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 #:
99985
Number of angles of attack:
61
 alpha  /   Cl   /  Cm
-10.08   -0.218  -0.0337
 -9.07   -0.270  -0.0203
 -8.09   -0.288  -0.0167
 -7.12   -0.340  -0.0133
 -6.08   -0.312  -0.0326
 -5.13   -0.012  -0.1532
 -4.14    0.116  -0.1651
 -3.12    0.244  -0.1727
 -2.09    0.368  -0.1807
 -1.05    0.456  -0.1646
 -0.01    0.527  -0.1677
  0.98    0.598  -0.1693
  2.03    0.656  -0.1654
  3.11    0.880  -0.1560
  4.11    1.016  -0.1454
  5.13    1.140  -0.1502
  6.19    1.237  -0.1543
  7.21    1.336  -0.1510
  8.23    1.410  -0.1436
  9.26    1.485  -0.1295
 10.26    1.528  -0.1328
 11.29    1.532  -0.1219
 12.24    1.514  -0.1242
 13.27    1.503  -0.1234
 14.24    1.491  -0.1279
 15.27    1.495  -0.1273
 16.24    1.508  -0.1309
 17.26    1.545  -0.1337
 18.26    1.566  -0.1376
 19.05    1.109  -0.2642
 20.03    1.191  -0.2861
 19.48    1.134  -0.2838
 18.47    1.102  -0.2707
 17.50    1.066  -0.2508
 16.50    1.107  -0.2425
 15.57    1.199  -0.2268
 14.80    1.506  -0.1251
 13.74    1.511  -0.1276
 12.74    1.520  -0.1220
 11.80    1.534  -0.1200
 10.69    1.540  -0.1271
  9.76    1.515  -0.1385
  8.71    1.461  -0.1383
  7.68    1.390  -0.1429
  6.68    1.299  -0.1466
  5.61    1.205  -0.1560
  4.59    1.079  -0.1497
  3.60    0.963  -0.1604
  2.48    0.699  -0.1640
  1.45    0.620  -0.1616
  0.50    0.568  -0.1676
 -0.56    0.501  -0.1723
 -1.59    0.432  -0.1879
 -2.59    0.316  -0.1707
 -3.60    0.181  -0.1614
 -4.57    0.073  -0.1585
 -5.60   -0.244  -0.0700
 -6.59   -0.307  -0.0244
 -7.59   -0.319  -0.0181
 -8.62   -0.277  -0.0266
 -9.56   -0.251  -0.0335
Tabulated from data in file bm05006.dat & reduced using program C10.20

Average Reynolds #:
149980
Number of angles of attack:
61
 alpha  /   Cl   /  Cm
-10.13   -0.239  -0.0144
 -9.09   -0.261  -0.0177
 -8.07   -0.267  -0.0268
 -7.11   -0.197  -0.0566
 -6.16   -0.023  -0.1541
 -5.14    0.159  -0.1856
 -4.12    0.302  -0.1925
 -3.06    0.422  -0.1982
 -2.06    0.535  -0.1980
 -1.03    0.643  -0.1927
  0.05    0.742  -0.1908
  1.03    0.832  -0.1868
  2.09    0.933  -0.1789
  3.07    1.024  -0.1751
  4.10    1.097  -0.1650
  5.12    1.168  -0.1579
  6.18    1.244  -0.1557
  7.18    1.306  -0.1494
  8.21    1.352  -0.1418
  9.23    1.384  -0.1324
 10.19    1.420  -0.1296
 11.25    1.442  -0.1274
 12.24    1.463  -0.1252
 13.25    1.474  -0.1269
 14.24    1.483  -0.1300
 15.26    1.485  -0.1329
 16.24    1.489  -0.1407
 17.21    1.470  -0.1416
 18.24    1.460  -0.1474
 19.26    1.491  -0.1509
 20.00    1.190  -0.2624
 19.56    1.181  -0.2647
 18.54    1.271  -0.2632
 17.54    1.285  -0.2448
 16.60    1.322  -0.2299
 15.62    1.296  -0.2128
 14.76    1.489  -0.1368
 13.74    1.486  -0.1321
 12.72    1.470  -0.1291
 11.75    1.454  -0.1287
 10.71    1.432  -0.1293
  9.72    1.407  -0.1326
  8.73    1.372  -0.1383
  7.65    1.327  -0.1455
  6.64    1.269  -0.1518
  5.61    1.207  -0.1596
  4.62    1.129  -0.1618
  3.57    1.059  -0.1697
  2.56    0.977  -0.1760
  1.52    0.881  -0.1807
  0.54    0.790  -0.1858
 -0.51    0.698  -0.1916
 -1.57    0.595  -0.1934
 -2.61    0.483  -0.1931
 -3.60    0.365  -0.1962
 -4.64    0.233  -0.1856
 -5.68    0.077  -0.1715
 -6.63   -0.147  -0.0765
 -7.61   -0.216  -0.0403
 -8.62   -0.275  -0.0177
 -9.58   -0.244  -0.0171
Tabulated from data in file bm05008.dat & reduced using program C10.20

