Airfoil: E387 (E) Builder: Y. Tinel Comment: clean Number of Reynolds #'s: 6 Average Reynolds #: 100029 Number of angles of attack: 17 alpha / Cl / Cd / Spanwise Cd's >>> -5.25 -0.292 0.0472 0.0473 0.0450 0.0419 0.0435 0.0447 0.0489 0.0498 0.0568 -4.24 -0.156 0.0293 0.0270 0.0302 0.0268 0.0279 0.0289 0.0288 0.0304 0.0343 -3.12 -0.001 0.0220 0.0228 0.0226 0.0211 0.0192 0.0190 0.0211 0.0242 0.0258 -2.13 0.139 0.0187 0.0201 0.0188 0.0187 0.0187 0.0173 0.0165 0.0187 0.0207 -1.11 0.238 0.0174 0.0197 0.0173 0.0168 0.0163 0.0158 0.0163 0.0172 0.0196 -0.08 0.339 0.0202 0.0216 0.0201 0.0196 0.0194 0.0199 0.0203 0.0198 0.0208 0.95 0.435 0.0229 0.0226 0.0226 0.0218 0.0222 0.0234 0.0231 0.0235 0.0237 1.96 0.530 0.0266 0.0273 0.0265 0.0263 0.0269 0.0268 0.0267 0.0262 0.0261 3.00 0.623 0.0290 0.0296 0.0287 0.0287 0.0281 0.0297 0.0289 0.0288 0.0299 4.00 0.715 0.0317 0.0318 0.0319 0.0311 0.0324 0.0323 0.0318 0.0311 0.0316 5.04 0.825 0.0278 0.0279 0.0277 0.0278 0.0278 0.0286 0.0282 0.0269 0.0277 6.04 0.928 0.0239 0.0242 0.0239 0.0240 0.0242 0.0241 0.0237 0.0239 0.0235 7.07 1.032 0.0218 0.0207 0.0217 0.0211 0.0221 0.0224 0.0215 0.0223 0.0228 8.11 1.130 0.0215 0.0216 0.0210 0.0225 0.0209 0.0200 0.0192 0.0226 0.0239 9.17 1.176 0.0269 0.0263 0.0276 0.0269 0.0268 0.0265 0.0271 0.0263 0.0274 10.11 1.185 0.0363 0.0387 0.0389 0.0377 0.0357 0.0351 0.0342 0.0336 0.0367 11.14 1.188 0.0526 0.0493 0.0507 0.0513 0.0539 0.0558 0.0567 0.0522 0.0506 Tabulated from data in file bm05141.dat & reduced using program C10.20 Average Reynolds #: 199879 Number of angles of attack: 19 alpha / Cl / Cd / Spanwise Cd's >>> -6.24 -0.332 0.0705 0.0738 0.0708 0.0709 0.0695 0.0668 0.0685 0.0697 0.0736 -5.20 -0.138 0.0352 0.0359 0.0365 0.0350 0.0364 0.0326 0.0332 0.0354 0.0368 -4.17 -0.015 0.0192 0.0203 0.0198 0.0185 0.0192 0.0181 0.0184 0.0194 0.0196 -3.14 0.081 0.0150 0.0156 0.0152 0.0144 0.0157 0.0141 0.0145 0.0152 0.0156 -2.14 0.178 0.0125 0.0130 0.0125 0.0119 0.0126 0.0124 0.0119 0.0124 0.0134 -1.09 0.271 0.0102 0.0105 0.0106 0.0102 0.0096 0.0106 0.0096 0.0097 0.0109 -0.05 0.381 0.0104 0.0104 0.0103 0.0103 0.0103 0.0111 0.0101 0.0102 0.0105 0.97 0.483 0.0110 0.0108 0.0109 0.0108 0.0110 0.0118 0.0109 0.0107 0.0109 2.01 0.593 0.0118 0.0116 0.0118 0.0114 0.0120 0.0126 0.0116 0.0114 0.0117 3.00 0.698 0.0126 0.0122 0.0125 0.0124 0.0131 0.0134 0.0125 0.0124 0.0127 4.09 0.806 0.0134 