Airfoil: SD2030 (B)
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 #:
99923
Number of angles of attack:
61
 alpha  /   Cl   /  Cm
-10.01   -0.509   0.0151
 -9.05   -0.520   0.0041
 -8.07   -0.518   0.0029
 -7.03   -0.478  -0.0203
 -6.05   -0.396  -0.0475
 -4.99   -0.303  -0.0512
 -4.01   -0.234  -0.0533
 -2.95   -0.150  -0.0382
 -1.93   -0.066  -0.0473
 -0.89    0.001  -0.0394
  0.13    0.092  -0.0302
  1.15    0.238  -0.0509
  2.18    0.428  -0.0567
  3.17    0.560  -0.0591
  4.22    0.660  -0.0570
  5.24    0.732  -0.0327
  6.29    0.803  -0.0353
  7.32    0.880  -0.0395
  8.29    0.960  -0.0371
  9.35    1.025  -0.0263
 10.33    1.071  -0.0303
 11.36    1.097  -0.0276
 12.27    1.026  -0.0856
 13.21    0.975  -0.1296
 14.21    0.939  -0.1350
 15.22    0.956  -0.1499
 16.18    0.942  -0.1559
 17.20    0.964  -0.1602
 18.20    0.959  -0.1671
 19.14    1.004  -0.1807
 20.18    1.022  -0.1937
 19.66    0.985  -0.1858
 18.69    0.987  -0.1802
 17.64    0.960  -0.1714
 16.67    0.997  -0.1736
 15.66    0.948  -0.1589
 14.65    0.940  -0.1479
 13.67    0.944  -0.1356
 12.75    1.063  -0.1094
 11.79    1.086  -0.0464
 10.83    1.091  -0.0179
  9.83    1.055  -0.0274
  8.83    1.000  -0.0251
  7.83    0.924  -0.0351
  6.70    0.845  -0.0417
  5.79    0.790  -0.0552
  4.70    0.710  -0.0424
  3.67    0.620  -0.0526
  2.72    0.528  -0.0691
  1.61    0.345  -0.0596
  0.59    0.153  -0.0299
 -0.42    0.049  -0.0247
 -1.44   -0.027  -0.0402
 -2.51   -0.101  -0.0468
 -3.48   -0.185  -0.0491
 -4.56   -0.265  -0.0571
 -5.57   -0.347  -0.0540
 -6.58   -0.426  -0.0493
 -7.53   -0.484  -0.0158
 -8.53   -0.505  -0.0020
 -9.56   -0.496   0.0073
Tabulated from data in file bm05095.dat & reduced using program C10.20

Average Reynolds #:
199981
Number of angles of attack:
61
 alpha  /   Cl   /  Cm
-10.03   -0.582   0.0323
 -9.01   -0.569   0.0244
 -8.03   -0.560   0.0075
 -7.03   -0.533  -0.0186
 -6.01   -0.459  -0.0433
 -5.05   -0.360  -0.0525
 -3.98   -0.264  -0.0525
 -3.02   -0.161  -0.0524
 -1.94   -0.004  -0.0651
 -0.98    0.136  -0.0735
  0.11    0.234  -0.0676
  1.18    0.316  -0.0599
  2.18    0.416  -0.0582
  3.15    0.511  -0.0581
  4.22    0.613  -0.0574
  5.23    0.708  -0.0557
  6.25    0.802  -0.0529
  7.27    0.895  -0.0516
  8.33    0.986  -0.0482
  9.30    1.045  -0.0429
 10.32    1.097  -0.0379
 11.35    1.139  -0.0324
 12.26    1.142  -0.0654
 13.26    1.077  -0.1320
 14.21    1.006  -0.1557
 15.20    0.978  -0.1594
 16.17    0.977  -0.1610
 17.20    0.964  -0.1624
 18.17    0.926  -0.1560
 19.16    0.944  -0.1643
 20.16    0.946  -0.1678
 19.71    0.942  -0.1700
 18.63    0.936  -0.1652
 17.65    0.947  -0.1614
 16.68    0.948  -0.1608
 15.66    0.970  -0.1603
 14.65    0.962  -0.1537
 13.71    1.053  -0.1508
 12.75    1.091  -0.1240
 11.89    1.147  -0.0321
 10.86    1.119  -0.0363
  9.81    1.070  -0.0422
  8.83    1.015  -0.0459
  7.83    0.939  -0.0492
  6.79    0.848  -0.0517
  5.68    0.754  -0.0551
  4.70    0.659  -0.0546
  3.68    0.565  -0.0559
  2.68    0.472  -0.0571
  1.63    0.371  -0.0580
  0.65    0.280  -0.0615
 -0.48    0.194  -0.0733
 -1.49    0.066  -0.0675
 -2.46   -0.086  -0.0530
 -3.47   -0.205  -0.0537
 -4.55   -0.314  -0.0467
 -5.57   -0.406  -0.0491
 -6.56   -0.500  -0.0285
 -7.55   -0.548  -0.0014
 -8.53   -0.565   0.0152
 -9.50   -0.571   0.0292
Tabulated from data in file bm05086.dat & reduced using program C10.20

