.0169 0.0173 0.0169 0.0168 0.0162 0.0164 6.09 0.937 0.0186 0.0182 0.0180 0.0187 0.0190 0.0187 0.0190 0.0183 0.0192 7.10 1.030 0.0204 0.0203 0.0198 0.0200 0.0206 0.0206 0.0207 0.0201 0.0214 8.12 1.117 0.0227 0.0217 0.0221 0.0215 0.0230 0.0231 0.0230 0.0226 0.0242 9.12 1.194 0.0258 0.0251 0.0253 0.0244 0.0256 0.0262 0.0264 0.0258 0.0273 10.13 1.237 0.0320 0.0330 0.0335 0.0311 0.0313 0.0327 0.0319 0.0307 0.0315 11.13 1.228 0.0503 0.0404 0.0415 0.0434 0.0536 0.0686 0.0654 0.0507 0.0385 12.17 1.215 0.0733 0.0520 0.0544 0.0616 0.0782 0.0924 0.0966 0.0851 0.0659 Tabulated from data in file bm04991.dat & reduced using program C10.20 Average Reynolds #: 349749 Number of angles of attack: 19 alpha / Cl / Cd / Spanwise Cd's >>> -6.28 -0.311 0.0700 0.0729 0.0703 0.0686 0.0691 0.0678 0.0688 0.0699 0.0727 -5.26 -0.161 0.0378 0.0397 0.0383 0.0391 0.0365 0.0353 0.0358 0.0383 0.0392 -4.19 -0.044 0.0162 0.0171 0.0168 0.0161 0.0162 0.0150 0.0154 0.0167 0.0165 -3.12 0.063 0.0123 0.0130 0.0133 0.0116 0.0125 0.0109 0.0117 0.0119 0.0138 -2.13 0.163 0.0112 0.0108 0.0128 0.0104 0.0117 0.0107 0.0111 0.0105 0.0112 -1.09 0.262 0.0113 0.0107 0.0112 0.0113 0.0121 0.0111 0.0109 0.0118 0.0112 -0.09 0.364 0.0122 0.0117 0.0124 0.0125 0.0117 0.0126 0.0124 0.0123 0.0123 0.97 0.464 0.0127 0.0122 0.0129 0.0130 0.0126 0.0131 0.0126 0.0127 0.0128 2.00 0.569 0.0136 0.0131 0.0138 0.0136 0.0137 0.0140 0.0134 0.0134 0.0139 2.98 0.677 0.0146 0.0141 0.0146 0.0147 0.0148 0.0152 0.0142 0.0141 0.0149 4.04 0.777 0.0156 0.0152 0.0154 0.0161 0.0159 0.0163 0.0153 0.0148 0.0158 5.02 0.876 0.0168 0.0167 0.0164 0.0175 0.0172 0.0171 0.0168 0.0160 0.0169 6.09 0.972 0.0176 0.0168 0.0167 0.0183 0.0186 0.0178 0.0179 0.0169 0.0179 7.14 1.065 0.0187 0.0187 0.0175 0.0185 0.0190 0.0186 0.0194 0.0183 0.0194 8.11 1.150 0.0208 0.0204 0.0197 0.0199 0.0211 0.0212 0.0210 0.0209 0.0221 9.14 1.227 0.0235 0.0231 0.0231 0.0224 0.0231 0.0245 0.0236 0.0233 0.0249 10.13 1.272 0.0292 0.0283 0.0283 0.0269 0.0283 0.0306 0.0302 0.0298 0.0310 11.17 1.277 0.0462 0.0286 0.0277 0.0286 0.0336 0.0477 0.0673 0.0735 0.0622 12.15 1.264 0.0643 0.0502 0.0406 0.0388 0.0411 0.0552 0.0819 0.1011 0.1054 Tabulated from data in file bm04993.dat & reduced using program C10.20 Average Reynolds #: 500060 Number of angles of attack: 19 alpha / Cl / Cd / Spanwise Cd's >>> -6.22 -0.295 0.0674 0.0686 0.0678 0.0681 0.0657 0.0644 0.0654 0.0685 0.0710 -5.20 -0.160 0.0363 0.0368 0.0365 0.0375 0.0353 0.0341 0.0350 0.0368 0.0384 -4.19 -0.047 0.0147 0.0154 0.0150 0.0147 0.0149 0.0137 0.0140 0.0155 0.0142 -3.20 0.047 0.0124 0.0125 0.0125 0.0118 0.0138 0.0117 0.0120 0.0130 0.0119 -2.16 0.155 0.0111 0.0110 0.0116 0.0113 0.0118 0.0106 0.0105 0.0110 0.0111 -1.12 0.261 0.0112 0.0110 0.0112 0.0111 0.0115 0.0116 0.0111 0.0110 0.0114 -0.08 0.374 0.0119 0.0113 0.0118 0.0122 0.0117 0.0122 0.0120 0.0120 0.0122 0.95 0.478 0.0124 0.0117 0.0124 0.0126 0.0121 0.0127 0.0124 0.0126 0.0126 1.98 0.582 0.0129 0.0125 0.0131 0.0128 0.0128 0.0133 0.0128 0.0129 0.0132 2.99 0.688 0.0136 0.0132 0.0136 0.0136 0.0140 0.0141 0.0133 0.0131 0.0140 4.04 0.794 0.0147 0.0143 0.0144 0.0151 0.0151 0.0153 0.0144 0.0138 0.0149 5.06 0.894 0.0159 0.0155 0.0153 0.0164 0.0163 0.0164 0.0160 0.0150 0.0161 6.08 0.986 0.0172 0.0173 0.0165 0.0174 0.0175 0.0174 0.0177 0.0166 0.0176 7.11 1.076 0.0189 0.0187 0.0177 0.0188 0.0191 0.0191 0.0195 0.0185 0.0195 8.09 1.162 0.0207 0.0200 0.0193 0.0200 0.0212 0.0210 0.0211 0.0204 0.0224 9.16 1.228 0.0231 0.0219 0.0219 0.0220 0.0239 0.0244 0.0234 0.0231 0.0241 10.16 1.242 0.0342 0.0233 0.0240 0.0272 0.0425 0.0528 0.0429 0.0316 0.0291 11.16 1.234 0.0585 0.0310 0.0298 0.0354 0.0587 0.0818 0.0906 0.0818 0.0589 12.12 1.227 0.0809 0.0446 0.0481 0.0617 0.0833 0.0997 0.1089 0.1065 0.0946 Tabulated from data in file bm04995.dat & reduced using program C10.20 File e387_tf.drg created using program C10.20 on Thu May 22 17:01:34 2003