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:
4

Average Reynolds #:
100118
Number of angles of attack:
19
 alpha  /   Cl   /  Cd   /  Spanwise Cd's >>>
 -5.95   -0.391   0.0523  0.0536   0.0541   0.0566   0.0543   0.0519   0.0503   0.0482   0.0493
 -4.96   -0.319   0.0315  0.0312   0.0317   0.0326   0.0320   0.0314   0.0311   0.0313   0.0309
 -3.96   -0.250   0.0236  0.0232   0.0233   0.0237   0.0239   0.0235   0.0236   0.0236   0.0241
 -2.94   -0.166   0.0187  0.0193   0.0188   0.0189   0.0189   0.0182   0.0185   0.0187   0.0182
 -1.92   -0.072   0.0154  0.0161   0.0150   0.0138   0.0171   0.0152   0.0153   0.0155   0.0156
 -0.87    0.006   0.0141  0.0152   0.0136   0.0147   0.0154   0.0138   0.0113   0.0138   0.0154
  0.10    0.105   0.0148  0.0145   0.0145   0.0144   0.0145   0.0151   0.0153   0.0150   0.0148
  1.21    0.267   0.0165  0.0166   0.0161   0.0164   0.0160   0.0169   0.0164   0.0159   0.0173
  2.18    0.438   0.0157  0.0167   0.0151   0.0149   0.0155   0.0158   0.0156   0.0154   0.0167
  3.25    0.557   0.0146  0.0140   0.0134   0.0125   0.0137   0.0154   0.0157   0.0159   0.0161
  4.27    0.659   0.0137  0.0151   0.0144   0.0133   0.0123   0.0130   0.0137   0.0135   0.0146
  5.31    0.736   0.0157  0.0151   0.0154   0.0150   0.0157   0.0153   0.0163   0.0161   0.0167
  6.29    0.804   0.0193  0.0194   0.0202   0.0182   0.0192   0.0186   0.0196   0.0191   0.0204
  7.30    0.879   0.0228  0.0213   0.0223   0.0224   0.0222   0.0227   0.0238   0.0233   0.0246
  8.32    0.958   0.0269  0.0269   0.0267   0.0260   0.0259   0.0264   0.0265   0.0271   0.0294
  9.32    1.015   0.0334  0.0335   0.0333   0.0321   0.0322   0.0319   0.0338   0.0342   0.0365
 10.37    1.060   0.0443  0.0460   0.0466   0.0443   0.0427   0.0430   0.0437   0.0434   0.0448
 11.39    1.080   0.0709  0.0656   0.0652   0.0661   0.0677   0.0703   0.0758   0.0771   0.0794
 12.40    0.999   0.1818  0.1663   0.1712   0.1791   0.1798   0.1809   0.1882   0.1934   0.1954
Tabulated from data in file bm05085.dat & reduced using program C10.20

Average Reynolds #:
200033
Number of angles of attack:
19
 alpha  /   Cl   /  Cd   /  Spanwise Cd's >>>
 -6.02   -0.440   0.0546  0.0573   0.0559   0.0560   0.0522   0.0497   0.0522   0.0554   0.0579
 -5.02   -0.351   0.0295  0.0308   0.0307   0.0299   0.0290   0.0283   0.0283   0.0295   0.0295
 -3.98   -0.252   0.0186  0.0196   0.0190   0.0188   0.0191   0.0178   0.0178   0.0182   0.0189
 -2.93   -0.139   0.0164  0.0194   0.0151   0.0145   0.0170   0.0166   0.0157   0.0155   0.0177
 -1.90    0.012   0.0137  0.0165   0.0166   0.0104   0.0111   0.0109   0.0125   0.0164   0.0150
 -0.89    0.159   0.0112  0.0118   0.0120   0.0105   0.0107   0.0107   0.0095   0.0107   0.0137
  0.18    0.253   0.0110  0.0125   0.0110   0.0110   0.0119   0.0120   0.0103   0.0103   0.0090
  1.14    0.336   0.0123  0.0130   0.0127   0.0124   0.0121   0.0126   0.0124   0.0117   0.0115
  2.19    0.437   0.0130  0.0130   0.0135   0.0130   0.0129   0.0135   0.0129   0.0127   0.0125
  3.16    0.535   0.0136  0.0134   0.0136   0.0137   0.0139   0.0140   0.0133   0.0132   0.0134
  4.27    0.635   0.0148  0.0141   0.0150   0.0152   0.0155   0.0155   0.0145   0.0142   0.0144
  5.29    0.735   0.0162  0.0158   0.0159   0.0165   0.0167   0.0169   0.0164   0.0157   0.0158
  6.30    0.824   0.0174  0.0165   0.0174   0.0178   0.0180   0.0177   0.0176   0.0170   0.0168
  7.36    0.917   0.0193  0.0188   0.0189   0.0197   0.0197   0.0195   0.0201   0.0179   0.0198
  8.31    0.999   0.0218  0.0214   0.0215   0.0216   0.0223   0.0217   0.0222   0.0213   0.0225
  9.37    1.062   0.0285  0.0283   0.0279   0.0277   0.0288   0.0290   0.0288   0.0283   0.0290
 10.37    1.108   0.0329  0.0337   0.0348   0.0330   0.0323   0.0329   0.0324   0.0320   0.0323
 11.42    1.145   0.0416  0.0387   0.0396   0.0394   0.0405   0.0434   0.0451   0.0431   0.0431
 12.36    1.067   0.1738  0.1664   0.1749   0.1816   0.1796   0.1753   0.1773   0.1700   0.1652
Tabulated from data in file bm05087.dat & reduced using program C10.20

