Airfoil: S822 (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 #:
99847
Number of angles of attack:
25
 alpha  /   Cl   /  Cd   /  Spanwise Cd's >>>
-10.24   -0.800   0.0373  0.0387   0.0371   0.0377   0.0358   0.0360   0.0372   0.0374   0.0383
 -9.25   -0.797   0.0309  0.0328   0.0329   0.0305   0.0282   0.0311   0.0302   0.0302   0.0314
 -8.29   -0.747   0.0278  0.0281   0.0273   0.0268   0.0271   0.0275   0.0279   0.0277   0.0300
 -7.23   -0.671   0.0253  0.0256   0.0260   0.0245   0.0254   0.0254   0.0243   0.0251   0.0261
 -6.24   -0.598   0.0243  0.0248   0.0256   0.0230   0.0243   0.0239   0.0245   0.0242   0.0238
 -5.19   -0.490   0.0232  0.0233   0.0223   0.0235   0.0237   0.0223   0.0233   0.0231   0.0238
 -4.20   -0.398   0.0225  0.0239   0.0231   0.0221   0.0214   0.0222   0.0217   0.0221   0.0233
 -3.16   -0.301   0.0253  0.0264   0.0272   0.0273   0.0235   0.0233   0.0247   0.0248   0.0252
 -2.13   -0.225   0.0275  0.0262   0.0251   0.0249   0.0266   0.0302   0.0283   0.0280   0.0310
 -1.12   -0.174   0.0304  0.0330   0.0307   0.0298   0.0294   0.0299   0.0299   0.0295   0.0314
 -0.10   -0.114   0.0297  0.0314   0.0304   0.0294   0.0284   0.0291   0.0290   0.0298   0.0296
  0.91   -0.048   0.0334  0.0341   0.0356   0.0338   0.0326   0.0330   0.0323   0.0328   0.0328
  1.94    0.030   0.0353  0.0372   0.0363   0.0355   0.0347   0.0351   0.0339   0.0347   0.0351
  2.98    0.132   0.0414  0.0432   0.0416   0.0423   0.0415   0.0410   0.0406   0.0400   0.0407
  3.97    0.269   0.0416  0.0421   0.0410   0.0408   0.0419   0.0428   0.0418   0.0411   0.0415
  5.12    0.692   0.0283  0.0279   0.0294   0.0288   0.0293   0.0284   0.0269   0.0273   0.0283
  6.18    0.837   0.0199  0.0204   0.0214   0.0204   0.0202   0.0189   0.0213   0.0172   0.0192
  7.19    0.900   0.0191  0.0191   0.0197   0.0197   0.0195   0.0183   0.0203   0.0178   0.0184
  8.23    0.942   0.0229  0.0219   0.0226   0.0240   0.0248   0.0234   0.0229   0.0207   0.0226
  9.13    0.953   0.0288  0.0266   0.0289   0.0310   0.0305   0.0303   0.0293   0.0267   0.0273
 10.16    0.993   0.0328  0.0300   0.0315   0.0341   0.0332   0.0350   0.0350   0.0328   0.0308
 11.15    1.045   0.0401  0.0368   0.0403   0.0432   0.0438   0.0417   0.0406   0.0380   0.0369
 12.20    1.067   0.0501  0.0492   0.0523   0.0542   0.0505   0.0497   0.0505   0.0493   0.0448
 13.20    1.082   0.0633  0.0602   0.0655   0.0717   0.0705   0.0657   0.0610   0.0575   0.0545
 14.22    1.085   0.0800  0.0828   0.0860   0.0878   0.0890   0.0831   0.0758   0.0684   0.0667
Tabulated from data in file bm05027.dat & reduced using program C10.20

Average Reynolds #:
150122
Number of angles of attack:
25
 alpha  /   Cl   /  Cd   /  Spanwise Cd's >>>
-10.33   -0.855   0.0320  0.0342   0.0334   0.0338   0.0320   0.0307   0.0305   0.0310   0.0303
 -9.27   -0.823   0.0281  0.0312   0.0292   0.0291   0.0266   0.0264   0.0265   0.0282   0.0275
 -8.24   -0.741   0.0253  0.0257   0.0252   0.0262   0.0253   0.0245   0.0253   0.0252   0.0248
 -7.23   -0.638   0.0243  0.0248   0.0245   0.0253   0.0247   0.0232   0.0233   0.0243   0.0239
 -6.27   -0.546   0.0232  0.0234   0.0233   0.0235   0.0229   0.0230   0.0234   0.0230   0.0229
