Airfoil: FX 63-137 (C)
Builder: Y. Tinel
Comment: clean

Number of Reynolds #'s:
5

Average Reynolds #:
100019
Number of angles of attack:
61
 alpha  /   Cl   /  Cm
-10.08   -0.223  -0.0207
 -9.04   -0.260  -0.0079
 -8.07   -0.317   0.0005
 -7.08   -0.328  -0.0120
 -6.10   -0.304  -0.0281
 -5.11    0.013  -0.1463
 -4.14    0.134  -0.1707
 -3.12    0.263  -0.1764
 -2.04    0.391  -0.1885
 -1.05    0.466  -0.1694
 -0.07    0.530  -0.1616
  1.02    0.630  -0.1703
  2.00    0.655  -0.1568
  3.08    0.698  -0.1653
  4.06    0.864  -0.1704
  5.11    1.152  -0.1632
  6.16    1.304  -0.1706
  7.16    1.417  -0.1551
  8.18    1.520  -0.1672
  9.31    1.611  -0.1574
 10.26    1.677  -0.1448
 11.31    1.722  -0.1460
 12.29    1.739  -0.1430
 13.30    1.735  -0.1358
 14.31    1.731  -0.1302
 15.37    1.739  -0.1291
 16.28    1.733  -0.1309
 17.33    1.734  -0.1281
 17.99    1.193  -0.2612
 19.03    1.211  -0.2783
 20.03    1.244  -0.2839
 19.51    1.232  -0.2913
 18.54    1.175  -0.2749
 17.52    1.174  -0.2621
 16.56    1.159  -0.2469
 15.56    1.219  -0.2443
 14.54    1.214  -0.2313
 13.63    1.196  -0.2190
 12.86    1.734  -0.1363
 11.80    1.740  -0.1391
 10.74    1.698  -0.1583
  9.79    1.649  -0.1656
  8.72    1.565  -0.1545
  7.66    1.476  -0.1623
  6.70    1.371  -0.1589
  5.65    1.235  -0.1593
  4.54    0.883  -0.1620
  3.51    0.773  -0.1693
  2.52    0.692  -0.1652
  1.53    0.649  -0.1586
  0.48    0.587  -0.1638
 -0.53    0.520  -0.1691
 -1.54    0.453  -0.1731
 -2.61    0.358  -0.1728
 -3.65    0.216  -0.1659
 -4.64    0.096  -0.1569
 -5.64   -0.227  -0.0739
 -6.60   -0.318  -0.0198
 -7.61   -0.287  -0.0082
 -8.56   -0.266  -0.0064
 -9.55   -0.236  -0.0104
Tabulated from data in file bm04996.dat & reduced using program C10.20

Average Reynolds #:
150054
Number of angles of attack:
61
 alpha  /   Cl   /  Cm
-10.02   -0.224  -0.0149
 -9.02   -0.253  -0.0118
 -8.04   -0.241  -0.0309
 -7.11   -0.194  -0.0582
 -6.16    0.016  -0.1689
 -5.15    0.172  -0.1825
 -4.14    0.316  -0.1984
 -3.06    0.451  -0.2001
 -2.05    0.559  -0.1996
 -1.04    0.657  -0.1971
  0.02    0.749  -0.1933
  1.06    0.833  -0.1867
  2.02    0.925  -0.1795
  3.09    1.028  -0.1799
  4.10    1.121  -0.1724
  5.14    1.224  -0.1715
  6.15    1.331  -0.1747
  7.18    1.430  -0.1723
  8.21    1.516  -0.1679
  9.27    1.597  -0.1608
 10.26    1.662  -0.1555
 11.31    1.704  -0.1474
 12.30    1.708  -0.1360
 13.30    1.708  -0.1269
 14.28    1.709  -0.1210
 15.28    1.720  -0.1178
 16.33    1.714  -0.1162
 17.35    1.708  -0.1193
 18.25    1.686  -0.1308
 18.98    1.158  -0.2588
 20.01    1.176  -0.2662
 19.49    1.221  -0.2823
 18.50    1.165  -0.2659
 17.52    1.156  -0.2592
 16.56    1.177  -0.2537
 15.54    1.201  -0.2471
 14.56    1.206  -0.2329
 13.83    1.709  -0.1286
 12.76    1.706  -0.1347
 11.76    1.706  -0.1458
 10.75    1.686  -0.1560
  9.73    1.621  -0.1624
  8.74    1.560  -0.1669
  7.68    1.476  -0.1733
  6.67    1.387  -0.1747
  5.64    1.281  -0.1752
  4.59    1.169  -0.1753
  3.58    1.079  -0.1770
  2.57    0.981  -0.1796
  1.54    0.888  -0.1833
  0.49    0.795  -0.1880
 -0.52    0.701  -0.1956
 -1.57    0.607  -0.1975
 -2.57    0.512  -0.2011
 -3.57    0.395  -0.1999
 -4.61    0.258  -0.1943
 -5.64    0.109  -0.1819
 -6.66   -0.129  -0.0916
 -7.59   -0.209  -0.0380
 -8.58   -0.254  -0.0161
 -9.56   -0.230  -0.0110
Tabulated from data in file bm04998.dat & reduced using program C10.20

