Airfoil: S834
Builder: Y. Tinel
Comment: 'clean'

Number of Reynolds #'s:
7

Average Reynolds #:
100033
Number of angles of attack:
61
 alpha  /   Cl   /  Cm
-10.31   -0.773  -0.0705
 -9.20   -0.769  -0.0536
 -8.24   -0.740  -0.0658
 -7.21   -0.693  -0.0552
 -6.18   -0.610  -0.0507
 -5.17   -0.516  -0.0473
 -4.12   -0.412  -0.0331
 -3.10   -0.332  -0.0217
 -2.08   -0.255  -0.0114
 -1.02   -0.242   0.0099
  0.01   -0.136  -0.0004
  0.96   -0.035   0.0100
  2.03    0.052  -0.0128
  3.07    0.153  -0.0076
  4.07    0.273  -0.0246
  5.04    0.452  -0.0343
  6.13    0.771  -0.0454
  7.21    0.869  -0.0451
  8.20    0.941  -0.0358
  9.24    0.996  -0.0326
 10.22    1.010  -0.0051
 11.26    1.036  -0.0073
 12.26    1.058   0.0024
 13.27    1.071   0.0044
 14.28    1.060  -0.0091
 15.12    0.851  -0.1012
 16.07    0.832  -0.1101
 17.08    0.767  -0.1180
 18.10    0.792  -0.1359
 19.08    0.802  -0.1471
 20.07    0.875  -0.1620
 19.60    0.848  -0.1608
 18.53    0.818  -0.1419
 17.54    0.789  -0.1272
 16.59    0.809  -0.1245
 15.58    0.796  -0.1059
 14.61    0.958  -0.1010
 13.79    1.079  -0.0004
 12.76    1.070  -0.0024
 11.78    1.059  -0.0006
 10.74    1.031  -0.0129
  9.73    1.011  -0.0169
  8.71    0.984  -0.0283
  7.68    0.917  -0.0447
  6.66    0.836  -0.0538
  5.63    0.695  -0.0567
  4.57    0.364  -0.0130
  3.62    0.236  -0.0051
  2.54    0.127   0.0025
  1.49    0.035   0.0035
  0.46   -0.057   0.0054
 -0.56   -0.168   0.0107
 -1.57   -0.237  -0.0011
 -2.54   -0.278  -0.0128
 -3.61   -0.351  -0.0441
 -4.65   -0.440  -0.0339
 -5.64   -0.537  -0.0395
 -6.71   -0.629  -0.0622
 -7.68   -0.693  -0.0388
 -8.73   -0.740  -0.0791
 -9.79   -0.758  -0.0687
Tabulated from data in file bm05036.dat & reduced using program C10.20

Average Reynolds #:
150063
Number of angles of attack:
61
 alpha  /   Cl   /  Cm
-10.27   -0.809  -0.0526
 -9.25   -0.806  -0.0490
 -8.22   -0.773  -0.0395
 -7.22   -0.704  -0.0315
 -6.21   -0.614  -0.0242
 -5.15   -0.500  -0.0293
 -4.13   -0.388  -0.0312
 -3.09   -0.295  -0.0345
 -2.07   -0.197  -0.0372
 -1.06   -0.111  -0.0263
 -0.01   -0.029  -0.0241
  1.00    0.064  -0.0203
  2.06    0.284  -0.0432
  3.09    0.524  -0.0693
  4.14    0.676  -0.0754
  5.13    0.755  -0.0676
  6.15    0.827  -0.0588
  7.17    0.886  -0.0529
  8.22    0.932  -0.0366
  9.26    0.983  -0.0364
 10.25    1.011  -0.0236
 11.23    1.041  -0.0182
 12.30    1.057  -0.0156
 13.29    1.065  -0.0160
 14.26    1.063  -0.0202
 15.11    0.924  -0.1116
 16.10    0.862  -0.1182
 17.10    0.795  -0.1237
 18.00    0.785  -0.1305
 19.08    0.805  -0.1378
 20.09    0.873  -0.1555
 19.55    0.814  -0.1447
 18.56    0.788  -0.1362
 17.58    0.778  -0.1274
 16.52    0.802  -0.1228
 15.57    0.875  -0.1153
 14.72    1.050  -0.0219
 13.73    1.058  -0.0203
 12.77    1.057  -0.0138
 11.80    1.051  -0.0174
 10.72    1.022  -0.0245
  9.75    0.996  -0.0290
  8.70    0.954  -0.0361
  7.66    0.908  -0.0442
  6.66    0.863  -0.0564
  5.67    0.786  -0.0631
  4.57    0.715  -0.0711
  3.57    0.608  -0.0788
  2.49    0.383  -0.0534
  1.57    0.177  -0.0364
  0.47    0.006  -0.0184
 -0.51   -0.067  -0.0257
 -1.51   -0.140  -0.0320
 -2.57   -0.246  -0.0346
 -3.58   -0.347  -0.0329
 -4.70   -0.445  -0.0340
 -5.66   -0.557  -0.0301
 -6.69   -0.661  -0.0277
 -7.69   -0.737  -0.0403
 -8.74   -0.795  -0.0393
 -9.74   -0.810  -0.0490
Tabulated from data in file bm05038.dat & reduced using program C10.20

