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CLARK V AIRFOIL (clarkv-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: CLARK V AIRFOIL (clarkv-il)
Reynolds number: 1,000,000
Max Cl/Cd: 129.42 at α=3.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-clarkv-il-1000000.txt
Download as CSV file: xf-clarkv-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: CLARK V AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.9794   0.04433   0.04185  -0.0886   1.0000   0.0128
 -14.500  -1.0410   0.03676   0.03405  -0.0904   1.0000   0.0126
 -14.250  -1.0684   0.03430   0.03147  -0.0870   0.9993   0.0126
 -14.000  -1.0560   0.03235   0.02937  -0.0882   0.9970   0.0129
 -13.750  -1.0356   0.03058   0.02746  -0.0900   0.9953   0.0132
 -13.500  -1.0134   0.02895   0.02567  -0.0917   0.9942   0.0136
 -13.250  -0.9953   0.02769   0.02428  -0.0918   0.9917   0.0138
 -13.000  -0.9720   0.02678   0.02324  -0.0924   0.9898   0.0141
 -12.750  -0.9556   0.02458   0.02087  -0.0932   0.9875   0.0147
 -12.500  -0.9270   0.02409   0.02035  -0.0943   0.9864   0.0151
 -12.250  -0.8971   0.02373   0.01997  -0.0954   0.9856   0.0156
 -12.000  -0.8676   0.02317   0.01935  -0.0967   0.9848   0.0160
 -11.750  -0.8380   0.02248   0.01857  -0.0980   0.9841   0.0166
 -11.500  -0.8078   0.02178   0.01775  -0.0994   0.9835   0.0171
 -11.250  -0.7897   0.02129   0.01716  -0.0980   0.9794   0.0174
 -11.000  -0.7676   0.01979   0.01549  -0.0982   0.9771   0.0180
 -10.750  -0.7384   0.01925   0.01492  -0.0992   0.9758   0.0186
 -10.500  -0.7068   0.01898   0.01464  -0.1005   0.9749   0.0191
 -10.250  -0.6745   0.01872   0.01435  -0.1018   0.9742   0.0197
 -10.000  -0.6421   0.01830   0.01385  -0.1033   0.9735   0.0205
  -9.750  -0.6099   0.01785   0.01332  -0.1046   0.9729   0.0211
  -9.500  -0.5774   0.01755   0.01293  -0.1059   0.9722   0.0215
  -9.250  -0.5505   0.01600   0.01124  -0.1068   0.9711   0.0225
  -9.000  -0.5317   0.01567   0.01090  -0.1052   0.9662   0.0231
  -8.750  -0.5031   0.01538   0.01059  -0.1056   0.9640   0.0238
  -8.500  -0.4738   0.01502   0.01018  -0.1062   0.9622   0.0245
  -8.250  -0.4441   0.01456   0.00966  -0.1068   0.9606   0.0253
  -8.000  -0.4140   0.01415   0.00918  -0.1074   0.9590   0.0259
  -7.750  -0.3845   0.01394   0.00891  -0.1079   0.9571   0.0263
  -7.500  -0.3665   0.01285   0.00773  -0.1062   0.9520   0.0274
  -7.250  -0.3405   0.01230   0.00716  -0.1060   0.9489   0.0282
  -7.000  -0.3126   0.01189   0.00672  -0.1062   0.9463   0.0289
  -6.750  -0.2844   0.01155   0.00635  -0.1063   0.9439   0.0298
  -6.500  -0.2594   0.01126   0.00602  -0.1058   0.9399   0.0306
  -6.250  -0.2337   0.01091   0.00563  -0.1054   0.9358   0.0313
  -6.000  -0.2063   0.01058   0.00526  -0.1053   0.9323   0.0318
  -5.750  -0.1780   0.01032   0.00495  -0.1054   0.9293   0.0322
  -5.500  -0.1545   0.00972   0.00429  -0.1046   0.9244   0.0335
  -5.250  -0.1285   0.00935   0.00389  -0.1042   0.9198   0.0347
  -5.000  -0.1009   0.00906   0.00358  -0.1042   0.9159   0.0358