Average Reynolds #:
199952
Number of angles of attack:
61
 alpha  /   Cl   /  Cm
-10.07   -0.227  -0.0112
 -9.06   -0.244  -0.0195
 -8.05   -0.188  -0.0437
 -7.14   -0.102  -0.0862
 -6.18    0.093  -0.1836
 -5.13    0.225  -0.1906
 -4.06    0.340  -0.1955
 -3.07    0.452  -0.2006
 -2.10    0.559  -0.1988
 -1.08    0.660  -0.1984
  0.04    0.767  -0.1951
  1.03    0.863  -0.1920
  2.01    0.964  -0.1898
  3.08    1.070  -0.1869
  4.14    1.171  -0.1848
  5.15    1.257  -0.1801
  6.17    1.356  -0.1784
  7.16    1.452  -0.1756
  8.19    1.538  -0.1710
  9.23    1.621  -0.1656
 10.25    1.679  -0.1573
 11.34    1.715  -0.1470
 12.28    1.717  -0.1363
 13.28    1.722  -0.1290
 14.35    1.727  -0.1232
 15.36    1.735  -0.1207
 16.34    1.741  -0.1204
 17.35    1.746  -0.1225
 18.27    1.734  -0.1254
 19.31    1.736  -0.1368
 20.27    1.685  -0.1430
 19.79    1.692  -0.1398
 18.81    1.728  -0.1336
 17.79    1.741  -0.1279
 16.78    1.745  -0.1237
 15.80    1.735  -0.1235
 14.83    1.731  -0.1241
 13.77    1.720  -0.1278
 12.81    1.713  -0.1341
 11.78    1.719  -0.1448
 10.78    1.697  -0.1554
  9.76    1.650  -0.1643
  8.71    1.582  -0.1715
  7.71    1.503  -0.1761
  6.68    1.410  -0.1801
  5.67    1.310  -0.1809
  4.56    1.219  -0.1857
  3.55    1.122  -0.1888
  2.56    1.023  -0.1908
  1.55    0.921  -0.1928
  0.54    0.822  -0.1964
 -0.52    0.721  -0.1982
 -1.55    0.620  -0.2003
 -2.59    0.514  -0.2025
 -3.61    0.397  -0.1987
 -4.61    0.292  -0.1986
 -5.65    0.167  -0.1891
 -6.65    0.002  -0.1539
 -7.60   -0.143  -0.0576
 -8.58   -0.213  -0.0321
 -9.55   -0.226  -0.0205
Tabulated from data in file bm05000.dat & reduced using program C10.20