 -5.18   -0.436   0.0222  0.0227   0.0220   0.0235   0.0216   0.0215   0.0221   0.0223   0.0219
 -4.16   -0.330   0.0224  0.0228   0.0229   0.0235   0.0221   0.0219   0.0222   0.0219   0.0216
 -3.13   -0.237   0.0231  0.0238   0.0238   0.0239   0.0222   0.0229   0.0226   0.0226   0.0225
 -2.08   -0.140   0.0249  0.0255   0.0251   0.0253   0.0261   0.0236   0.0251   0.0242   0.0245
 -1.10   -0.063   0.0270  0.0272   0.0274   0.0274   0.0280   0.0262   0.0271   0.0261   0.0271
 -0.07    0.037   0.0286  0.0299   0.0289   0.0292   0.0280   0.0280   0.0284   0.0278   0.0286
  1.02    0.242   0.0240  0.0251   0.0251   0.0242   0.0242   0.0235   0.0238   0.0216   0.0246
  2.03    0.349   0.0190  0.0230   0.0234   0.0183   0.0169   0.0149   0.0184   0.0153   0.0218
  3.07    0.449   0.0164  0.0172   0.0200   0.0154   0.0159   0.0144   0.0178   0.0136   0.0171
  4.08    0.569   0.0154  0.0150   0.0166   0.0141   0.0167   0.0169   0.0154   0.0139   0.0143
  5.13    0.709   0.0171  0.0151   0.0196   0.0185   0.0178   0.0180   0.0150   0.0170   0.0155
  6.11    0.713   0.0188  0.0184   0.0192   0.0195   0.0205   0.0207   0.0181   0.0173   0.0168
  7.12    0.772   0.0213  0.0202   0.0213   0.0219   0.0228   0.0224   0.0208   0.0205   0.0209
  8.13    0.845   0.0245  0.0238   0.0241   0.0247   0.0266   0.0256   0.0239   0.0236   0.0237
  9.21    0.908   0.0276  0.0261   0.0269   0.0288   0.0296   0.0281   0.0282   0.0268   0.0264
 10.15    0.971   0.0312  0.0295   0.0303   0.0339   0.0340   0.0320   0.0309   0.0298   0.0295
 11.21    1.027   0.0383  0.0353   0.0379   0.0428   0.0439   0.0400   0.0371   0.0349   0.0343
 12.23    1.044   0.0488  0.0428   0.0475   0.0547   0.0608   0.0516   0.0467   0.0443   0.0419
 13.26    1.056   0.0606  0.0574   0.0622   0.0691   0.0714   0.0669   0.0580   0.0504   0.0494
 14.19    1.064   0.0773  0.0778   0.0804   0.0842   0.0840   0.0805   0.0745   0.0691   0.0675
Tabulated from data in file bm05029.dat & reduced using program C10.20

Average Reynolds #:
200042
Number of angles of attack:
24
 alpha  /   Cl   /  Cd   /  Spanwise Cd's >>>
-10.24   -0.810   0.0285  0.0280   0.0279   0.0282   0.0271   0.0275   0.0287   0.0297   0.0311
 -9.30   -0.733   0.0245  0.0259   0.0243   0.0253   0.0241   0.0235   0.0242   0.0240   0.0248
 -8.20   -0.623   0.0222  0.0226   0.0218   0.0234   0.0219   0.0215   0.0217   0.0224   0.0223
 -7.18   -0.517   0.0212  0.0212   0.0215   0.0225   0.0208   0.0207   0.0210   0.0209   0.0209
 -6.18   -0.409   0.0207  0.0209   0.0210   0.0219   0.0203   0.0206   0.0205   0.0204   0.0202
 -5.14   -0.305   0.0207  0.0213   0.0210   0.0218   0.0204   0.0202   0.0206   0.0204   0.0197
 -4.10   -0.202   0.0209  0.0216   0.0215   0.0215   0.0209   0.0205   0.0206   0.0206   0.0202
 -3.12   -0.111   0.0210  0.0217   0.0217   0.0211   0.0208   0.0204   0.0207   0.0211   0.0204
 -2.07   -0.018   0.0216  0.0226   0.0224   0.0214   0.0215   0.0216   0.0213   0.0209   0.0214
 -1.04    0.089   0.0187  0.0225   0.0220   0.0184   0.0180   0.0173   0.0166   0.0143   0.0203
 -0.02    0.206   0.0145  0.0134   0.0197   0.0136   0.0134   0.0121   0.0163   0.0117   0.0156
