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

Number of Reynolds #'s:
7

Average Reynolds #:
100002
Number of angles of attack:
18
 alpha  /   Cl   /  Cd   /  Spanwise Cd's >>>
 -6.02   -0.414   0.0531  0.0529   0.0531   0.0560   0.0558   0.0541   0.0521   0.0506   0.0505
 -4.95   -0.339   0.0321  0.0313   0.0318   0.0339   0.0342   0.0323   0.0317   0.0312   0.0305
 -3.98   -0.262   0.0238  0.0226   0.0228   0.0240   0.0248   0.0249   0.0239   0.0234   0.0238
 -2.99   -0.170   0.0189  0.0185   0.0186   0.0180   0.0189   0.0188   0.0193   0.0190   0.0202
 -1.90   -0.074   0.0136  0.0132   0.0133   0.0137   0.0144   0.0135   0.0126   0.0138   0.0146
 -0.93    0.011   0.0138  0.0151   0.0126   0.0114   0.0125   0.0143   0.0133   0.0147   0.0162
  0.11    0.122   0.0154  0.0190   0.0160   0.0149   0.0151   0.0159   0.0148   0.0132   0.0142
  1.14    0.231   0.0163  0.0163   0.0167   0.0143   0.0159   0.0157   0.0176   0.0170   0.0171
  2.17    0.403   0.0188  0.0195   0.0185   0.0181   0.0188   0.0189   0.0190   0.0187   0.0188
  3.17    0.574   0.0171  0.0175   0.0162   0.0166   0.0166   0.0166   0.0179   0.0172   0.0186
  4.26    0.693   0.0154  0.0154   0.0150   0.0148   0.0140   0.0155   0.0160   0.0156   0.0170
  5.29    0.784   0.0147  0.0153   0.0139   0.0144   0.0151   0.0144   0.0148   0.0144   0.0157
  6.32    0.873   0.0170  0.0153   0.0156   0.0157   0.0160   0.0175   0.0179   0.0180   0.0198
  7.33    0.945   0.0215  0.0218   0.0215   0.0198   0.0217   0.0206   0.0211   0.0217   0.0235
  8.34    1.000   0.0269  0.0275   0.0255   0.0246   0.0260   0.0259   0.0274   0.0276   0.0306
  9.36    1.051   0.0351  0.0353   0.0345   0.0335   0.0337   0.0346   0.0360   0.0361   0.0372
 10.34    1.090   0.0437  0.0405   0.0392   0.0393   0.0415   0.0440   0.0464   0.0486   0.0499
 11.39    1.105   0.0679  0.0691   0.0660   0.0665   0.0669   0.0681   0.0685   0.0682   0.0698
Tabulated from data in file bm05077.dat & reduced using program C10.20