  -4.750  -0.0737   0.00883   0.00332  -0.1040   0.9115   0.0368
  -4.500  -0.0471   0.00862   0.00308  -0.1037   0.9060   0.0380
  -4.250  -0.0191   0.00843   0.00286  -0.1037   0.9014   0.0390
  -4.000   0.0080   0.00818   0.00257  -0.1035   0.8963   0.0412
  -3.750   0.0347   0.00797   0.00237  -0.1033   0.8903   0.0442
  -3.500   0.0632   0.00781   0.00217  -0.1033   0.8852   0.0475
  -3.250   0.0897   0.00761   0.00202  -0.1031   0.8787   0.0576
  -3.000   0.1170   0.00739   0.00186  -0.1029   0.8725   0.0769
  -2.750   0.1443   0.00722   0.00174  -0.1028   0.8663   0.0946
  -2.500   0.1709   0.00700   0.00163  -0.1026   0.8592   0.1299
  -2.250   0.1980   0.00681   0.00153  -0.1025   0.8526   0.1666
  -2.000   0.2243   0.00657   0.00144  -0.1023   0.8449   0.2163
  -1.750   0.2505   0.00633   0.00138  -0.1020   0.8366   0.2826
  -1.500   0.2765   0.00615   0.00132  -0.1017   0.8262   0.3386
  -1.250   0.3025   0.00599   0.00128  -0.1013   0.8148   0.3906
  -1.000   0.3283   0.00582   0.00126  -0.1009   0.8046   0.4512
  -0.750   0.3540   0.00565   0.00124  -0.1005   0.7953   0.5174
  -0.500   0.3792   0.00543   0.00124  -0.1000   0.7858   0.5972
  -0.250   0.4030   0.00518   0.00126  -0.0991   0.7764   0.6994
   0.000   0.4261   0.00497   0.00130  -0.0980   0.7662   0.7910
   0.250   0.4501   0.00486   0.00136  -0.0970   0.7559   0.8532
   0.500   0.4745   0.00484   0.00141  -0.0959   0.7443   0.9001
   0.750   0.5001   0.00490   0.00148  -0.0952   0.7299   0.9391
   1.000   0.5309   0.00501   0.00154  -0.0956   0.7124   0.9635
   1.250   0.5653   0.00515   0.00160  -0.0970   0.6959   0.9794
   1.500   0.6025   0.00527   0.00166  -0.0991   0.6813   0.9861
   1.750   0.6417   0.00541   0.00172  -0.1016   0.6647   0.9920
   2.000   0.6790   0.00555   0.00178  -0.1038   0.6480   0.9956
   2.250   0.7158   0.00567   0.00184  -0.1059   0.6317   0.9986
   2.500   0.7454   0.00581   0.00190  -0.1064   0.6154   1.0000
   2.750   0.7670   0.00594   0.00197  -0.1051   0.5989   1.0000
   3.000   0.7879   0.00609   0.00204  -0.1037   0.5807   1.0000
   3.250   0.8089   0.00625   0.00213  -0.1023   0.5605   1.0000
   3.500   0.8288   0.00645   0.00223  -0.1007   0.5366   1.0000
   3.750   0.8488   0.00667   0.00234  -0.0990   0.5115   1.0000
   4.000   0.8684   0.00691   0.00247  -0.0974   0.4860   1.0000
   4.250   0.8876   0.00718   0.00262  -0.0956   0.4563   1.0000
   4.500   0.9072   0.00748   0.00278  -0.0940   0.4259   1.0000
   4.750   0.9272   0.00780   0.00297  -0.0925   0.3959   1.0000
   5.000   0.9473   0.00814   0.00317  -0.0910   0.3655   1.0000
   5.250   0.9686   0.00845   0.00338  -0.0898   0.3403   1.0000
   5.500   0.9900   0.00877   0.00360  -0.0886   0.3175   1.0000
   5.750   1.0110   0.00913   0.00383  -0.0874   0.2913   1.0000
   6.000   1.0322   0.00948   0.00407  -0.0863   0.2661   1.0000
   6.250   1.0532   0.00985   0.00433  -0.0851   0.2425   1.0000
   6.500   1.0739   0.01025   0.00460  -0.0839   0.2171   1.0000