Average Reynolds #:
200005
Number of angles of attack:
61
 alpha  /   Cl   /  Cm
-10.11   -0.212  -0.0155
 -9.09   -0.246  -0.0197
 -8.08   -0.185  -0.0436
 -7.09   -0.110  -0.0857
 -6.17    0.085  -0.1815
 -5.15    0.207  -0.1908
 -4.11    0.321  -0.1936
 -3.10    0.431  -0.1959
 -2.07    0.538  -0.1944
 -1.01    0.640  -0.1919
  0.01    0.752  -0.1912
  1.01    0.849  -0.1879
  2.03    0.937  -0.1812
  3.07    1.006  -0.1735
  4.09    1.084  -0.1673
  5.17    1.162  -0.1608
  6.16    1.225  -0.1550
  7.15    1.296  -0.1501
  8.22    1.346  -0.1430
  9.25    1.392  -0.1366
 10.26    1.426  -0.1327
 11.27    1.453  -0.1311
 12.25    1.478  -0.1309
 13.23    1.492  -0.1309
 14.22    1.500  -0.1334
 15.26    1.495  -0.1367
 16.25    1.489  -0.1415
 17.24    1.509  -0.1481
 18.21    1.482  -0.1509
 19.25    1.494  -0.1600
 20.17    1.496  -0.1632
 19.70    1.493  -0.1649
 18.70    1.506  -0.1608
 17.70    1.492  -0.1520
 16.71    1.512  -0.1479
 15.73    1.506  -0.1420
 14.71    1.508  -0.1378
 13.71    1.501  -0.1349
 12.72    1.491  -0.1334
 11.67    1.471  -0.1329
 10.72    1.444  -0.1340
  9.77    1.411  -0.1369
  8.71    1.379  -0.1427
  7.67    1.326  -0.1487
  6.64    1.257  -0.1543
  5.62    1.199  -0.1610
  4.60    1.131  -0.1671
  3.59    1.052  -0.1734
  2.54    0.981  -0.1806
  1.51    0.892  -0.1862
  0.55    0.805  -0.1905
 -0.53    0.695  -0.1934
 -1.56    0.595  -0.1961
 -2.59    0.487  -0.1965
 -3.64    0.377  -0.1942
 -4.62    0.269  -0.1912
 -5.66    0.150  -0.1866
 -6.61   -0.014  -0.1435
 -7.59   -0.156  -0.0625
 -8.59   -0.225  -0.0313
 -9.61   -0.233  -0.0180
Tabulated from data in file bm05010.dat & reduced using program C10.20

