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SD7034 (sd7034-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: SD7034 (sd7034-il)
Reynolds number: 200,000
Max Cl/Cd: 77.81 at α=6°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-sd7034-il-200000.txt
Download as CSV file: xf-sd7034-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SD7034                                          
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -8.500  -0.3256   0.09119   0.08797  -0.0423   1.0000   0.0507
  -8.250  -0.3388   0.08881   0.08572  -0.0433   1.0000   0.0508
  -8.000  -0.3700   0.08913   0.08617  -0.0376   1.0000   0.0508
  -7.750  -0.3592   0.08401   0.08107  -0.0374   0.9972   0.0517
  -7.500  -0.3337   0.08094   0.07798  -0.0373   0.9941   0.0531
  -7.250  -0.3097   0.07701   0.07404  -0.0425   0.9867   0.0551
  -7.000  -0.2818   0.07054   0.06754  -0.0557   0.9773   0.0594
  -6.750  -0.2534   0.05881   0.05559  -0.0781   0.9662   0.0630
  -6.500  -0.2273   0.05776   0.05461  -0.0767   0.9616   0.0655
  -6.250  -0.2009   0.05306   0.04979  -0.0834   0.9527   0.0695
  -6.000  -0.1961   0.03196   0.02691  -0.0963   0.9355   0.0421
  -5.750  -0.1718   0.02822   0.02278  -0.0970   0.9286   0.0412
  -5.250  -0.1292   0.02353   0.01746  -0.0960   0.9100   0.0444
  -5.000  -0.1055   0.02201   0.01566  -0.0952   0.9014   0.0462
  -4.750  -0.0812   0.02042   0.01371  -0.0943   0.8930   0.0481
  -4.500  -0.0560   0.01942   0.01233  -0.0933   0.8851   0.0512
  -4.250  -0.0319   0.01814   0.01102  -0.0926   0.8766   0.0548
  -4.000  -0.0065   0.01736   0.01008  -0.0917   0.8691   0.0588
  -3.750   0.0188   0.01644   0.00904  -0.0909   0.8605   0.0640
  -3.500   0.0442   0.01579   0.00836  -0.0900   0.8532   0.0699
  -3.250   0.0696   0.01510   0.00764  -0.0893   0.8445   0.0783
  -3.000   0.0954   0.01452   0.00699  -0.0885   0.8373   0.0893
  -2.750   0.1212   0.01402   0.00654  -0.0880   0.8284   0.1046
  -2.500   0.1471   0.01355   0.00609  -0.0873   0.8213   0.1229
  -2.250   0.1735   0.01320   0.00577  -0.0868   0.8122   0.1472
  -2.000   0.1994   0.01268   0.00541  -0.0863   0.8051   0.1859
  -1.750   0.2249   0.01206   0.00521  -0.0860   0.7957   0.2815
  -1.500   0.2491   0.01134   0.00507  -0.0852   0.7888   0.4551
  -1.250   0.2718   0.01083   0.00509  -0.0840   0.7790   0.6133
  -1.000   0.2920   0.01035   0.00503  -0.0815   0.7718   0.7573
  -0.750   0.3241   0.00994   0.00489  -0.0810   0.7624   0.9368
  -0.500   0.3647   0.00987   0.00464  -0.0833   0.7540   1.0000
  -0.250   0.3913   0.00990   0.00452  -0.0829   0.7446   1.0000
   0.000   0.4180   0.00997   0.00445  -0.0825   0.7349   1.0000
   0.250   0.4450   0.01001   0.00431  -0.0820   0.7266   1.0000
   0.500   0.4719   0.01008   0.00430  -0.0817   0.7158   1.0000
   0.750   0.4989   0.01015   0.00425  -0.0813   0.7063   1.0000
   1.000   0.5261   0.01021   0.00418  -0.0810   0.6967   1.0000
   1.250   0.5531   0.01029   0.00420  -0.0807   0.6858   1.0000
   1.500   0.5803   0.01038   0.00418  -0.0803   0.6758   1.0000
   1.750   0.6075   0.01046   0.00415  -0.0800   0.6655   1.0000
   2.000   0.6345   0.01056   0.00420  -0.0797   0.6539   1.0000
   2.250   0.6615   0.01067   0.00424  -0.0793   0.6427   1.0000
   2.500   0.6887   0.01078   0.00425  -0.0790   0.6321   1.0000
   2.750   0.7156   0.01089   0.00430  -0.0787   0.6200   1.0000
   3.000   0.7424   0.01102   0.00440  -0.0784   0.6076   1.0000
   3.250   0.7692   0.01116   0.00449  -0.0781   0.5953   1.0000
