Airfoil: SH3055
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 #:
99926
Number of angles of attack:
61
 alpha  /   Cl   /  Cm
-10.09   -0.204   0.0033
 -9.00   -0.198   0.0032
 -7.95   -0.207   0.0033
 -6.98   -0.224   0.0036
 -5.95   -0.172   0.0027
 -4.91   -0.081   0.0013
 -3.99    0.116  -0.0019
 -2.98    0.259  -0.0042
 -2.03    0.403  -0.0065
 -0.90    0.571  -0.0092
  0.17    0.705  -0.0114
  1.25    0.752  -0.0121
  2.22    0.826  -0.0133
  3.20    0.940  -0.0152
  4.26    1.057  -0.0170
  5.21    1.161  -0.0187
  6.32    1.276  -0.0205
  7.40    1.386  -0.0223
  8.50    1.484  -0.0239
  9.50    1.562  -0.0251
 10.50    1.634  -0.0263
 11.37    1.686  -0.0271
 12.51    1.733  -0.0279
 13.35    1.736  -0.0279
 14.44    1.692  -0.0272
 15.32    1.648  -0.0265
 16.51    1.622  -0.0261
 17.40    1.645  -0.0265
 18.29    1.654  -0.0266
 19.54    1.678  -0.0270
 20.40    1.677  -0.0270
 19.83    1.676  -0.0270
 18.94    1.667  -0.0268
 17.92    1.650  -0.0265
 16.85    1.638  -0.0264
 16.00    1.649  -0.0265
 14.90    1.663  -0.0268
 13.83    1.713  -0.0276
 12.94    1.739  -0.0280
 11.81    1.714  -0.0276
 10.83    1.650  -0.0265
  9.85    1.587  -0.0255
  8.82    1.504  -0.0242
  7.71    1.410  -0.0227
  6.86    1.333  -0.0215
  5.81    1.223  -0.0197
  4.69    1.105  -0.0178
  3.83    1.010  -0.0163
  2.76    0.886  -0.0143
  1.61    0.770  -0.0124
  0.69    0.723  -0.0117
 -0.42    0.641  -0.0103
 -1.38    0.523  -0.0084
 -2.38    0.357  -0.0058
 -3.39    0.204  -0.0033
 -4.44    0.082  -0.0014
 -5.57   -0.069   0.0011
 -6.46   -0.190   0.0030
 -7.66   -0.345   0.0055
 -8.59   -0.209   0.0033
 -9.57   -0.189   0.0030
Tabulated from data in file bm05117.dat & reduced using program C10.20

Average Reynolds #:
200101
Number of angles of attack:
61
 alpha  /   Cl   /  Cm
-10.06   -0.266  -0.0074
 -9.09   -0.286  -0.0131
 -8.13   -0.297  -0.0656
 -7.21   -0.237  -0.1513
 -6.21   -0.027  -0.1858
 -5.12    0.173  -0.2108
 -4.14    0.341  -0.2274
 -3.11    0.471  -0.2360
 -2.09    0.588  -0.2383
 -1.07    0.696  -0.2378
 -0.06    0.802  -0.2356
  0.96    0.904  -0.2316
  2.06    0.992  -0.2264
  3.02    1.064  -0.2185
  4.06    1.144  -0.2110
  5.13    1.229  -0.2052
  6.12    1.298  -0.1973
  7.16    1.361  -0.1899
  8.20    1.422  -0.1823
  9.18    1.471  -0.1753
 10.24    1.504  -0.1677
 11.22    1.527  -0.1659
 12.17    1.539  -0.1638
 13.22    1.537  -0.1645
 14.19    1.519  -0.1671
 15.23    1.527  -0.1703
 16.22    1.524  -0.1732
 17.21    1.520  -0.1771
 18.18    1.543  -0.1827
 19.21    1.561  -0.1871
 20.17    1.600  -0.1957
 19.67    1.587  -0.1920
 18.71    1.532  -0.1852
 17.69    1.539  -0.1828
 16.67    1.528  -0.1772
 15.72    1.531  -0.1744
 14.69    1.534  -0.1685
 13.70    1.539  -0.1668
 12.70    1.530  -0.1650
 11.71    1.533  -0.1653
 10.75    1.518  -0.1671
  9.68    1.487  -0.1725
  8.68    1.446  -0.1802
  7.70    1.390  -0.1878
  6.62    1.335  -0.1964
  5.63    1.262  -0.2020
  4.61    1.188  -0.2103
  3.58    1.105  -0.2153
  2.51    1.026  -0.2235
  1.53    0.949  -0.2311
  0.46    0.850  -0.2345
 -0.52    0.746  -0.2356
 -1.58    0.642  -0.2361
 -2.62    0.532  -0.2389
 -3.61    0.405  -0.2328
 -4.62    0.254  -0.2225
 -5.68    0.061  -0.1991
 -6.73   -0.140  -0.1685
 -7.70   -0.333  -0.1338
 -8.72   -0.495  -0.1068
 -9.76   -0.604  -0.0995
Tabulated from data in file bm05066.dat & reduced using program C10.20

