Airfoil: SH3055
Builder: Y. Tinel
Comment: 'clean'

Number of Reynolds #'s:
4

Average Reynolds #:
99991
Number of angles of attack:
61
 alpha  /   Cl   /  Cm
-10.15   -0.226  -0.0345
 -9.08   -0.213  -0.0308
 -8.08   -0.279  -0.0155
 -7.05   -0.287  -0.0199
 -6.11   -0.273  -0.0254
 -5.06   -0.210  -0.0389
 -4.05   -0.120  -0.0658
 -3.09    0.003  -0.0976
 -2.08    0.184  -0.1314
 -1.05    0.344  -0.1484
 -0.02    0.504  -0.1622
  1.00    0.628  -0.1695
  2.01    0.740  -0.1603
  3.05    0.864  -0.1810
  4.12    0.990  -0.1845
  5.11    1.093  -0.1801
  6.13    1.215  -0.1874
  7.13    1.324  -0.1793
  8.20    1.436  -0.1763
  9.16    1.543  -0.1852
 10.22    1.627  -0.1661
 11.26    1.718  -0.1694
 12.26    1.771  -0.1604
 13.28    1.823  -0.1624
 14.35    1.846  -0.1547
 15.30    1.868  -0.1615
 16.33    1.885  -0.1615
 17.25    1.824  -0.1647
 18.33    1.751  -0.1698
 19.26    1.702  -0.1770
 20.24    1.645  -0.1905
 19.72    1.648  -0.1904
 18.73    1.726  -0.1790
 17.81    1.785  -0.1709
 16.79    1.866  -0.1709
 15.87    1.894  -0.1700
 14.80    1.855  -0.1549
 13.78    1.844  -0.1666
 12.71    1.801  -0.1786
 11.78    1.750  -0.1782
 10.73    1.662  -0.1699
  9.70    1.586  -0.1774
  8.71    1.481  -0.1746
  7.65    1.370  -0.1758
  6.67    1.268  -0.1938
  5.63    1.146  -0.1902
  4.60    1.039  -0.1822
  3.54    0.923  -0.1782
  2.50    0.804  -0.1723
  1.46    0.674  -0.1586
  0.48    0.553  -0.1591
 -0.53    0.452  -0.1556
 -1.56    0.288  -0.1437
 -2.59    0.071  -0.1064
 -3.61   -0.080  -0.0799
 -4.60   -0.178  -0.0516
 -5.63   -0.244  -0.0301
 -6.61   -0.247  -0.0259
 -7.61   -0.278  -0.0149
 -8.55   -0.237  -0.0196
 -9.61   -0.238  -0.0272
Tabulated from data in file bm05056.dat & reduced using program C10.20

Average Reynolds #:
200055
Number of angles of attack:
61
 alpha  /   Cl   /  Cm
-10.10   -0.255  -0.0072
 -9.01   -0.236  -0.0112
 -8.02   -0.238  -0.0166
 -7.10   -0.183  -0.0319
 -6.16   -0.026  -0.1297
 -5.16    0.220  -0.2281
 -4.17    0.376  -0.2374
 -3.11    0.498  -0.2388
 -2.10    0.606  -0.2391
 -1.07    0.705  -0.2352
 -0.10    0.802  -0.2344
  0.94    0.901  -0.2308
  2.06    1.008  -0.2283
  3.06    1.110  -0.2252
  4.10    1.206  -0.2216
  5.10    1.303  -0.2183
  6.17    1.402  -0.2143
  7.18    1.492  -0.2097
  8.18    1.581  -0.2057
  9.17    1.662  -0.2006
 10.27    1.742  -0.1945
 11.29    1.809  -0.1875
 12.29    1.874  -0.1806
 13.35    1.908  -0.1699
 14.32    1.891  -0.1572
 15.30    1.875  -0.1528
 16.30    1.829  -0.1534
 17.26    1.786  -0.1588
 18.25    1.731  -0.1674
 19.22    1.683  -0.1775
 20.19    1.643  -0.1902
 19.70    1.662  -0.1824
 18.75    1.714  -0.1755
 17.73    1.760  -0.1656
 16.75    1.816  -0.1583
 15.80    1.851  -0.1550
 14.80    1.883  -0.1556
 13.80    1.905  -0.1650
 12.75    1.888  -0.1771
 11.83    1.847  -0.1855
 10.74    1.775  -0.1928
  9.72    1.705  -0.1987
  8.71    1.623  -0.2044
  7.70    1.539  -0.2092
  6.62    1.445  -0.2138
  5.65    1.361  -0.2182
  4.60    1.252  -0.2207
  3.59    1.153  -0.2242
  2.52    1.054  -0.2274
  1.51    0.959  -0.2306
  0.46    0.853  -0.2325
 -0.60    0.756  -0.2376
 -1.57    0.668  -0.2407
 -2.60    0.559  -0.2410
 -3.64    0.446  -0.2407
 -4.65    0.311  -0.2341
 -5.70    0.133  -0.2193
 -6.71   -0.050  -0.1988
 -7.72   -0.217  -0.1836
 -8.78   -0.390  -0.1605
 -9.79   -0.558  -0.1271
Tabulated from data in file bm05058.dat & reduced using program C10.20