0.0127 0.0133 0.0132 0.0141 0.0139 0.0136 0.0132 0.0135 5.02 0.902 0.0138 0.0133 0.0135 0.0138 0.0144 0.0138 0.0138 0.0136 0.0139 6.09 1.017 0.0140 0.0136 0.0135 0.0138 0.0143 0.0140 0.0144 0.0141 0.0145 7.14 1.119 0.0149 0.0148 0.0138 0.0139 0.0145 0.0151 0.0150 0.0157 0.0163 8.15 1.191 0.0181 0.0179 0.0176 0.0171 0.0185 0.0184 0.0186 0.0177 0.0187 9.18 1.226 0.0265 0.0275 0.0289 0.0253 0.0253 0.0265 0.0266 0.0256 0.0266 10.12 1.234 0.0358 0.0356 0.0366 0.0352 0.0361 0.0394 0.0362 0.0334 0.0338 11.18 1.227 0.0550 0.0416 0.0428 0.0452 0.0572 0.0731 0.0754 0.0600 0.0447 12.20 1.218 0.0774 0.0546 0.0575 0.0642 0.0778 0.0931 0.1007 0.0932 0.0779 Tabulated from data in file bm04979.dat & reduced using program C10.20 Average Reynolds #: 300289 Number of angles of attack: 19 alpha / Cl / Cd / Spanwise Cd's >>> -6.25 -0.304 0.0669 0.0688 0.0678 0.0671 0.0652 0.0658 0.0665 0.0648 0.0691 -5.21 -0.139 0.0341 0.0357 0.0351 0.0346 0.0335 0.0321 0.0325 0.0336 0.0359 -4.18 -0.028 0.0169 0.0178 0.0174 0.0165 0.0168 0.0159 0.0161 0.0173 0.0172 -3.20 0.064 0.0131 0.0136 0.0134 0.0125 0.0139 0.0124 0.0130 0.0133 0.0129 -2.07 0.184 0.0110 0.0111 0.0111 0.0104 0.0114 0.0107 0.0108 0.0111 0.0115 -1.11 0.288 0.0092 0.0091 0.0091 0.0089 0.0088 0.0091 0.0090 0.0091 0.0101 -0.04 0.393 0.0083 0.0081 0.0081 0.0083 0.0082 0.0086 0.0082 0.0083 0.0086 1.02 0.502 0.0088 0.0084 0.0086 0.0088 0.0087 0.0092 0.0088 0.0089 0.0088 1.96 0.610 0.0092 0.0090 0.0092 0.0089 0.0093 0.0098 0.0091 0.0089 0.0093 3.02 0.714 0.0098 0.0096 0.0098 0.0099 0.0102 0.0104 0.0096 0.0094 0.0099 4.00 0.817 0.0105 0.0101 0.0102 0.0107 0.0109 0.0111 0.0106 0.0100 0.0103 5.06 0.935 0.0112 0.0110 0.0107 0.0114 0.0117 0.0113 0.0117 0.0107 0.0110 6.11 1.041 0.0115 0.0112 0.0107 0.0113 0.0117 0.0115 0.0126 0.0116 0.0118 7.15 1.135 0.0131 0.0128 0.0122 0.0128 0.0132 0.0125 0.0140 0.0129 0.0140 8.14 1.201 0.0176 0.0175 0.0175 0.0169 0.0178 0.0177 0.0179 0.0174 0.0184 9.15 1.241 0.0246 0.0262 0.0267 0.0234 0.0239 0.0245 0.0244 0.0232 0.0241 10.12 1.250 0.0343 0.0327 0.0344 0.0323 0.0366 0.0412 0.0362 0.0301 0.0310 11.16 1.245 0.0537 0.0410 0.0401 0.0405 0.0516 0.0692 0.0756 0.0652 0.0466 12.17 1.236 0.0774 0.0586 0.0581 0.0633 0.0763 0.0890 0.0978 0.0964 0.0797 Tabulated from data in file bm04981.dat & reduced using program C10.20 Average Reynolds #: 349865 Number of angles of attack: 19 alpha / Cl / Cd / Spanwise Cd's >>> -6.25 -0.288 0.0647 0.0674 0.0654 0.0632 0.0624 0.0621 0.0637 0.0643 0.0688 -5.18 -0.144 0.0337 0.0347 0.0341 0.0337 0.0330 0.0317 0.0324 0.0343 0.0358 -4.19 -0.038 0.0164 0.0173 0.0169 0.0161 0.0164 0.0154 0.0155 0.0171 0.0169 -3.15 0.071 0.0123 0.0124 0.0124 0.0116 0.0130 0.0116 0.0123 0.0126 0.0122 -2.11 0.180 0.0106 0.0107 0.0106 0.0100 0.0111 0.0103 0.0105 0.0109 0.0110 -1.16 0.277 0.0090 0.0088 0.0088 0.0089 0.0087 0.0089 0.0089 0.0090 0.0097 -0.05 0.389 0.0078 0.0074 0.0076 0.0079 0.0075 0.0080 0.0079 0.0079 0.0082 0.94 0.493 0.0081 0.0078 0.0080 0.0082 0.0079 0.0085 0.0081 0.0083 0.0082 1.97 0.605 0.0085 0.0082 0.0086 0.0084 0.0086 0.0089 0.0084 0.0085 0.0086 3.00 0.714 0.0091 0.0090 0.0091 0.0091 0.0094 0.0096 0.0090 0.0086 0.0092 4.03 0.833 0.0098 0.0096 0.0096 0.0101 0.0101 0.0103 0.0100 0.0095 0.0095 5.08 0.942 0.0104 0.0103 0.0099 0.0104 0.0109 0.0103 0.0111 0.0101 0.0101 6.08 1.045 0.0111 0.0112 0.0101 0.0111 0.0113 0.0108 0.0121 0.0107 0.0114 7.08 1.134 0.0128 0.0127 0.0123 0.0127 0.0131 0.0124 0.0137 0.0124 0.0135 8.11 1.200 0.0177 0.0182 0.0181 0.0168 0.0176 0.0175 0.0179 0.0172 0.0183 9.11 1.240 0.0238 0.0255 0.0258 0.0230 0.0231 0.0238 0.0235 0.0225 0.0235 10.14 1.249 0.0347 0.0336 0.0344 0.0336 0.0373 0.0424 0.0361 0.0297 0.0303 11.15 1.245 0.0564 0.0411 0.0414 0.0419 0.0558 0.0745 0.0801 0.0685 0.0478 12.14 1.238 0.0781 0.0554 0.0569 0.0638 0.0811 0.0977 0.1003 0.0934 0.0761 Tabulated from data in file bm04983.dat & reduced using program C10.20 Average Reynolds #: 459961 Number of angles of attack: 19 alpha / Cl / Cd / Spanwise Cd's >>> -6.23 -0.292 0.0651 0.0677 0.0665 0.0645 0.0622 0.0618 0.0640 0.0659 0.0683 -5.20 -0.150 0.0341 0.0349 0.0346 0.0347 0.0334 0.0322 0.0324 0.0343 0.0361 -4.16 -0.040 0.0145 0.0148 0.0147 0.0144 0.0147 0.0134 0.0139 0.0152 0.0146 -3.13 0.064 0.0114 0.0113 0.0115 0.0110 0.0121 0.0109 0.0114 0.0115 0.0112 -2.13 0.172 0.0099 0.0097 0.0099 0.0097 0.0104 0.0095 0.0098 0.0102 0.0101 -1.08 0.280 0.0085 0.0085 0.0084 0.0084 0.0083 0.0086 0.0085 0.0087 0.0090 -0.09 0.382 0.0069 0.0066 0.0068 0.0070 0.0065 0.0068 0.0068 0.0069 0.0074 0.96 0.500 0.0072 0.0067 0.0072 0.0073 0.0071 0.0074 0.0071 0.0074 0.0073 1.98 0.611 0.0075 0.0073 0.0077 0.0074 0.0076 0.0078 0.0074 0.0075 0.0076 3.00 0.721 0.0079 0.0077 0.0080 0.0079 0.0082 0.0083 0.0078 0.0075 0.0080 4.03 0.835 0.0087 