Average Reynolds #:
199829
Number of angles of attack:
18
 alpha  /   Cl   /  Cd   /  Spanwise Cd's >>>
 -6.04   -0.447   0.0550  0.0575   0.0573   0.0558   0.0546   0.0527   0.0535   0.0535   0.0551
 -4.98   -0.336   0.0286  0.0304   0.0295   0.0289   0.0279   0.0269   0.0278   0.0287   0.0288
 -3.95   -0.235   0.0194  0.0203   0.0199   0.0193   0.0194   0.0186   0.0189   0.0193   0.0198
 -2.98   -0.126   0.0163  0.0180   0.0154   0.0156   0.0159   0.0163   0.0159   0.0158   0.0174
 -1.87    0.006   0.0131  0.0145   0.0119   0.0125   0.0139   0.0131   0.0128   0.0132   0.0128
 -0.88    0.115   0.0116  0.0083   0.0160   0.0077   0.0143   0.0107   0.0160   0.0108   0.0088
  0.15    0.252   0.0118  0.0115   0.0135   0.0096   0.0124   0.0115   0.0131   0.0103   0.0129
  1.17    0.391   0.0111  0.0109   0.0121   0.0103   0.0112   0.0110   0.0118   0.0105   0.0113
  2.23    0.499   0.0104  0.0101   0.0104   0.0093   0.0111   0.0114   0.0098   0.0100   0.0109
  3.21    0.593   0.0099  0.0097   0.0105   0.0103   0.0106   0.0103   0.0086   0.0087   0.0106
  4.22    0.690   0.0096  0.0088   0.0089   0.0098   0.0099   0.0104   0.0101   0.0092   0.0095
  5.26    0.784   0.0113  0.0105   0.0110   0.0110   0.0115   0.0118   0.0117   0.0110   0.0116
  6.30    0.869   0.0142  0.0131   0.0139   0.0140   0.0149   0.0148   0.0147   0.0141   0.0143
  7.34    0.945   0.0178  0.0177   0.0169   0.0178   0.0199   0.0177   0.0171   0.0183   0.0172
  8.35    1.012   0.0221  0.0220   0.0206   0.0209   0.0227   0.0223   0.0222   0.0225   0.0233
  9.34    1.070   0.0278  0.0275   0.0274   0.0269   0.0278   0.0277   0.0285   0.0280   0.0285
 10.37    1.112   0.0344  0.0336   0.0335   0.0334   0.0343   0.0349   0.0358   0.0347   0.0349
 11.38    1.138   0.0472  0.0441   0.0450   0.0459   0.0481   0.0489   0.0490   0.0488   0.0481
Tabulated from data in file bm05079.dat & reduced using program C10.20

Average Reynolds #:
204098
Number of angles of attack:
2
 alpha  /   Cl   /  Cd   /  Spanwise Cd's >>>
 12.41    1.072   0.1847  0.1799   0.1885   0.1900   0.1901   0.1879   0.1889   0.1797   0.1727
 13.39    0.996   0.2214  0.2130   0.2141   0.2190   0.2271   0.2355   0.2316   0.2198   0.2114
Tabulated from data in file bm05133.dat & reduced using program C10.20

Average Reynolds #:
349873
Number of angles of attack:
18
 alpha  /   Cl   /  Cd   /  Spanwise Cd's >>>
 -6.53   -0.486   0.0698  0.0729   0.0706   0.0696   0.0672   0.0665   0.0669   0.0701   0.0746
 -5.48   -0.361   0.0371  0.0391   0.0375   0.0380   0.0359   0.0343   0.0362   0.0369   0.0386
 -4.50   -0.246   0.0186  0.0203   0.0202   0.0186   0.0144   0.0179   0.0180   0.0197   0.0197
 -3.44   -0.115   0.0142  0.0151   0.0146   0.0156   0.0158   0.0121   0.0129   0.0134   0.0143
 -2.44    0.024   0.0105  0.0090   0.0108   0.0117   0.0133   0.0076   0.0096   0.0104   0.0114
 -1.36    0.140   0.0085  0.0064   0.0087   0.0092   0.0096   0.0069   0.0073   0.0081   0.0115
 -0.35    0.229   0.0075  0.0070   0.0075   0.0077   0.0065   0.0069   0.0072   0.0065   0.0111
  0.67    0.331   0.0070  0.0085   0.0052   0.0064   0.0061   0.0070   0.0071   0.0061   0.0097
  1.68    0.444   0.0071  0.0064   0.0071   0.0067   0.0073   0.0061   0.0079   0.0065   0.0087
  2.72    0.552   0.0070  0.0066   0.0071   0.0072   0.0067   0.0061   0.0077   0.0067   0.0080
  3.74    0.661   0.0074  0.0073   0.0076   0.0080   0.0074   0.0075   0.0072   0.0070   0.0071
  4.85    0.757   0.0094  0.0094   0.0095   0.0101   0.0098   0.0097   0.0091   0.0090   0.0088
  5.81    0.843   0.0117  0.0117   0.0116   0.0123   0.0122   0.0119   0.0117   0.0112   0.0110
  6.83    0.930   0.0144  0.0147   0.0140   0.0150   0.0150   0.0143   0.0149   0.0139   0.0134
  7.78    1.003   0.0170  0.0174   0.0165   0.0171   0.0171   0.0169   0.0176   0.0171   0.0165
  8.85    1.075   0.0212  0.0217   0.0205   0.0208   0.0216   0.0212   0.0217   0.0215   0.0205
  9.87    1.129   0.0271  0.0272   0.0265   0.0261   0.0278   0.0275   0.0284   0.0268   0.0266
 10.90    1.167   0.0392  0.0378   0.0379   0.0372   0.0392   0.0418   0.0419   0.0394   0.0381
Tabulated from data in file bm05081.dat & reduced using program C10.20

