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