Average Reynolds #:
350702
Number of angles of attack:
19
 alpha  /   Cl   /  Cd   /  Spanwise Cd's >>>
 -6.02   -0.406   0.0482  0.0527   0.0524   0.0481   0.0420   0.0418   0.0470   0.0491   0.0522
 -4.97   -0.260   0.0187  0.0175   0.0244   0.0184   0.0173   0.0160   0.0167   0.0183   0.0212
 -3.95   -0.146   0.0141  0.0142   0.0141   0.0140   0.0151   0.0130   0.0129   0.0154   0.0140
 -2.94   -0.056   0.0132  0.0134   0.0138   0.0134   0.0138   0.0123   0.0124   0.0137   0.0127
 -1.89    0.047   0.0130  0.0134   0.0132   0.0123   0.0139   0.0127   0.0124   0.0129   0.0128
 -0.82    0.150   0.0129  0.0130   0.0130   0.0125   0.0138   0.0129   0.0127   0.0128   0.0129
  0.12    0.248   0.0132  0.0131   0.0132   0.0132   0.0133   0.0133   0.0132   0.0132   0.0133
  1.18    0.360   0.0135  0.0132   0.0137   0.0137   0.0133   0.0138   0.0135   0.0135   0.0134
  2.21    0.459   0.0138  0.0133   0.0142   0.0140   0.0139   0.0142   0.0136   0.0137   0.0135
  3.27    0.565   0.0145  0.0140   0.0147   0.0145   0.0150   0.0148   0.0143   0.0143   0.0142
  4.21    0.666   0.0152  0.0150   0.0154   0.0158   0.0159   0.0156   0.0148   0.0145   0.0148
  5.28    0.769   0.0162  0.0158   0.0160   0.0171   0.0166   0.0168   0.0161   0.0153   0.0155
  6.31    0.868   0.0170  0.0170   0.0169   0.0176   0.0176   0.0173   0.0174   0.0163   0.0159
  7.27    0.953   0.0174  0.0176   0.0170   0.0178   0.0181   0.0174   0.0182   0.0167   0.0166
  8.35    1.044   0.0190  0.0191   0.0184   0.0187   0.0195   0.0186   0.0200   0.0190   0.0190
  9.32    1.111   0.0237  0.0221   0.0214   0.0220   0.0240   0.0247   0.0257   0.0250   0.0244
 10.39    1.149   0.0315  0.0287   0.0281   0.0296   0.0320   0.0332   0.0352   0.0327   0.0325
 11.37    1.164   0.0426  0.0393   0.0394   0.0399   0.0437   0.0464   0.0470   0.0437   0.0414
 12.29    1.117   0.1592  0.1541   0.1630   0.1717   0.1671   0.1655   0.1609   0.1493   0.1417
Tabulated from data in file bm05089.dat & reduced using program C10.20

Average Reynolds #:
499335
Number of angles of attack:
19
 alpha  /   Cl   /  Cd   /  Spanwise Cd's >>>
 -5.98   -0.340   0.0411  0.0415   0.0417   0.0425   0.0400   0.0381   0.0390   0.0417   0.0443
 -5.02   -0.256   0.0180  0.0179   0.0184   0.0189   0.0184   0.0166   0.0165   0.0187   0.0186
 -3.92   -0.149   0.0144  0.0153   0.0151   0.0147   0.0145   0.0136   0.0133   0.0150   0.0140
 -2.91   -0.056   0.0129  0.0136   0.0134   0.0129   0.0134   0.0123   0.0124   0.0129   0.0121
 -1.92    0.046   0.0122  0.0128   0.0126   0.0119   0.0131   0.0116   0.0119   0.0122   0.0118
 -0.86    0.149   0.0123  0.0125   0.0123   0.0119   0.0131   0.0121   0.0120   0.0120   0.0121
  0.17    0.251   0.0124  0.0123   0.0122   0.0123   0.0127   0.0124   0.0122   0.0124   0.0125
  1.21    0.366   0.0127  0.0122   0.0127   0.0131   0.0124   0.0129   0.0127   0.0126   0.0127
  2.21    0.474   0.0131  0.0125   0.0133   0.0133   0.0130   0.0134   0.0131   0.0131   0.0130
  3.27    0.576   0.0134  0.0127   0.0137   0.0134   0.0136   0.0137   0.0133   0.0133   0.0134
  4.27    0.675   0.0142  0.0138   0.0143   0.0145   0.0147   0.0147   0.0139   0.0137   0.0139
  5.30    0.777   0.0149  0.0148   0.0150   0.0158   0.0154   0.0153   0.0147   0.0141   0.0145
  6.28    0.874   0.0161  0.0160   0.0159   0.0171   0.0165   0.0163   0.0161   0.0152   0.0155
  7.37    0.975   0.0173  0.0174   0.0168   0.0179   0.0178   0.0172   0.0182   0.0166   0.0167
  8.35    1.059   0.0198  0.0191   0.0181   0.0194   0.0204   0.0200   0.0219   0.0200   0.0193
  9.40    1.108   0.0247  0.0240   0.0233   0.0232   0.0254   0.0259   0.0270   0.0249   0.0239
 10.39    1.149   0.0299  0.0293   0.0282   0.0288   0.0302   0.0317   0.0325   0.0297   0.0290
 11.42    1.171   0.0392  0.0357   0.0360   0.0369   0.0409   0.0448   0.0437   0.0392   0.0366
 12.41    1.159   0.0675  0.0430   0.0476   0.0625   0.0804   0.0900   0.0870   0.0722   0.0574
Tabulated from data in file bm05091.dat & reduced using program C10.20

File sd2030_tf.drg created using program C10.20 on Thu May 22 17:01:36 2003