Average Reynolds #:
199991
Number of angles of attack:
61
 alpha  /   Cl   /  Cm
-10.31   -0.838  -0.0572
 -9.20   -0.829  -0.0406
 -8.23   -0.778  -0.0372
 -7.20   -0.698  -0.0358
 -6.20   -0.594  -0.0403
 -5.13   -0.468  -0.0457
 -4.12   -0.353  -0.0477
 -3.13   -0.230  -0.0555
 -2.06   -0.110  -0.0584
 -1.09    0.003  -0.0582
 -0.01    0.115  -0.0550
  1.07    0.219  -0.0515
  2.05    0.310  -0.0453
  3.06    0.460  -0.0542
  4.04    0.617  -0.0641
  5.16    0.766  -0.0732
  6.15    0.853  -0.0688
  7.20    0.882  -0.0537
  8.19    0.927  -0.0435
  9.27    0.980  -0.0375
 10.23    1.016  -0.0309
 11.22    1.047  -0.0240
 12.23    1.064  -0.0213
 13.29    1.067  -0.0185
 14.27    1.073  -0.0211
 15.21    1.064  -0.0296
 16.09    0.912  -0.1205
 17.09    0.819  -0.1254
 18.04    0.798  -0.1308
 19.04    0.805  -0.1362
 20.06    0.857  -0.1495
 19.54    0.818  -0.1417
 18.56    0.801  -0.1378
 17.58    0.812  -0.1310
 16.57    0.838  -0.1259
 15.64    0.999  -0.1082
 14.70    1.066  -0.0289
 13.74    1.066  -0.0216
 12.73    1.064  -0.0216
 11.73    1.055  -0.0270
 10.75    1.031  -0.0297
  9.73    0.996  -0.0372
  8.70    0.950  -0.0422
  7.64    0.891  -0.0498
  6.67    0.872  -0.0642
  5.60    0.810  -0.0740
  4.65    0.708  -0.0728
  3.56    0.546  -0.0618
  2.57    0.380  -0.0503
  1.51    0.267  -0.0529
  0.47    0.174  -0.0580
 -0.56    0.067  -0.0597
 -1.55   -0.046  -0.0591
 -2.62   -0.169  -0.0570
 -3.62   -0.290  -0.0529
 -4.62   -0.404  -0.0511
 -5.68   -0.528  -0.0408
 -6.70   -0.646  -0.0351
 -7.74   -0.746  -0.0379
 -8.74   -0.808  -0.0361
 -9.75   -0.840  -0.0522
Tabulated from data in file bm05040.dat & reduced using program C10.20

Average Reynolds #:
350168
Number of angles of attack:
53
 alpha  /   Cl   /  Cm
-10.27   -0.879  -0.0475
 -9.28   -0.798  -0.0498
 -8.21   -0.679  -0.0581
 -7.18   -0.551  -0.0666
 -6.19   -0.429  -0.0724
 -5.14   -0.306  -0.0766
 -4.11   -0.190  -0.0783
 -3.10   -0.085  -0.0786
 -2.05    0.021  -0.0775
 -1.02    0.122  -0.0769
 -0.00    0.223  -0.0753
  0.99    0.324  -0.0734
  2.00    0.424  -0.0708
  3.07    0.520  -0.0668
  4.08    0.604  -0.0613
  5.11    0.689  -0.0558
  6.16    0.786  -0.0559
  7.20    0.855  -0.0495
  8.23    0.913  -0.0435
  9.19    0.978  -0.0398
 10.23    1.031  -0.0351
 11.26    1.067  -0.0302
 12.24    1.088  -0.0270
 13.33    1.088  -0.0260
 14.25    1.084  -0.0328
 15.24    1.073  -0.0453
 16.22    1.053  -0.0594
 15.70    1.063  -0.0519
 14.75    1.078  -0.0379
 13.77    1.091  -0.0272
 12.73    1.087  -0.0258
 11.68    1.075  -0.0284
 10.75    1.050  -0.0324
  9.70    1.002  -0.0377
  8.68    0.944  -0.0419
  7.69    0.880  -0.0459
  6.67    0.840  -0.0566
  5.64    0.742  -0.0562
  4.63    0.648  -0.0597
  3.60    0.563  -0.0651
  2.55    0.468  -0.0694
  1.50    0.375  -0.0730
  0.51    0.277  -0.0752
 -0.50    0.173  -0.0769
 -1.57    0.069  -0.0779
 -2.56   -0.029  -0.0794
 -3.61   -0.144  -0.0794
 -4.63   -0.249  -0.0785
 -5.69   -0.374  -0.0754
 -6.68   -0.492  -0.0705
 -7.70   -0.621  -0.0631
 -8.74   -0.748  -0.0544
 -9.77   -0.844  -0.0493
Tabulated from data in file bm05042.dat & reduced using program C10.20