Average Reynolds #:
349945
Number of angles of attack:
61
 alpha  /   Cl   /  Cm
-10.08   -0.268  -0.0218
 -9.27   -0.344  -0.0716
 -8.21   -0.238  -0.1171
 -7.14   -0.087  -0.1804
 -6.20    0.098  -0.2101
 -5.23    0.240  -0.2226
 -4.16    0.374  -0.2307
 -3.08    0.494  -0.2342
 -2.11    0.597  -0.2341
 -1.06    0.694  -0.2310
 -0.07    0.787  -0.2281
  1.03    0.894  -0.2276
  2.01    0.990  -0.2249
  2.98    1.077  -0.2220
  4.06    1.167  -0.2171
  5.11    1.263  -0.2129
  6.14    1.334  -0.2051
  7.14    1.400  -0.1972
  8.17    1.460  -0.1881
  9.26    1.509  -0.1796
 10.24    1.533  -0.1735
 11.21    1.556  -0.1724
 12.19    1.561  -0.1724
 13.23    1.565  -0.1713
 14.23    1.562  -0.1728
 15.22    1.570  -0.1741
 16.15    1.547  -0.1770
 17.19    1.558  -0.1831
 18.23    1.563  -0.1876
 19.20    1.568  -0.1922
 20.14    1.566  -0.2021
 19.67    1.578  -0.1986
 18.68    1.563  -0.1915
 17.69    1.568  -0.1859
 16.72    1.558  -0.1825
 15.72    1.561  -0.1792
 14.66    1.571  -0.1768
 13.69    1.566  -0.1734
 12.68    1.562  -0.1730
 11.69    1.553  -0.1717
 10.70    1.549  -0.1732
  9.69    1.521  -0.1767
  8.67    1.486  -0.1851
  7.64    1.432  -0.1935
  6.62    1.372  -0.2027
  5.65    1.304  -0.2094
  4.56    1.222  -0.2168
  3.55    1.133  -0.2211
  2.54    1.044  -0.2254
  1.53    0.953  -0.2282
  0.43    0.843  -0.2304
 -0.51    0.749  -0.2320
 -1.58    0.650  -0.2338
 -2.58    0.552  -0.2366
 -3.63    0.435  -0.2339
 -4.66    0.321  -0.2304
 -5.68    0.175  -0.2191
 -6.64    0.014  -0.1976
 -7.68   -0.183  -0.1636
 -8.70   -0.362  -0.1291
 -9.74   -0.490  -0.1050
Tabulated from data in file bm05068.dat & reduced using program C10.20

Average Reynolds #:
500080
Number of angles of attack:
61
 alpha  /   Cl   /  Cm
-10.23   -0.276  -0.0358
 -9.11   -0.312  -0.1029
 -8.21   -0.217  -0.1604
 -7.23   -0.045  -0.1902
 -6.20    0.108  -0.2105
 -5.13    0.255  -0.2248
 -4.11    0.369  -0.2296
 -3.06    0.486  -0.2301
 -2.08    0.598  -0.2316
 -1.06    0.695  -0.2303
  0.02    0.796  -0.2284
  1.00    0.889  -0.2256
  2.00    0.983  -0.2225
  3.05    1.079  -0.2186
  4.10    1.172  -0.2141
  5.14    1.253  -0.2081
  6.07    1.333  -0.2037
  7.15    1.404  -0.1948
  8.15    1.449  -0.1853
  9.19    1.495  -0.1776
 10.24    1.520  -0.1741
 11.20    1.529  -0.1736
 12.23    1.539  -0.1755
 13.20    1.534  -0.1746
 14.20    1.527  -0.1765
 15.20    1.516  -0.1793
 16.21    1.530  -0.1817
 17.26    1.528  -0.1850
 18.19    1.531  -0.1888
 19.15    1.531  -0.2033
 20.17    1.491  -0.2118
 19.67    1.513  -0.2083
 18.60    1.528  -0.1974
 17.71    1.539  -0.1877
 16.70    1.548  -0.1859
 15.73    1.531  -0.1823
 14.65    1.524  -0.1786
 13.69    1.538  -0.1764
 12.65    1.538  -0.1758
 11.65    1.530  -0.1744
 10.70    1.522  -0.1737
  9.67    1.509  -0.1748
  8.70    1.473  -0.1801
  7.64    1.431  -0.1895
  6.66    1.372  -0.1977
  5.56    1.295  -0.2053
  4.56    1.217  -0.2117
  3.58    1.127  -0.2159
  2.51    1.022  -0.2187
  1.48    0.937  -0.2237
  0.44    0.843  -0.2274
 -0.54    0.748  -0.2298
 -1.58    0.644  -0.2294
 -2.66    0.532  -0.2303
 -3.67    0.425  -0.2295
 -4.67    0.306  -0.2268
 -5.72    0.182  -0.2187
 -6.67    0.037  -0.2021
 -7.69   -0.123  -0.1764
 -8.70   -0.297  -0.1410
 -9.70   -0.450  -0.1055
Tabulated from data in file bm05070.dat & reduced using program C10.20

File sh3055_tf.lft created using program C10.20 on Thu May 22 17:01:23 2003