Average Reynolds #:
349891
Number of angles of attack:
61
 alpha  /   Cl   /  Cm
-10.15   -0.252  -0.0298
 -9.08   -0.213  -0.0451
 -8.12   -0.143  -0.0780
 -7.17   -0.044  -0.1271
 -6.13    0.126  -0.1858
 -5.09    0.241  -0.1898
 -4.08    0.362  -0.1943
 -3.05    0.468  -0.1943
 -2.02    0.568  -0.1919
 -1.00    0.658  -0.1885
 -0.01    0.746  -0.1843
  1.00    0.839  -0.1819
  2.01    0.927  -0.1789
  3.08    1.027  -0.1761
  4.10    1.109  -0.1717
  5.10    1.195  -0.1675
  6.19    1.276  -0.1629
  7.15    1.337  -0.1564
  8.20    1.383  -0.1480
  9.25    1.419  -0.1420
 10.21    1.455  -0.1384
 11.23    1.492  -0.1368
 12.23    1.509  -0.1363
 13.21    1.527  -0.1370
 14.25    1.538  -0.1393
 15.24    1.519  -0.1428
 16.22    1.508  -0.1456
 17.16    1.521  -0.1523
 18.20    1.516  -0.1576
 19.20    1.518  -0.1651
 20.19    1.500  -0.1710
 19.69    1.514  -0.1698
 18.67    1.521  -0.1624
 17.72    1.513  -0.1545
 16.72    1.527  -0.1501
 15.72    1.526  -0.1448
 14.70    1.532  -0.1403
 13.68    1.534  -0.1389
 12.71    1.512  -0.1344
 11.74    1.492  -0.1352
 10.69    1.469  -0.1371
  9.73    1.433  -0.1393
  8.67    1.398  -0.1446
  7.66    1.361  -0.1524
  6.65    1.309  -0.1599
  5.64    1.233  -0.1652
  4.61    1.155  -0.1697
  3.64    1.068  -0.1732
  2.59    0.976  -0.1772
  1.52    0.884  -0.1807
  0.49    0.790  -0.1833
 -0.50    0.696  -0.1864
 -1.57    0.607  -0.1907
 -2.60    0.511  -0.1952
 -3.58    0.409  -0.1952
 -4.63    0.297  -0.1922
 -5.67    0.172  -0.1877
 -6.64    0.060  -0.1813
 -7.56   -0.099  -0.1000
 -8.63   -0.181  -0.0509
 -9.62   -0.223  -0.0267
Tabulated from data in file bm05012.dat & reduced using program C10.20

Average Reynolds #:
499970
Number of angles of attack:
61
 alpha  /   Cl   /  Cm
-10.10   -0.218  -0.0234
 -9.16   -0.191  -0.0438
 -8.14   -0.129  -0.0760
 -7.12   -0.025  -0.1402
 -6.16    0.132  -0.1850
 -5.08    0.259  -0.1912
 -4.08    0.358  -0.1907
 -3.05    0.460  -0.1899
 -2.03    0.566  -0.1886
 -1.04    0.654  -0.1857
  0.02    0.752  -0.1833
  1.06    0.841  -0.1807
  2.08    0.939  -0.1778
  3.10    1.028  -0.1737
  4.15    1.118  -0.1705
  5.13    1.195  -0.1662
  6.17    1.267  -0.1597
  7.15    1.336  -0.1532
  8.18    1.390  -0.1468
  9.20    1.431  -0.1420
 10.19    1.475  -0.1389
 11.24    1.497  -0.1380
 12.24    1.508  -0.1383
 13.22    1.519  -0.1419
 14.22    1.525  -0.1449
 15.28    1.519  -0.1472
 16.28    1.519  -0.1518
 17.26    1.506  -0.1552
 18.20    1.509  -0.1627
 19.22    1.496  -0.1666
 20.20    1.516  -0.1770
 19.71    1.495  -0.1708
 18.73    1.507  -0.1652
 17.65    1.511  -0.1586
 16.71    1.520  -0.1540
 15.71    1.511  -0.1494
 14.72    1.531  -0.1466
 13.67    1.530  -0.1423
 12.72    1.520  -0.1389
 11.72    1.512  -0.1378
 10.72    1.476  -0.1375
  9.75    1.452  -0.1399
  8.67    1.414  -0.1440
  7.69    1.364  -0.1492
  6.64    1.308  -0.1567
  5.64    1.236  -0.1626
  4.60    1.161  -0.1684
  3.56    1.065  -0.1722
  2.50    0.973  -0.1753
  1.49    0.883  -0.1787
  0.47    0.787  -0.1820
 -0.51    0.693  -0.1834
 -1.54    0.611  -0.1869
 -2.61    0.503  -0.1879
 -3.54    0.412  -0.1901
 -4.61    0.296  -0.1902
 -5.60    0.190  -0.1871
 -6.69    0.066  -0.1818
 -7.57   -0.081  -0.1042
 -8.53   -0.150  -0.0627
 -9.43   -0.198  -0.0381
Tabulated from data in file bm05014.dat & reduced using program C10.20

File fx63137_tf.lft created using program C10.20 on Thu May 22 17:01:21 2003