Average Reynolds #:
349748
Number of angles of attack:
21
 alpha  /   Cl   /  Cm
 10.27    1.053  -0.0169
 11.29    1.087  -0.0175
 12.21    1.098  -0.0177
 13.29    1.102  -0.0177
 14.22    1.100  -0.0177
 15.23    1.083  -0.0174
 16.29    0.999  -0.0161
 17.08    0.855  -0.0138
 18.16    0.842  -0.0135
 19.21    0.824  -0.0133
 20.20    0.855  -0.0137
 19.66    0.837  -0.0135
 18.70    0.833  -0.0134
 17.70    0.850  -0.0137
 16.71    0.933  -0.0150
 15.72    1.062  -0.0171
 14.76    1.093  -0.0176
 13.69    1.109  -0.0178
 12.80    1.105  -0.0178
 11.69    1.089  -0.0175
 10.74    1.075  -0.0173
Tabulated from data in file bm05129.dat & reduced using program C10.20

Average Reynolds #:
499828
Number of angles of attack:
53
 alpha  /   Cl   /  Cm
-10.24   -0.820  -0.0663
 -9.20   -0.707  -0.0735
 -8.18   -0.589  -0.0800
 -7.21   -0.483  -0.0822
 -6.17   -0.381  -0.0811
 -5.11   -0.279  -0.0792
 -4.13   -0.182  -0.0784
 -3.07   -0.076  -0.0776
 -2.05    0.026  -0.0772
 -1.01    0.134  -0.0767
 -0.03    0.235  -0.0762
  1.05    0.341  -0.0749
  2.06    0.449  -0.0744
  3.06    0.547  -0.0727
  4.10    0.648  -0.0699
  5.08    0.734  -0.0648
  6.20    0.797  -0.0546
  7.19    0.851  -0.0470
  8.26    0.923  -0.0421
  9.21    0.991  -0.0385
 10.21    1.044  -0.0343
 11.29    1.088  -0.0296
 12.27    1.113  -0.0267
 13.21    1.130  -0.0275
 14.24    1.122  -0.0396
 15.21    1.086  -0.0565
 16.19    1.074  -0.0675
 15.68    1.074  -0.0626
 14.71    1.095  -0.0488
 13.70    1.131  -0.0310
 12.74    1.130  -0.0267
 11.73    1.112  -0.0279
 10.71    1.068  -0.0317
  9.71    1.015  -0.0361
  8.68    0.953  -0.0402
  7.69    0.888  -0.0445
  6.64    0.822  -0.0502
  5.61    0.761  -0.0595
  4.62    0.693  -0.0678
  3.59    0.598  -0.0714
  2.56    0.502  -0.0739
  1.56    0.397  -0.0749
  0.49    0.288  -0.0760
 -0.54    0.181  -0.0762
 -1.55    0.082  -0.0765
 -2.59   -0.027  -0.0771
 -3.57   -0.129  -0.0779
 -4.64   -0.230  -0.0787
 -5.67   -0.325  -0.0805
 -6.73   -0.432  -0.0817
 -7.72   -0.532  -0.0810
 -8.72   -0.645  -0.0763
 -9.75   -0.769  -0.0693
Tabulated from data in file bm05044.dat & reduced using program C10.20

Average Reynolds #:
499966
Number of angles of attack:
21
 alpha  /   Cl   /  Cm
 10.28    1.060  -0.0170
 11.19    1.095  -0.0176
 12.27    1.125  -0.0181
 13.25    1.136  -0.0183
 14.27    1.116  -0.0179
 15.20    1.085  -0.0174
 16.38    1.058  -0.0170
 17.18    0.894  -0.0144
 18.14    0.851  -0.0137
 19.21    0.864  -0.0139
 20.19    0.882  -0.0142
 19.60    0.875  -0.0141
 18.74    0.867  -0.0139
 17.65    0.877  -0.0141
 16.61    0.940  -0.0151
 15.90    1.066  -0.0171
 14.75    1.099  -0.0177
 13.78    1.125  -0.0181
 12.77    1.132  -0.0182
 11.75    1.120  -0.0180
 10.85    1.088  -0.0175
Tabulated from data in file bm05130.dat & reduced using program C10.20

File s834_c.lft created using program C10.20 on Thu May 22 17:01:22 2003
