Airfoil: FX 63-137 (C)
Builder: Y. Tinel
Comment: 'u.s.t. located at 2% chord, l.s.t. located at 5% chord' 

Number of Reynolds #'s:
5

Average Reynolds #:
100069
Number of angles of attack:
21
 alpha  /   Cl   /  Cd   /  Spanwise Cd's >>>
 -7.26   -0.323   0.1440  0.1399   0.1443   0.1444   0.1463   0.1473   0.1463   0.1426   0.1409
 -6.23   -0.301   0.1257  0.1288   0.1272   0.1258   0.1242   0.1256   0.1253   0.1230   0.1255
 -5.17   -0.025   0.0434  0.0463   0.0445   0.0446   0.0430   0.0414   0.0405   0.0433   0.0441
 -4.13    0.112   0.0368  0.0370   0.0374   0.0377   0.0367   0.0358   0.0371   0.0364   0.0362
 -3.07    0.258   0.0357  0.0361   0.0357   0.0361   0.0361   0.0351   0.0353   0.0362   0.0351
 -2.04    0.378   0.0362  0.0366   0.0364   0.0366   0.0371   0.0360   0.0362   0.0354   0.0356
 -1.00    0.473   0.0403  0.0410   0.0397   0.0405   0.0409   0.0407   0.0411   0.0398   0.0392
 -0.01    0.547   0.0456  0.0459   0.0456   0.0458   0.0467   0.0462   0.0451   0.0445   0.0452
  1.04    0.613   0.0532  0.0524   0.0524   0.0543   0.0542   0.0547   0.0532   0.0525   0.0518
  2.02    0.673   0.0592  0.0585   0.0590   0.0611   0.0602   0.0594   0.0606   0.0593   0.0552
  3.07    0.878   0.0405  0.0399   0.0401   0.0424   0.0401   0.0405   0.0389   0.0410   0.0409
  4.08    1.046   0.0283  0.0300   0.0282   0.0261   0.0271   0.0281   0.0276   0.0292   0.0298
  5.16    1.171   0.0246  0.0257   0.0253   0.0237   0.0231   0.0238   0.0243   0.0249   0.0259
  6.13    1.263   0.0235  0.0253   0.0261   0.0238   0.0195   0.0209   0.0236   0.0244   0.0243
  7.23    1.359   0.0242  0.0248   0.0274   0.0232   0.0234   0.0225   0.0265   0.0224   0.0233
  8.20    1.429   0.0260  0.0239   0.0286   0.0264   0.0267   0.0266   0.0284   0.0222   0.0250
  9.24    1.489   0.0295  0.0290   0.0296   0.0289   0.0314   0.0326   0.0288   0.0278   0.0278
 10.22    1.523   0.0350  0.0350   0.0341   0.0333   0.0399   0.0399   0.0337   0.0310   0.0331
 11.29    1.519   0.0505  0.0426   0.0414   0.0512   0.0726   0.0717   0.0497   0.0366   0.0377
 12.24    1.494   0.0744  0.0499   0.0599   0.0861   0.1089   0.1058   0.0884   0.0533   0.0427
 13.23    1.462   0.1096  0.0708   0.0982   0.1246   0.1472   0.1471   0.1244   0.0975   0.0668
Tabulated from data in file bm05007.dat & reduced using program C10.20