0.0084 0.0085 0.0089 0.0089 0.0092 0.0088 0.0082 0.0084 5.12 0.948 0.0094 0.0093 0.0091 0.0093 0.0096 0.0096 0.0101 0.0089 0.0093 6.09 1.045 0.0101 0.0101 0.0095 0.0103 0.0102 0.0097 0.0108 0.0095 0.0104 7.15 1.132 0.0128 0.0127 0.0123 0.0125 0.0132 0.0127 0.0135 0.0126 0.0131 8.18 1.195 0.0172 0.0176 0.0173 0.0164 0.0173 0.0170 0.0173 0.0168 0.0177 9.12 1.236 0.0224 0.0228 0.0236 0.0212 0.0221 0.0229 0.0222 0.0214 0.0227 10.14 1.255 0.0318 0.0296 0.0319 0.0309 0.0338 0.0391 0.0345 0.0272 0.0278 11.12 1.252 0.0543 0.0341 0.0345 0.0383 0.0589 0.0800 0.0811 0.0655 0.0419 12.16 1.242 0.0790 0.0439 0.0508 0.0672 0.0883 0.1035 0.1058 0.0946 0.0783 Tabulated from data in file bm04985.dat & reduced using program C10.20 Average Reynolds #: 500094 Number of angles of attack: 19 alpha / Cl / Cd / Spanwise Cd's >>> -6.20 -0.289 0.0643 0.0664 0.0651 0.0652 0.0649 0.0626 0.0611 0.0619 0.0675 -5.18 -0.155 0.0352 0.0359 0.0353 0.0353 0.0346 0.0334 0.0336 0.0354 0.0378 -4.15 -0.040 0.0139 0.0141 0.0141 0.0139 0.0142 0.0131 0.0132 0.0147 0.0140 -3.20 0.056 0.0114 0.0115 0.0114 0.0111 0.0122 0.0109 0.0112 0.0115 0.0111 -2.16 0.171 0.0097 0.0095 0.0097 0.0092 0.0101 0.0093 0.0096 0.0099 0.0100 -1.09 0.276 0.0085 0.0084 0.0083 0.0083 0.0083 0.0085 0.0084 0.0086 0.0088 -0.04 0.388 0.0067 0.0064 0.0066 0.0068 0.0063 0.0067 0.0066 0.0068 0.0072 0.88 0.497 0.0068 0.0063 0.0069 0.0070 0.0066 0.0070 0.0068 0.0071 0.0070 1.97 0.613 0.0072 0.0069 0.0073 0.0070 0.0072 0.0075 0.0071 0.0072 0.0073 2.98 0.720 0.0077 0.0077 0.0078 0.0077 0.0080 0.0081 0.0076 0.0071 0.0079 4.02 0.833 0.0084 0.0082 0.0084 0.0087 0.0088 0.0088 0.0084 0.0078 0.0082 5.08 0.941 0.0091 0.0089 0.0089 0.0091 0.0094 0.0093 0.0096 0.0086 0.0089 6.11 1.047 0.0099 0.0098 0.0095 0.0101 0.0100 0.0097 0.0105 0.0094 0.0100 7.15 1.129 0.0128 0.0126 0.0121 0.0127 0.0131 0.0127 0.0135 0.0126 0.0131 8.14 1.195 0.0169 0.0173 0.0170 0.0162 0.0170 0.0167 0.0172 0.0167 0.0174 9.14 1.244 0.0226 0.0231 0.0236 0.0213 0.0223 0.0231 0.0223 0.0218 0.0230 10.09 1.259 0.0300 0.0295 0.0325 0.0293 0.0309 0.0347 0.0300 0.0260 0.0267 11.17 1.257 0.0548 0.0344 0.0343 0.0383 0.0569 0.0780 0.0820 0.0696 0.0449 12.13 1.248 0.0804 0.0457 0.0533 0.0718 0.0897 0.1028 0.1062 0.0955 0.0782 Tabulated from data in file bm04987.dat & reduced using program C10.20 File e387_c.drg created using program C10.20 on Thu May 22 17:01:34 2003