Airfoil: S8025
Builder: J. Thurmond
Comment: clean

Number of Reynolds #'s:
 4 

Average Reynolds #:
 60300 
Number of angles of attack:
 49 
 alpha /   Cl   /  Cm
 -6.87  -0.596  -0.0030
 -5.34  -0.477  -0.0030
 -4.30  -0.401  -0.0030
 -3.48  -0.329  -0.0030
 -2.41  -0.212  -0.0030
 -1.28  -0.073  -0.0030
 -0.40  -0.010  -0.0030
  0.87   0.123  -0.0030
  1.78   0.221  -0.0030
  2.69   0.321  -0.0030
  3.83   0.428  -0.0030
  4.98   0.533  -0.0030
  5.93   0.615  -0.0030
  6.84   0.691  -0.0030
  7.99   0.785  -0.0030
  8.88   0.846  -0.0030
 10.01   0.848  -0.0030
 10.86   0.846  -0.0030
 11.95   0.864  -0.0030
 12.83   0.853  -0.0030
 13.98   0.863  -0.0030
 14.93   0.879  -0.0030
 15.94   0.889  -0.0030
 17.00   0.894  -0.0030
 17.97   0.888  -0.0030
 16.39   0.911  -0.0030
 15.56   0.879  -0.0030
 14.45   0.858  -0.0030
 13.44   0.877  -0.0030
 12.37   0.872  -0.0030
 11.48   0.843  -0.0030
 10.29   0.824  -0.0030
  9.54   0.824  -0.0030
  8.45   0.809  -0.0030
  7.43   0.728  -0.0030
  6.36   0.642  -0.0030
  5.32   0.553  -0.0030
  4.25   0.453  -0.0030
  3.23   0.362  -0.0030
  2.40   0.278  -0.0030
  1.28   0.153  -0.0030
  0.25   0.036  -0.0030
 -0.75  -0.050  -0.0030
 -1.74  -0.154  -0.0030
 -3.02  -0.304  -0.0030
 -3.77  -0.377  -0.0030
 -4.90  -0.475  -0.0030
 -5.97  -0.561  -0.0030
 -7.07  -0.646  -0.0030
Tabulated from data in file CF00875.DAT & reduced using program Q02.00L

Average Reynolds #:
 100600 
Number of angles of attack:
 49 
 alpha /   Cl   /  Cm
 -6.51  -0.608  -0.0030
 -5.47  -0.523  -0.0030
 -4.26  -0.418  -0.0030
 -3.33  -0.333  -0.0030
 -2.16  -0.221  -0.0030
 -1.24  -0.098  -0.0030
 -0.18  -0.003  -0.0030
  0.65   0.077  -0.0030
  1.81   0.218  -0.0030
  2.73   0.300  -0.0030
  3.90   0.411  -0.0030
  4.85   0.503  -0.0030
  6.03   0.615  -0.0030
  7.01   0.701  -0.0030
  7.97   0.779  -0.0030
  8.90   0.846  -0.0030
 10.10   0.910  -0.0030
 10.94   0.838  -0.0030
 11.97   0.843  -0.0030
 12.88   0.849  -0.0030
 14.03   0.845  -0.0030
 14.96   0.840  -0.0030
 15.87   0.838  -0.0030
 17.09   0.838  -0.0030
 17.99   0.843  -0.0030
 16.46   0.844  -0.0030
 15.44   0.824  -0.0030
 14.31   0.835  -0.0030
 13.51   0.825  -0.0030
 12.42   0.832  -0.0030
 11.35   0.833  -0.0030
 10.33   0.875  -0.0030
  9.28   0.860  -0.0030
  8.43   0.799  -0.0030
  7.38   0.712  -0.0030
  6.30   0.620  -0.0030
  5.19   0.522  -0.0030
  4.38   0.448  -0.0030
  3.30   0.344  -0.0030
  2.23   0.247  -0.0030
  1.20   0.148  -0.0030
  0.17   0.021  -0.0030
 -0.83  -0.059  -0.0030
 -1.84  -0.181  -0.0030
 -2.91  -0.303  -0.0030
 -3.95  -0.395  -0.0030
 -5.02  -0.485  -0.0030
 -5.97  -0.565  -0.0030
 -7.05  -0.648  -0.0030
Tabulated from data in file CF00877.DAT & reduced using program Q02.00L