Average Reynolds #:
349860
Number of angles of attack:
61
 alpha  /   Cl   /  Cm
-10.05   -0.215  -0.0199
 -9.08   -0.194  -0.0370
 -8.15   -0.133  -0.0691
 -7.14   -0.036  -0.1323
 -6.12    0.129  -0.1869
 -5.09    0.251  -0.1940
 -4.15    0.352  -0.1956
 -3.07    0.483  -0.2009
 -2.08    0.598  -0.2045
 -1.05    0.704  -0.2027
  0.01    0.819  -0.2019
  1.04    0.922  -0.2004
  1.99    1.023  -0.1995
  3.09    1.129  -0.1964
  4.15    1.240  -0.1941
  5.13    1.327  -0.1903
  6.18    1.425  -0.1861
  7.19    1.509  -0.1804
  8.24    1.593  -0.1747
  9.26    1.647  -0.1662
 10.31    1.692  -0.1554
 11.28    1.717  -0.1453
 12.27    1.728  -0.1365
 13.28    1.741  -0.1298
 14.33    1.749  -0.1264
 15.29    1.762  -0.1253
 16.32    1.759  -0.1249
 17.30    1.765  -0.1280
 18.25    1.756  -0.1304
 19.28    1.741  -0.1347
 20.30    1.724  -0.1406
 19.77    1.726  -0.1389
 18.80    1.763  -0.1365
 17.80    1.754  -0.1294
 16.81    1.758  -0.1270
 15.80    1.763  -0.1257
 14.80    1.753  -0.1265
 13.81    1.738  -0.1286
 12.76    1.733  -0.1347
 11.74    1.723  -0.1433
 10.85    1.705  -0.1517
  9.74    1.669  -0.1622
  8.72    1.621  -0.1719
  7.68    1.547  -0.1786
  6.62    1.467  -0.1847
  5.65    1.385  -0.1905
  4.61    1.283  -0.1943
  3.63    1.188  -0.1966
  2.55    1.080  -0.1989
  1.57    0.969  -0.1995
  0.46    0.859  -0.2016
 -0.49    0.764  -0.2036
 -1.53    0.648  -0.2045
 -2.56    0.536  -0.2043
 -3.61    0.411  -0.1986
 -4.67    0.295  -0.1956
 -5.65    0.181  -0.1903
 -6.69    0.067  -0.1812
 -7.57   -0.089  -0.0967
 -8.63   -0.171  -0.0500
 -9.62   -0.209  -0.0262
Tabulated from data in file bm05002.dat & reduced using program C10.20

Average Reynolds #:
499848
Number of angles of attack:
61
 alpha  /   Cl   /  Cm
-10.20   -0.235  -0.0254
 -9.10   -0.193  -0.0476
 -8.32   -0.152  -0.0757
 -7.31   -0.042  -0.1319
 -6.11    0.137  -0.1860
 -5.04    0.257  -0.1901
 -4.13    0.361  -0.1931
 -3.04    0.493  -0.1978
 -2.02    0.616  -0.2013
 -0.97    0.720  -0.2003
 -0.02    0.819  -0.1986
  1.00    0.928  -0.1980
  2.08    1.031  -0.1964
  3.15    1.143  -0.1936
  4.17    1.243  -0.1910
  5.19    1.345  -0.1874
  6.17    1.444  -0.1833
  7.17    1.525  -0.1770
  8.23    1.599  -0.1678
  9.27    1.656  -0.1579
 10.28    1.687  -0.1468
 11.37    1.714  -0.1363
 12.32    1.723  -0.1302
 13.30    1.739  -0.1254
 14.28    1.749  -0.1246
 15.35    1.747  -0.1232
 16.34    1.760  -0.1255
 17.34    1.746  -0.1271
 18.35    1.729  -0.1308
 19.31    1.737  -0.1377
 20.29    1.715  -0.1455
 19.77    1.720  -0.1436
 18.77    1.730  -0.1348
 17.82    1.732  -0.1298
 16.74    1.753  -0.1277
 15.82    1.763  -0.1267
 14.86    1.745  -0.1248
 13.75    1.744  -0.1263
 12.74    1.736  -0.1293
 11.79    1.727  -0.1348
 10.74    1.711  -0.1433
  9.71    1.681  -0.1547
  8.68    1.622  -0.1645
  7.74    1.572  -0.1738
  6.68    1.485  -0.1805
  5.62    1.395  -0.1866
  4.62    1.300  -0.1908
  3.63    1.189  -0.1928
  2.52    1.081  -0.1952
  1.49    0.984  -0.1981
  0.50    0.873  -0.1989
 -0.54    0.770  -0.2005
 -1.52    0.666  -0.2012
 -2.57    0.546  -0.1993
 -3.63    0.422  -0.1948
 -4.64    0.302  -0.1924
 -5.64    0.188  -0.1873
 -6.69    0.072  -0.1807
 -7.62   -0.085  -0.1116
 -8.57   -0.155  -0.0608
 -9.55   -0.208  -0.0354
Tabulated from data in file bm05004.dat & reduced using program C10.20

File fx63137_c.lft created using program C10.20 on Thu May 22 17:01:21 2003