   6.750   1.0945   0.01065   0.00489  -0.0827   0.1950   1.0000
   7.000   1.1150   0.01104   0.00519  -0.0814   0.1758   1.0000
   7.250   1.1363   0.01139   0.00549  -0.0803   0.1619   1.0000
   7.500   1.1570   0.01173   0.00578  -0.0792   0.1489   1.0000
   7.750   1.1765   0.01211   0.00610  -0.0777   0.1344   1.0000
   8.000   1.1944   0.01258   0.00646  -0.0761   0.1161   1.0000
   8.250   1.2118   0.01309   0.00688  -0.0743   0.0972   1.0000
   8.500   1.2291   0.01362   0.00732  -0.0726   0.0825   1.0000
   8.750   1.2461   0.01415   0.00779  -0.0709   0.0694   1.0000
   9.000   1.2613   0.01481   0.00835  -0.0689   0.0521   1.0000
   9.250   1.2720   0.01575   0.00912  -0.0662   0.0306   1.0000
   9.500   1.2867   0.01646   0.00979  -0.0642   0.0228   1.0000
   9.750   1.3022   0.01712   0.01044  -0.0624   0.0195   1.0000
  10.000   1.3189   0.01769   0.01104  -0.0607   0.0180   1.0000
  10.250   1.3332   0.01841   0.01179  -0.0588   0.0164   1.0000
  10.500   1.3487   0.01906   0.01249  -0.0571   0.0156   1.0000
  10.750   1.3646   0.01969   0.01317  -0.0555   0.0149   1.0000
  11.000   1.3794   0.02038   0.01391  -0.0538   0.0143   1.0000
  11.250   1.3927   0.02119   0.01475  -0.0519   0.0136   1.0000
  11.500   1.4010   0.02234   0.01597  -0.0494   0.0128   1.0000
  11.750   1.4142   0.02315   0.01685  -0.0477   0.0124   1.0000
  12.000   1.4275   0.02398   0.01773  -0.0461   0.0121   1.0000
  12.250   1.4394   0.02491   0.01873  -0.0443   0.0117   1.0000
  12.500   1.4503   0.02593   0.01980  -0.0425   0.0113   1.0000
  12.750   1.4604   0.02703   0.02096  -0.0408   0.0110   1.0000
  13.000   1.4691   0.02825   0.02225  -0.0390   0.0107   1.0000
  13.250   1.4746   0.02975   0.02382  -0.0370   0.0104   1.0000
  13.500   1.4738   0.03180   0.02597  -0.0346   0.0100   1.0000
  13.750   1.4726   0.03398   0.02826  -0.0324   0.0098   1.0000
  14.000   1.4801   0.03548   0.02984  -0.0311   0.0097   1.0000
  14.250   1.4862   0.03715   0.03159  -0.0298   0.0095   1.0000
  14.500   1.4905   0.03905   0.03358  -0.0285   0.0094   1.0000
  14.750   1.4938   0.04111   0.03573  -0.0274   0.0092   1.0000
  15.000   1.4968   0.04328   0.03799  -0.0264   0.0090   1.0000
  15.250   1.4986   0.04566   0.04046  -0.0256   0.0088   1.0000
  15.500   1.5002   0.04815   0.04304  -0.0250   0.0086   1.0000
  15.750   1.5006   0.05087   0.04584  -0.0246   0.0085   1.0000
  16.000   1.5001   0.05376   0.04882  -0.0243   0.0083   1.0000
  16.250   1.4980   0.05697   0.05211  -0.0242   0.0082   1.0000
  16.500   1.4937   0.06056   0.05581  -0.0243   0.0081   1.0000
  16.750   1.4869   0.06460   0.05994  -0.0247   0.0080   1.0000
  17.000   1.4776   0.06907   0.06452  -0.0254   0.0079   1.0000
  17.250   1.4655   0.07408   0.06965  -0.0263   0.0078   1.0000
  17.500   1.4513   0.07954   0.07523  -0.0276   0.0077   1.0000
  17.750   1.4350   0.08540   0.08121  -0.0291   0.0076   1.0000
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