Average Reynolds #:
 201500 
Number of angles of attack:
 49 
 alpha /   Cl   /  Cm
 -6.85  -0.637  -0.0030
 -5.34  -0.507  -0.0030
 -4.33  -0.413  -0.0030
 -3.35  -0.320  -0.0030
 -2.38  -0.228  -0.0030
 -1.26  -0.116  -0.0030
 -0.11   0.029  -0.0030
  0.87   0.126  -0.0030
  1.98   0.221  -0.0030
  2.83   0.307  -0.0030
  3.78   0.404  -0.0030
  4.98   0.525  -0.0030
  5.90   0.629  -0.0030
  6.96   0.731  -0.0030
  7.87   0.812  -0.0030
  9.00   0.904  -0.0030
  9.97   0.961  -0.0030
 10.83   0.914  -0.0030
 12.11   0.884  -0.0030
 13.07   0.863  -0.0030
 13.94   0.872  -0.0030
 14.95   0.854  -0.0030
 15.86   0.839  -0.0030
 16.92   0.856  -0.0030
 17.97   0.849  -0.0030
 16.19   0.848  -0.0030
 15.28   0.843  -0.0030
 14.25   0.860  -0.0030
 13.51   0.877  -0.0030
 12.31   0.875  -0.0030
 11.34   0.902  -0.0030
 10.45   0.976  -0.0030
  9.43   0.924  -0.0030
  8.46   0.852  -0.0030
  7.48   0.766  -0.0030
  6.32   0.657  -0.0030
  5.40   0.564  -0.0030
  4.29   0.442  -0.0030
  3.38   0.352  -0.0030
  2.18   0.229  -0.0030
  1.06   0.125  -0.0030
  0.21   0.051  -0.0030
 -0.91  -0.082  -0.0030
 -1.97  -0.201  -0.0030
 -2.81  -0.281  -0.0030
 -3.96  -0.390  -0.0030
 -4.98  -0.484  -0.0030
 -5.87  -0.564  -0.0030
 -7.11  -0.665  -0.0030
Tabulated from data in file CF00879.DAT & reduced using program Q02.00L

Average Reynolds #:
 302000 
Number of angles of attack:
 49 
 alpha /   Cl   /  Cm
 -6.50  -0.618  -0.0030
 -5.20  -0.503  -0.0030
 -4.34  -0.420  -0.0030
 -3.37  -0.326  -0.0030
 -2.32  -0.221  -0.0030
 -1.29  -0.119  -0.0030
 -0.27   0.004  -0.0030
  1.04   0.122  -0.0030
  1.75   0.192  -0.0030
  2.83   0.320  -0.0030
  3.75   0.418  -0.0030
  4.92   0.536  -0.0030
  5.86   0.625  -0.0030
  6.98   0.735  -0.0030
  7.84   0.812  -0.0030
  9.05   0.916  -0.0030
  9.94   0.973  -0.0030
 10.93   1.007  -0.0030
 11.91   0.928  -0.0030
 12.88   0.888  -0.0030
 14.03   0.875  -0.0030
 14.83   0.860  -0.0030
 15.95   0.851  -0.0030
 16.97   0.843  -0.0030
 17.90   0.868  -0.0030
 16.17   0.844  -0.0030
 15.47   0.857  -0.0030
 14.34   0.871  -0.0030
 13.44   0.899  -0.0030
 12.30   0.915  -0.0030
 11.32   0.955  -0.0030
 10.63   0.998  -0.0030
  9.40   0.936  -0.0030
  8.42   0.860  -0.0030
  7.39   0.768  -0.0030
  6.29   0.661  -0.0030
  5.41   0.575  -0.0030
  4.24   0.458  -0.0030
  3.28   0.359  -0.0030
  2.37   0.266  -0.0030
  1.29   0.140  -0.0030
  0.13   0.038  -0.0030
 -0.70  -0.055  -0.0030
 -1.84  -0.179  -0.0030
 -3.05  -0.300  -0.0030
 -3.95  -0.386  -0.0030
 -4.90  -0.479  -0.0030
 -6.12  -0.589  -0.0030
 -7.13  -0.673  -0.0030
Tabulated from data in file AG00881.DAT & reduced using program Q02.00L

File s8025.lft created on 09-12-1997 at 13:46:18 using program FORMAT