Airfoil: SD2030 (B)
Builder: Y. Tinel
Comment: 'clean'

Number of Reynolds #'s:
5

Average Reynolds #:
99958
Number of angles of attack:
61
 alpha  /   Cl   /  Cm
 -9.97   -0.568   0.0171
 -9.01   -0.571   0.0153
 -8.03   -0.561   0.0039
 -7.07   -0.517  -0.0176
 -6.08   -0.449  -0.0430
 -5.03   -0.361  -0.0320
 -3.98   -0.275  -0.0355
 -2.97   -0.183  -0.0331
 -1.94   -0.095  -0.0406
 -0.92   -0.015  -0.0249
  0.06    0.088  -0.0360
  1.13    0.194  -0.0207
  2.18    0.352  -0.0368
  3.21    0.525  -0.0649
  4.25    0.634  -0.0561
  5.26    0.725  -0.0522
  6.27    0.805  -0.0303
  7.30    0.878  -0.0424
  8.31    0.931  -0.0183
  9.33    0.999  -0.0330
 10.34    1.046  -0.0300
 11.34    1.074  -0.0282
 12.29    1.048  -0.0896
 13.23    0.959  -0.1253
 14.20    0.914  -0.1396
 15.22    0.900  -0.1466
 16.18    0.970  -0.1678
 17.20    0.926  -0.1649
 18.15    0.957  -0.1735
 19.16    0.966  -0.1832
 20.14    0.946  -0.1844
 19.65    0.954  -0.1882
 18.62    0.949  -0.1828
 17.66    0.978  -0.1803
 16.62    0.924  -0.1716
 15.64    0.921  -0.1612
 14.71    0.914  -0.1514
 13.70    0.970  -0.1421
 12.76    1.023  -0.1177
 11.83    1.108  -0.0514
 10.83    1.071  -0.0307
  9.78    1.025  -0.0230
  8.79    0.971  -0.0292
  7.80    0.912  -0.0330
  6.78    0.862  -0.0605
  5.71    0.767  -0.0452
  4.72    0.675  -0.0568
  3.70    0.589  -0.0740
  2.61    0.438  -0.0653
  1.63    0.281  -0.0575
  0.61    0.156  -0.0520
 -0.43    0.050  -0.0300
 -1.45   -0.047  -0.0403
 -2.50   -0.125  -0.0598
 -3.52   -0.222  -0.0622
 -4.54   -0.309  -0.0454
 -5.55   -0.385  -0.0726
 -6.56   -0.482  -0.0519
 -7.58   -0.550  -0.0216
 -8.56   -0.571  -0.0048
 -9.56   -0.585  -0.0019
Tabulated from data in file bm05094.dat & reduced using program C10.20

Average Reynolds #:
199941
Number of angles of attack:
61
 alpha  /   Cl   /  Cm
 -9.99   -0.589   0.0367
 -8.95   -0.586   0.0282
 -8.02   -0.590   0.0096
 -7.07   -0.554  -0.0147
 -6.08   -0.479  -0.0408
 -5.06   -0.374  -0.0525
 -3.99   -0.272  -0.0461
 -2.97   -0.157  -0.0531
 -1.98   -0.037  -0.0581
 -0.92    0.076  -0.0617
  0.10    0.214  -0.0693
  1.16    0.350  -0.0766
  2.13    0.453  -0.0751
  3.15    0.546  -0.0703
  4.19    0.658  -0.0683
  5.25    0.753  -0.0634
  6.22    0.835  -0.0591
  7.37    0.917  -0.0542
  8.29    0.985  -0.0489
  9.36    1.043  -0.0429
 10.35    1.095  -0.0371
 11.40    1.127  -0.0314
 12.30    1.148  -0.0868
 13.24    1.079  -0.1345
 14.17    0.991  -0.1556
 15.22    0.969  -0.1588
 16.17    0.979  -0.1630
 17.19    0.949  -0.1622
 18.17    0.931  -0.1606
 19.20    0.939  -0.1691
 20.13    0.954  -0.1737
 19.71    0.924  -0.1661
 18.67    0.927  -0.1635
 17.68    0.937  -0.1643
 16.69    0.974  -0.1678
 15.71    0.969  -0.1617
 14.63    0.983  -0.1604
 13.68    1.043  -0.1485
 12.76    1.102  -0.1203
 11.86    1.110  -0.0494
 10.89    1.110  -0.0364
  9.83    1.071  -0.0416
  8.77    1.013  -0.0471
  7.81    0.958  -0.0532
  6.74    0.882  -0.0577
  5.72    0.797  -0.0620
  4.74    0.718  -0.0684
  3.65    0.609  -0.0719
  2.63    0.507  -0.0755
  1.58    0.405  -0.0779
  0.61    0.292  -0.0778
 -0.44    0.145  -0.0669
 -1.45    0.033  -0.0638
 -2.49   -0.089  -0.0568
 -3.50   -0.207  -0.0504
 -4.55   -0.316  -0.0488
 -5.55   -0.416  -0.0507
 -6.54   -0.511  -0.0306
 -7.57   -0.561  -0.0063
 -8.56   -0.583   0.0139
 -9.50   -0.591   0.0305
Tabulated from data in file bm05078.dat & reduced using program C10.20