Average Reynolds #:
150199
Number of angles of attack:
21
 alpha  /   Cl   /  Cd   /  Spanwise Cd's >>>
 -7.20   -0.145   0.1164  0.1192   0.1188   0.1168   0.1136   0.1113   0.1133   0.1166   0.1213
 -6.13    0.037   0.0460  0.0486   0.0464   0.0455   0.0450   0.0433   0.0449   0.0464   0.0481
 -5.10    0.198   0.0281  0.0293   0.0282   0.0284   0.0286   0.0274   0.0273   0.0272   0.0285
 -4.08    0.330   0.0229  0.0236   0.0231   0.0228   0.0239   0.0222   0.0216   0.0232   0.0227
 -3.04    0.457   0.0205  0.0215   0.0207   0.0199   0.0212   0.0210   0.0191   0.0207   0.0195
 -2.02    0.573   0.0194  0.0198   0.0194   0.0195   0.0202   0.0195   0.0183   0.0199   0.0190
 -0.99    0.678   0.0197  0.0199   0.0196   0.0202   0.0206   0.0197   0.0185   0.0199   0.0191
 -0.01    0.774   0.0206  0.0206   0.0210   0.0210   0.0218   0.0202   0.0197   0.0205   0.0202
  1.05    0.880   0.0203  0.0218   0.0221   0.0208   0.0208   0.0185   0.0197   0.0177   0.0209
  2.11    0.988   0.0185  0.0211   0.0225   0.0175   0.0162   0.0147   0.0189   0.0155   0.0216
  3.11    1.079   0.0178  0.0144   0.0238   0.0157   0.0178   0.0160   0.0201   0.0157   0.0187
  4.12    1.169   0.0174  0.0163   0.0180   0.0160   0.0183   0.0171   0.0181   0.0178   0.0174
  5.16    1.243   0.0202  0.0212   0.0208   0.0202   0.0207   0.0207   0.0183   0.0192   0.0202
  6.18    1.313   0.0233  0.0233   0.0229   0.0217   0.0243   0.0236   0.0234   0.0235   0.0240
  7.19    1.366   0.0273  0.0282   0.0269   0.0262   0.0284   0.0291   0.0270   0.0254   0.0270
  8.20    1.413   0.0322  0.0337   0.0320   0.0314   0.0324   0.0345   0.0318   0.0307   0.0312
  9.21    1.443   0.0396  0.0417   0.0392   0.0392   0.0416   0.0454   0.0389   0.0351   0.0357
 10.23    1.465   0.0516  0.0525   0.0537   0.0540   0.0598   0.0629   0.0497   0.0395   0.0410
 11.22    1.476   0.0740  0.0588   0.0667   0.0814   0.0949   0.0986   0.0833   0.0612   0.0473
 12.23    1.484   0.0943  0.0786   0.0889   0.1032   0.1139   0.1130   0.1034   0.0866   0.0670
 13.22    1.486   0.1105  0.1047   0.1122   0.1129   0.1177   0.1182   0.1167   0.1091   0.0926
Tabulated from data in file bm05009.dat & reduced using program C10.20

Average Reynolds #:
199966
Number of angles of attack:
18
 alpha  /   Cl   /  Cd   /  Spanwise Cd's >>>
 -7.18   -0.079   0.0892  0.0898   0.0878   0.0868   0.0872   0.0876   0.0853   0.0908   0.0986
 -6.07    0.114   0.0287  0.0301   0.0291   0.0280   0.0291   0.0270   0.0277   0.0278   0.0310
 -5.10    0.235   0.0204  0.0210   0.0211   0.0206   0.0207   0.0197   0.0194   0.0195   0.0211
 -4.06    0.352   0.0169  0.0166   0.0180   0.0169   0.0169   0.0161   0.0164   0.0173   0.0171
 -3.00    0.462   0.0155  0.0158   0.0159   0.0153   0.0160   0.0159   0.0143   0.0160   0.0148
 -2.05    0.561   0.0152  0.0154   0.0155   0.0152   0.0159   0.0160   0.0144   0.0142   0.0149
 -1.00    0.670   0.0147  0.0155   0.0158   0.0152   0.0157   0.0141   0.0144   0.0123   0.0149
  0.08    0.787   0.0139  0.0120   0.0201   0.0129   0.0134   0.0122   0.0158   0.0106   0.0145
  1.06    0.883   0.0146  0.0125   0.0185   0.0154   0.0143   0.0141   0.0158   0.0134   0.0130
  2.13    0.971   0.0155  0.0138   0.0154   0.0170   0.0182   0.0153   0.0147   0.0145   0.0153
  3.11    1.040   0.0186  0.0186   0.0179   0.0188   0.0194   0.0182   0.0188   0.0184   0.0186
  4.12    1.119   0.0200  0.0199   0.0195   0.0193   0.0206   0.0202   0.0199   0.0206   0.0205
  5.13    1.197   0.0221  0.0218   0.0222   0.0213   0.0225   0.0225   0.0210   0.0235   0.0216
  6.16    1.263   0.0251  0.0257   0.0250   0.0241   0.0249   0.0257   0.0252   0.0248   0.0257
  7.17    1.325   0.0284  0.0291   0.0286   0.0274   0.0278   0.0294   0.0285   0.0275   0.0286
  8.17    1.376   0.0328  0.0341   0.0326   0.0316   0.0326   0.0361   0.0330   0.0314   0.0314
  9.23    1.413   0.0416  0.0385   0.0387   0.0397   0.0483   0.0543   0.0436   0.0352   0.0347
 10.20    1.437   0.0562  0.0452   0.0459   0.0522   0.0721   0.0809   0.0669   0.0463   0.0404
Tabulated from data in file bm05011.dat & reduced using program C10.20