Average Reynolds #:
349925
Number of angles of attack:
37
 alpha  /   Cl   /  Cm
 -6.05   -0.415  -0.0557
 -5.07   -0.280  -0.0666
 -3.99   -0.148  -0.0694
 -2.95   -0.061  -0.0668
 -1.92    0.043  -0.0665
 -0.97    0.137  -0.0664
  0.11    0.247  -0.0661
  1.10    0.347  -0.0658
  2.14    0.448  -0.0649
  3.22    0.554  -0.0642
  4.20    0.660  -0.0630
  5.20    0.758  -0.0615
  6.26    0.855  -0.0598
  7.30    0.948  -0.0571
  8.28    1.032  -0.0540
  9.33    1.103  -0.0485
 10.36    1.145  -0.0410
 11.34    1.161  -0.0345
 12.39    1.159  -0.0762
 11.86    1.169  -0.0337
 10.84    1.152  -0.0386
  9.81    1.124  -0.0462
  8.78    1.070  -0.0530
  7.78    0.990  -0.0563
  6.73    0.902  -0.0597
  5.74    0.805  -0.0618
  4.69    0.706  -0.0634
  3.69    0.608  -0.0648
  2.68    0.504  -0.0655
  1.61    0.393  -0.0660
  0.60    0.292  -0.0667
 -0.44    0.189  -0.0668
 -1.50    0.086  -0.0669
 -2.49   -0.013  -0.0668
 -3.46   -0.104  -0.0678
 -4.54   -0.195  -0.0719
 -5.59   -0.344  -0.0636
Tabulated from data in file bm05088.dat & reduced using program C10.20

Average Reynolds #:
350116
Number of angles of attack:
21
 alpha  /   Cl   /  Cm
 10.41    1.159  -0.0186
 11.45    1.176  -0.0189
 12.32    1.188  -0.0191
 13.32    1.139  -0.0183
 14.30    1.105  -0.0178
 15.31    1.029  -0.0166
 16.28    0.997  -0.0160
 17.19    0.976  -0.0157
 18.42    0.944  -0.0152
 19.26    0.963  -0.0155
 20.34    0.975  -0.0157
 19.73    0.985  -0.0158
 18.85    0.950  -0.0153
 17.82    0.963  -0.0155
 16.72    0.981  -0.0158
 15.89    1.014  -0.0163
 14.76    1.073  -0.0173
 13.96    1.118  -0.0180
 12.89    1.153  -0.0185
 11.91    1.181  -0.0190
 10.85    1.166  -0.0187
Tabulated from data in file bm05131.dat & reduced using program C10.20

Average Reynolds #:
500249
Number of angles of attack:
37
 alpha  /   Cl   /  Cm
 -6.07   -0.354  -0.0698
 -4.98   -0.250  -0.0688
 -4.00   -0.161  -0.0682
 -2.92   -0.058  -0.0671
 -1.91    0.039  -0.0668
 -0.93    0.140  -0.0667
  0.12    0.243  -0.0658
  1.13    0.355  -0.0654
  2.19    0.463  -0.0644
  3.23    0.569  -0.0639
  4.19    0.665  -0.0625
  5.22    0.768  -0.0611
  6.25    0.862  -0.0591
  7.29    0.962  -0.0569
  8.34    1.044  -0.0532
  9.37    1.098  -0.0460
 10.34    1.141  -0.0398
 11.36    1.165  -0.0345
 12.38    1.169  -0.0360
 11.87    1.175  -0.0334
 10.78    1.159  -0.0379
  9.82    1.119  -0.0435
  8.81    1.072  -0.0506
  7.77    0.993  -0.0554
  6.72    0.911  -0.0584
  5.74    0.810  -0.0604
  4.72    0.714  -0.0620
  3.69    0.614  -0.0634
  2.65    0.507  -0.0647
  1.64    0.406  -0.0656
  0.61    0.303  -0.0659
 -0.42    0.188  -0.0664
 -1.42    0.089  -0.0670
 -2.49   -0.016  -0.0672
 -3.52   -0.119  -0.0680
 -4.54   -0.211  -0.0684
 -5.60   -0.305  -0.0713
Tabulated from data in file bm05090.dat & reduced using program C10.20

File sd2030_tf.lft created using program C10.20 on Thu May 22 17:01:22 2003