Average Reynolds #:
349542
Number of angles of attack:
33
 alpha  /   Cl   /  Cm
 -6.03   -0.446  -0.0483
 -5.02   -0.310  -0.0606
 -3.97   -0.189  -0.0660
 -2.99   -0.062  -0.0734
 -1.94    0.071  -0.0807
 -0.90    0.173  -0.0815
  0.11    0.260  -0.0746
  1.12    0.378  -0.0763
  2.19    0.488  -0.0749
  3.17    0.584  -0.0733
  4.18    0.692  -0.0712
  5.23    0.785  -0.0672
  6.29    0.876  -0.0637
  7.26    0.951  -0.0600
  8.29    1.028  -0.0551
  9.33    1.094  -0.0493
 10.37    1.145  -0.0429
  9.85    1.120  -0.0473
  8.78    1.062  -0.0533
  7.82    0.990  -0.0585
  6.76    0.910  -0.0626
  5.75    0.823  -0.0660
  4.70    0.735  -0.0697
  3.69    0.637  -0.0730
  2.64    0.537  -0.0757
  1.67    0.431  -0.0764
  0.62    0.321  -0.0756
 -0.41    0.214  -0.0782
 -1.47    0.122  -0.0827
 -2.47    0.006  -0.0781
 -3.45   -0.126  -0.0699
 -4.54   -0.259  -0.0622
 -5.57   -0.381  -0.0580
Tabulated from data in file bm05080.dat & reduced using program C10.20

Average Reynolds #:
350076
Number of angles of attack:
21
 alpha  /   Cl   /  Cm
 10.40    1.155  -0.0186
 11.46    1.186  -0.0191
 12.35    1.174  -0.0189
 13.34    1.149  -0.0185
 14.37    1.117  -0.0180
 15.34    1.034  -0.0166
 16.38    0.982  -0.0158
 17.20    0.965  -0.0155
 18.42    0.954  -0.0153
 19.34    0.949  -0.0153
 20.34    0.978  -0.0157
 19.81    0.952  -0.0153
 18.85    0.941  -0.0151
 17.71    0.958  -0.0154
 16.76    0.974  -0.0157
 15.79    1.021  -0.0164
 14.79    1.043  -0.0168
 13.82    1.119  -0.0180
 12.98    1.157  -0.0186
 11.87    1.189  -0.0191
 10.92    1.173  -0.0189
Tabulated from data in file bm05132.dat & reduced using program C10.20

Average Reynolds #:
500252
Number of angles of attack:
35
 alpha  /   Cl   /  Cm
 -6.06   -0.384  -0.0634
 -4.96   -0.250  -0.0722
 -3.99   -0.132  -0.0768
 -2.97   -0.021  -0.0786
 -1.94    0.081  -0.0784
 -0.91    0.170  -0.0755
  0.11    0.263  -0.0712
  1.13    0.383  -0.0716
  2.14    0.494  -0.0723
  3.19    0.599  -0.0704
  4.22    0.698  -0.0677
  5.25    0.788  -0.0646
  6.25    0.876  -0.0616
  7.34    0.963  -0.0579
  8.30    1.042  -0.0537
  9.37    1.106  -0.0479
 10.31    1.160  -0.0420
 11.38    1.189  -0.0363
 10.84    1.187  -0.0401
  9.83    1.131  -0.0458
  8.74    1.072  -0.0517
  7.76    1.005  -0.0566
  6.73    0.917  -0.0605
  5.71    0.829  -0.0636
  4.73    0.739  -0.0665
  3.68    0.645  -0.0698
  2.65    0.550  -0.0727
  1.65    0.440  -0.0726
  0.59    0.320  -0.0708
 -0.40    0.216  -0.0736
 -1.43    0.131  -0.0785
 -2.48    0.029  -0.0792
 -3.55   -0.084  -0.0781
 -4.52   -0.194  -0.0745
 -5.55   -0.316  -0.0706
Tabulated from data in file bm05082.dat & reduced using program C10.20

File sd2030_c.lft created using program C10.20 on Thu May 22 17:01:22 2003