Average Reynolds #:
350058
Number of angles of attack:
18
 alpha  /   Cl   /  Cd   /  Spanwise Cd's >>>
 -7.15   -0.033   0.0711  0.0717   0.0701   0.0697   0.0698   0.0682   0.0697   0.0715   0.0781
 -6.07    0.139   0.0158  0.0169   0.0171   0.0156   0.0166   0.0143   0.0155   0.0152   0.0151
 -5.09    0.248   0.0142  0.0143   0.0144   0.0145   0.0145   0.0138   0.0141   0.0138   0.0144
 -4.07    0.364   0.0121  0.0118   0.0127   0.0131   0.0123   0.0116   0.0123   0.0113   0.0121
 -3.05    0.479   0.0119  0.0125   0.0151   0.0115   0.0121   0.0109   0.0123   0.0100   0.0109
 -2.00    0.581   0.0115  0.0113   0.0134   0.0110   0.0124   0.0115   0.0116   0.0106   0.0106
 -1.00    0.666   0.0129  0.0124   0.0136   0.0145   0.0142   0.0127   0.0112   0.0121   0.0127
  0.03    0.759   0.0149  0.0148   0.0152   0.0159   0.0150   0.0154   0.0137   0.0144   0.0147
  1.07    0.855   0.0160  0.0158   0.0159   0.0171   0.0165   0.0162   0.0154   0.0152   0.0156
  2.11    0.950   0.0173  0.0173   0.0168   0.0182   0.0181   0.0170   0.0174   0.0169   0.0168
  3.12    1.042   0.0188  0.0188   0.0179   0.0190   0.0193   0.0186   0.0196   0.0186   0.0188
  4.13    1.129   0.0207  0.0208   0.0196   0.0205   0.0212   0.0204   0.0214   0.0206   0.0213
  5.14    1.205   0.0225  0.0228   0.0220   0.0217   0.0224   0.0227   0.0225   0.0223   0.0235
  6.16    1.289   0.0248  0.0255   0.0246   0.0234   0.0244   0.0255   0.0248   0.0244   0.0259
  7.19    1.348   0.0278  0.0287   0.0274   0.0269   0.0273   0.0296   0.0279   0.0270   0.0280
  8.19    1.388   0.0335  0.0333   0.0312   0.0319   0.0353   0.0403   0.0343   0.0311   0.0309
  9.23    1.422   0.0440  0.0412   0.0403   0.0408   0.0508   0.0586   0.0494   0.0358   0.0348
 10.22    1.448   0.0607  0.0480   0.0456   0.0555   0.0774   0.0863   0.0764   0.0565   0.0401
Tabulated from data in file bm05013.dat & reduced using program C10.20

Average Reynolds #:
499532
Number of angles of attack:
18
 alpha  /   Cl   /  Cd   /  Spanwise Cd's >>>
 -7.21   -0.027   0.0675  0.0682   0.0682   0.0667   0.0653   0.0649   0.0663   0.0663   0.0745
 -6.13    0.142   0.0144  0.0135   0.0144   0.0136   0.0158   0.0140   0.0148   0.0145   0.0146
 -5.09    0.260   0.0115  0.0108   0.0113   0.0112   0.0123   0.0112   0.0124   0.0112   0.0116
 -4.07    0.366   0.0111  0.0100   0.0118   0.0112   0.0119   0.0109   0.0112   0.0113   0.0105
 -3.09    0.463   0.0112  0.0106   0.0116   0.0119   0.0116   0.0111   0.0107   0.0116   0.0108
 -2.02    0.572   0.0121  0.0113   0.0124   0.0126   0.0130   0.0124   0.0116   0.0120   0.0115
 -0.99    0.667   0.0133  0.0128   0.0135   0.0138   0.0140   0.0138   0.0127   0.0126   0.0130
 -0.02    0.749   0.0145  0.0143   0.0144   0.0153   0.0151   0.0151   0.0140   0.0139   0.0142
  1.07    0.853   0.0158  0.0158   0.0154   0.0166   0.0161   0.0162   0.0157   0.0153   0.0154
  2.08    0.943   0.0171  0.0172   0.0164   0.0176   0.0175   0.0172   0.0174   0.0168   0.0165
  3.06    1.032   0.0183  0.0187   0.0174   0.0185   0.0186   0.0181   0.0191   0.0181   0.0180
  4.16    1.135   0.0201  0.0202   0.0192   0.0195   0.0204   0.0201   0.0208   0.0200   0.0205
  5.18    1.218   0.0221  0.0222   0.0216   0.0207   0.0218   0.0228   0.0224   0.0222   0.0232
  6.16    1.287   0.0248  0.0251   0.0243   0.0227   0.0238   0.0262   0.0249   0.0250   0.0263
  7.21    1.350   0.0294  0.0302   0.0284   0.0266   0.0278   0.0324   0.0310   0.0298   0.0292
  8.22    1.395   0.0362  0.0360   0.0330   0.0325   0.0376   0.0474   0.0407   0.0318   0.0310
  9.23    1.431   0.0486  0.0433   0.0408   0.0410   0.0564   0.0690   0.0623   0.0410   0.0352
 10.22    1.456   0.0667  0.0509   0.0488   0.0562   0.0775   0.0919   0.0892   0.0713   0.0481
Tabulated from data in file bm05015.dat & reduced using program C10.20

File fx63137_tf.drg created using program C10.20 on Thu May 22 17:01:35 2003