Average Reynolds #:
355456
Number of angles of attack:
2
 alpha  /   Cl   /  Cd   /  Spanwise Cd's >>>
 11.87    1.152   0.1079  0.1125   0.1153   0.1163   0.1147   0.1120   0.1056   0.0974   0.0893
 12.88    1.094   0.1997  0.2045   0.2117   0.2151   0.2138   0.2045   0.1922   0.1810   0.1744
Tabulated from data in file bm05134.dat & reduced using program C10.20

Average Reynolds #:
499053
Number of angles of attack:
18
 alpha  /   Cl   /  Cd   /  Spanwise Cd's >>>
 -6.00   -0.368   0.0445  0.0450   0.0466   0.0463   0.0434   0.0414   0.0424   0.0440   0.0470
 -4.93   -0.238   0.0164  0.0153   0.0186   0.0186   0.0131   0.0165   0.0176   0.0144   0.0172
 -3.95   -0.122   0.0119  0.0111   0.0133   0.0132   0.0115   0.0100   0.0128   0.0112   0.0122
 -2.91   -0.009   0.0105  0.0112   0.0113   0.0109   0.0106   0.0096   0.0102   0.0098   0.0107
 -1.88    0.099   0.0090  0.0111   0.0076   0.0082   0.0112   0.0063   0.0098   0.0068   0.0114
 -0.86    0.186   0.0064  0.0064   0.0053   0.0052   0.0075   0.0059   0.0068   0.0054   0.0090
  0.20    0.291   0.0058  0.0056   0.0051   0.0056   0.0065   0.0048   0.0060   0.0053   0.0076
  1.16    0.410   0.0053  0.0049   0.0052   0.0056   0.0053   0.0049   0.0056   0.0050   0.0063
  2.23    0.525   0.0057  0.0056   0.0060   0.0055   0.0054   0.0058   0.0058   0.0059   0.0057
  3.24    0.628   0.0064  0.0064   0.0068   0.0063   0.0067   0.0066   0.0063   0.0063   0.0062
  4.28    0.725   0.0084  0.0085   0.0085   0.0087   0.0087   0.0086   0.0082   0.0079   0.0080
  5.28    0.814   0.0103  0.0102   0.0103   0.0109   0.0106   0.0106   0.0101   0.0098   0.0098
  6.30    0.909   0.0125  0.0126   0.0123   0.0130   0.0130   0.0126   0.0127   0.0121   0.0117
  7.34    0.993   0.0149  0.0151   0.0143   0.0153   0.0153   0.0149   0.0155   0.0143   0.0141
  8.36    1.068   0.0178  0.0181   0.0171   0.0178   0.0181   0.0177   0.0190   0.0176   0.0170
  9.39    1.134   0.0220  0.0218   0.0211   0.0212   0.0223   0.0222   0.0236   0.0220   0.0214
 10.42    1.176   0.0273  0.0263   0.0262   0.0256   0.0276   0.0286   0.0295   0.0278   0.0271
 11.40    1.199   0.0356  0.0323   0.0323   0.0323   0.0355   0.0411   0.0412   0.0367   0.0337
Tabulated from data in file bm05083.dat & reduced using program C10.20

Average Reynolds #:
501810
Number of angles of attack:
1
 alpha  /   Cl   /  Cd   /  Spanwise Cd's >>>
 12.40    1.205   0.0594  0.0398   0.0412   0.0537   0.0721   0.0791   0.0777   0.0627   0.0487
Tabulated from data in file bm05135.dat & reduced using program C10.20

File sd2030_c.drg created using program C10.20 on Thu May 22 17:01:36 2003