  1.01    0.294   0.0128  0.0131   0.0144   0.0122   0.0124   0.0127   0.0138   0.0116   0.0126
  2.04    0.353   0.0149  0.0150   0.0147   0.0145   0.0175   0.0131   0.0198   0.0120   0.0127
  3.04    0.416   0.0160  0.0149   0.0152   0.0135   0.0199   0.0144   0.0209   0.0127   0.0163
  4.05    0.480   0.0166  0.0143   0.0153   0.0178   0.0176   0.0167   0.0189   0.0172   0.0152
  5.07    0.589   0.0182  0.0162   0.0167   0.0209   0.0201   0.0202   0.0157   0.0194   0.0163
  6.10    0.661   0.0192  0.0185   0.0194   0.0191   0.0196   0.0204   0.0188   0.0188   0.0188
  7.12    0.749   0.0211  0.0206   0.0210   0.0212   0.0221   0.0227   0.0208   0.0203   0.0205
  8.15    0.830   0.0239  0.0229   0.0235   0.0244   0.0261   0.0252   0.0238   0.0231   0.0225
  9.17    0.900   0.0266  0.0250   0.0260   0.0271   0.0292   0.0284   0.0270   0.0255   0.0248
 10.15    0.964   0.0298  0.0268   0.0283   0.0323   0.0359   0.0310   0.0288   0.0275   0.0275
 11.21    1.022   0.0361  0.0336   0.0343   0.0371   0.0402   0.0389   0.0380   0.0347   0.0324
 12.20    1.048   0.0462  0.0439   0.0450   0.0452   0.0471   0.0509   0.0525   0.0455   0.0399
 13.21    1.060   0.0583  0.0537   0.0594   0.0673   0.0701   0.0655   0.0558   0.0476   0.0467
Tabulated from data in file bm05031.dat & reduced using program C10.20

Average Reynolds #:
350505
Number of angles of attack:
24
 alpha  /   Cl   /  Cd   /  Spanwise Cd's >>>
-10.24   -0.651   0.0224  0.0218   0.0220   0.0242   0.0212   0.0211   0.0224   0.0233   0.0236
 -9.20   -0.610   0.0180  0.0185   0.0178   0.0191   0.0171   0.0174   0.0176   0.0183   0.0180
 -8.20   -0.531   0.0169  0.0168   0.0172   0.0183   0.0161   0.0167   0.0170   0.0169   0.0164
 -7.18   -0.448   0.0164  0.0162   0.0167   0.0178   0.0158   0.0164   0.0161   0.0159   0.0159
 -6.18   -0.355   0.0155  0.0153   0.0160   0.0167   0.0152   0.0154   0.0152   0.0153   0.0152
 -5.10   -0.251   0.0151  0.0151   0.0157   0.0160   0.0152   0.0146   0.0146   0.0149   0.0146
 -4.11   -0.159   0.0143  0.0144   0.0159   0.0145   0.0146   0.0119   0.0156   0.0130   0.0147
 -3.06   -0.074   0.0137  0.0124   0.0162   0.0136   0.0141   0.0131   0.0124   0.0146   0.0129
 -2.07   -0.007   0.0144  0.0139   0.0147   0.0147   0.0152   0.0141   0.0136   0.0150   0.0144
 -1.02    0.084   0.0148  0.0152   0.0156   0.0143   0.0152   0.0147   0.0141   0.0147   0.0145
 -0.04    0.180   0.0150  0.0153   0.0153   0.0144   0.0157   0.0151   0.0145   0.0147   0.0150
  0.98    0.269   0.0154  0.0154   0.0154   0.0150   0.0158   0.0156   0.0153   0.0152   0.0154
  2.01    0.361   0.0159  0.0156   0.0157   0.0158   0.0158   0.0163   0.0162   0.0156   0.0159
  3.07    0.456   0.0164  0.0158   0.0162   0.0165   0.0161   0.0169   0.0166   0.0161   0.0166
  4.12    0.550   0.0175  0.0169   0.0174   0.0175   0.0178   0.0181   0.0175   0.0171   0.0174
  5.10    0.632   0.0184  0.0176   0.0185   0.0185   0.0188   0.0199   0.0181   0.0178   0.0182
  6.10    0.714   0.0188  0.0187   0.0187   0.0186   0.0192   0.0206   0.0185   0.0180   0.0186
  7.14    0.790   0.0200  0.0200   0.0200   0.0206   0.0205   0.0221   0.0201   0.0191   0.0177