   3.500   0.7960   0.01131   0.00458  -0.0777   0.5832   1.0000
   3.750   0.8227   0.01148   0.00466  -0.0774   0.5707   1.0000
   4.000   0.8492   0.01165   0.00480  -0.0770   0.5576   1.0000
   4.250   0.8755   0.01182   0.00495  -0.0767   0.5437   1.0000
   4.500   0.9016   0.01202   0.00512  -0.0763   0.5297   1.0000
   4.750   0.9276   0.01223   0.00531  -0.0759   0.5154   1.0000
   5.000   0.9534   0.01246   0.00550  -0.0755   0.5009   1.0000
   5.250   0.9790   0.01270   0.00571  -0.0751   0.4860   1.0000
   5.500   1.0044   0.01297   0.00596  -0.0747   0.4710   1.0000
   5.750   1.0295   0.01325   0.00621  -0.0742   0.4556   1.0000
   6.000   1.0543   0.01355   0.00648  -0.0737   0.4401   1.0000
   6.250   1.0788   0.01388   0.00679  -0.0732   0.4244   1.0000
   6.500   1.1031   0.01422   0.00711  -0.0726   0.4087   1.0000
   6.750   1.1269   0.01459   0.00746  -0.0720   0.3930   1.0000
   7.000   1.1504   0.01498   0.00783  -0.0714   0.3771   1.0000
   7.250   1.1734   0.01540   0.00823  -0.0707   0.3612   1.0000
   7.500   1.1959   0.01584   0.00864  -0.0699   0.3453   1.0000
   7.750   1.2179   0.01630   0.00909  -0.0692   0.3294   1.0000
   8.000   1.2393   0.01680   0.00957  -0.0683   0.3136   1.0000
   8.250   1.2602   0.01731   0.01007  -0.0674   0.2980   1.0000
   8.500   1.2805   0.01784   0.01061  -0.0664   0.2825   1.0000
   8.750   1.3001   0.01841   0.01118  -0.0654   0.2673   1.0000
   9.000   1.3189   0.01900   0.01180  -0.0642   0.2522   1.0000
   9.250   1.3367   0.01963   0.01244  -0.0630   0.2372   1.0000
   9.500   1.3533   0.02030   0.01313  -0.0616   0.2223   1.0000
   9.750   1.3686   0.02102   0.01386  -0.0600   0.2074   1.0000
  10.000   1.3820   0.02179   0.01466  -0.0583   0.1924   1.0000
  10.250   1.3922   0.02263   0.01550  -0.0561   0.1783   1.0000
  10.500   1.4000   0.02357   0.01644  -0.0536   0.1643   1.0000
  10.750   1.4066   0.02466   0.01752  -0.0513   0.1506   1.0000
  11.000   1.4118   0.02593   0.01877  -0.0491   0.1376   1.0000
  11.250   1.4154   0.02739   0.02021  -0.0469   0.1254   1.0000
  11.500   1.4186   0.02900   0.02182  -0.0450   0.1142   1.0000
  11.750   1.4227   0.03065   0.02352  -0.0433   0.1039   1.0000
  12.000   1.4249   0.03255   0.02545  -0.0417   0.0953   1.0000
  12.250   1.4231   0.03486   0.02770  -0.0402   0.0885   1.0000
  12.500   1.4280   0.03674   0.02971  -0.0391   0.0817   1.0000
  12.750   1.4247   0.03942   0.03232  -0.0379   0.0765   1.0000
  13.000   1.4291   0.04149   0.03457  -0.0371   0.0713   1.0000
  13.250   1.4282   0.04413   0.03722  -0.0365   0.0672   1.0000
  13.500   1.4280   0.04681   0.03999  -0.0357   0.0634   1.0000
  13.750   1.4293   0.04942   0.04272  -0.0354   0.0597   1.0000
  14.000   1.4281   0.05233   0.04565  -0.0352   0.0567   1.0000
  14.250   1.4279   0.05526   0.04864  -0.0347   0.0539   1.0000
  14.500   1.4283   0.05820   0.05175  -0.0347   0.0513   1.0000
  14.750   1.4281   0.06126   0.05490  -0.0349   0.0489   1.0000
  15.000   1.4279   0.06436   0.05797  -0.0349   0.0465   1.0000
  15.250   1.4285   0.06754   0.06129  -0.0349   0.0445   1.0000
  15.500   1.4269   0.07109   0.06503  -0.0355   0.0428   1.0000
  15.750   1.4259   0.07461   0.06869  -0.0362   0.0410   1.0000
  16.000   1.4257   0.07804   0.07218  -0.0369   0.0395   1.0000
  16.250   1.4298   0.08084   0.07493  -0.0364   0.0374   1.0000
  16.500   1.4234   0.08545   0.07979  -0.0381   0.0366   1.0000
  16.750   1.4176   0.09008   0.08464  -0.0398   0.0355   1.0000
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