Average Reynolds #:
349917
Number of angles of attack:
61
 alpha  /   Cl   /  Cm
-10.07   -0.277  -0.0091
 -9.04   -0.244  -0.0213
 -8.09   -0.180  -0.0514
 -7.17    0.011  -0.2258
 -6.17    0.166  -0.2402
 -5.13    0.296  -0.2442
 -4.13    0.409  -0.2469
 -3.13    0.521  -0.2475
 -2.09    0.631  -0.2476
 -1.08    0.737  -0.2474
 -0.07    0.843  -0.2455
  1.01    0.960  -0.2446
  2.02    1.057  -0.2421
  3.07    1.165  -0.2393
  4.09    1.269  -0.2369
  5.08    1.366  -0.2327
  6.14    1.466  -0.2280
  7.17    1.559  -0.2230
  8.22    1.645  -0.2161
  9.26    1.731  -0.2099
 10.26    1.783  -0.2013
 11.24    1.838  -0.1907
 12.30    1.868  -0.1777
 13.28    1.871  -0.1664
 14.29    1.842  -0.1625
 15.31    1.798  -0.1651
 16.31    1.753  -0.1667
 17.27    1.720  -0.1689
 18.26    1.706  -0.1722
 19.23    1.676  -0.1770
 20.17    1.649  -0.1930
 19.70    1.659  -0.1863
 18.78    1.694  -0.1767
 17.74    1.713  -0.1698
 16.77    1.757  -0.1664
 15.75    1.784  -0.1637
 14.82    1.822  -0.1596
 13.87    1.858  -0.1628
 12.76    1.874  -0.1729
 11.78    1.866  -0.1847
 10.71    1.826  -0.1972
  9.73    1.767  -0.2056
  8.70    1.695  -0.2140
  7.68    1.612  -0.2205
  6.62    1.520  -0.2265
  5.59    1.417  -0.2303
  4.56    1.322  -0.2355
  3.58    1.223  -0.2385
  2.55    1.117  -0.2412
  1.56    1.011  -0.2431
  0.44    0.900  -0.2451
 -0.58    0.797  -0.2474
 -1.61    0.683  -0.2470
 -2.63    0.574  -0.2478
 -3.66    0.466  -0.2481
 -4.68    0.348  -0.2467
 -5.69    0.229  -0.2422
 -6.68    0.100  -0.2350
 -7.75   -0.095  -0.2135
 -8.77   -0.281  -0.1896
 -9.76   -0.477  -0.1580
Tabulated from data in file bm05060.dat & reduced using program C10.20

Average Reynolds #:
500174
Number of angles of attack:
61
 alpha  /   Cl   /  Cm
-10.16   -0.267  -0.0211
 -9.17   -0.226  -0.0472
 -8.22   -0.099  -0.2220
 -7.24    0.054  -0.2349
 -6.20    0.188  -0.2412
 -5.23    0.304  -0.2459
 -4.11    0.436  -0.2472
 -3.12    0.547  -0.2487
 -2.12    0.654  -0.2480
 -1.04    0.767  -0.2474
 -0.02    0.877  -0.2473
  0.97    0.976  -0.2448
  2.06    1.092  -0.2440
  3.05    1.190  -0.2404
  4.09    1.283  -0.2354
  5.16    1.395  -0.2327
  6.17    1.492  -0.2275
  7.17    1.584  -0.2217
  8.29    1.680  -0.2151
  9.30    1.764  -0.2077
 10.27    1.822  -0.1969
 11.30    1.859  -0.1840
 12.27    1.862  -0.1702
 13.27    1.846  -0.1608
 14.30    1.830  -0.1601
 15.33    1.784  -0.1594
 16.32    1.731  -0.1614
 17.27    1.712  -0.1683
 18.26    1.668  -0.1760
 19.23    1.635  -0.1851
 20.16    1.600  -0.1972
 19.69    1.602  -0.1916
 18.70    1.653  -0.1811
 17.70    1.701  -0.1732
 16.73    1.727  -0.1659
 15.75    1.771  -0.1626
 14.73    1.811  -0.1591
 13.81    1.840  -0.1603
 12.77    1.852  -0.1641
 11.74    1.859  -0.1755
 10.71    1.838  -0.1894
  9.69    1.786  -0.2010
  8.70    1.720  -0.2109
  7.67    1.643  -0.2196
  6.62    1.549  -0.2260
  5.65    1.459  -0.2310
  4.58    1.350  -0.2357
  3.54    1.240  -0.2383
  2.56    1.143  -0.2405
  1.48    1.027  -0.2428
  0.52    0.929  -0.2465
 -0.51    0.827  -0.2473
 -1.57    0.712  -0.2481
 -2.61    0.597  -0.2482
 -3.61    0.492  -0.2488
 -4.63    0.373  -0.2474
 -5.69    0.244  -0.2430
 -6.71    0.120  -0.2384
 -7.80   -0.023  -0.2263
 -8.75   -0.183  -0.2108
 -9.76   -0.396  -0.1729
Tabulated from data in file bm05062.dat & reduced using program C10.20

File sh3055_c.lft created using program C10.20 on Thu May 22 17:01:22 2003