  8.13    0.854   0.0221  0.0210   0.0219   0.0221   0.0243   0.0245   0.0213   0.0205   0.0210
  9.18    0.921   0.0251  0.0234   0.0241   0.0247   0.0289   0.0297   0.0248   0.0227   0.0223
 10.20    0.986   0.0282  0.0246   0.0256   0.0285   0.0357   0.0343   0.0287   0.0248   0.0235
 11.16    1.048   0.0326  0.0309   0.0302   0.0323   0.0369   0.0387   0.0356   0.0289   0.0275
 12.22    1.095   0.0402  0.0372   0.0332   0.0363   0.0460   0.0473   0.0441   0.0396   0.0379
 13.25    1.126   0.0543  0.0454   0.0498   0.0616   0.0743   0.0704   0.0552   0.0409   0.0371
Tabulated from data in file bm05033.dat & reduced using program C10.20

Average Reynolds #:
499806
Number of angles of attack:
24
 alpha  /   Cl   /  Cd   /  Spanwise Cd's >>>
-10.25   -0.666   0.0214  0.0213   0.0215   0.0228   0.0208   0.0202   0.0212   0.0220   0.0217
 -9.22   -0.620   0.0178  0.0179   0.0171   0.0188   0.0165   0.0164   0.0179   0.0190   0.0184
 -8.17   -0.549   0.0155  0.0156   0.0157   0.0167   0.0149   0.0155   0.0156   0.0154   0.0150
 -7.14   -0.452   0.0146  0.0143   0.0151   0.0160   0.0141   0.0146   0.0145   0.0142   0.0142
 -6.23   -0.365   0.0141  0.0137   0.0146   0.0153   0.0135   0.0140   0.0137   0.0138   0.0138
 -5.14   -0.267   0.0131  0.0125   0.0145   0.0131   0.0136   0.0124   0.0126   0.0127   0.0132
 -4.12   -0.187   0.0134  0.0129   0.0141   0.0144   0.0138   0.0126   0.0124   0.0139   0.0132
 -3.09   -0.097   0.0136  0.0140   0.0144   0.0141   0.0136   0.0132   0.0125   0.0137   0.0132
 -2.03    0.001   0.0137  0.0143   0.0144   0.0136   0.0140   0.0133   0.0128   0.0142   0.0131
 -1.06    0.087   0.0140  0.0145   0.0146   0.0137   0.0147   0.0136   0.0135   0.0142   0.0135
 -0.03    0.184   0.0143  0.0144   0.0146   0.0138   0.0151   0.0142   0.0141   0.0142   0.0141
  1.04    0.281   0.0148  0.0148   0.0147   0.0142   0.0152   0.0150   0.0149   0.0148   0.0148
  2.00    0.369   0.0150  0.0151   0.0147   0.0145   0.0147   0.0149   0.0153   0.0142   0.0164
  3.06    0.446   0.0156  0.0158   0.0157   0.0153   0.0162   0.0159   0.0154   0.0161   0.0148
  4.06    0.523   0.0166  0.0166   0.0162   0.0160   0.0175   0.0170   0.0163   0.0170   0.0159
  5.17    0.605   0.0178  0.0171   0.0174   0.0170   0.0194   0.0185   0.0175   0.0181   0.0172
  6.10    0.686   0.0188  0.0183   0.0178   0.0180   0.0214   0.0194   0.0183   0.0189   0.0183
  7.18    0.760   0.0211  0.0199   0.0191   0.0202   0.0250   0.0228   0.0204   0.0205   0.0204
  8.15    0.879   0.0233  0.0215   0.0225   0.0223   0.0251   0.0298   0.0225   0.0210   0.0217
  9.20    0.933   0.0246  0.0219   0.0239   0.0240   0.0278   0.0312   0.0239   0.0222   0.0218
 10.15    0.993   0.0278  0.0249   0.0251   0.0262   0.0327   0.0347   0.0289   0.0246   0.0250
 11.19    1.051   0.0351  0.0305   0.0305   0.0348   0.0450   0.0455   0.0357   0.0300   0.0291
 12.25    1.085   0.0477  0.0370   0.0399   0.0537   0.0683   0.0660   0.0506   0.0348   0.0316
 13.19    1.096   0.0664  0.0592   0.0683   0.0786   0.0850   0.0793   0.0688   0.0513   0.0405
Tabulated from data in file bm05035.dat & reduced using program C10.20

File s822_tf.drg created using program C10.20 on Thu May 22 17:01:35 2003
