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SD7034 (sd7034-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: SD7034 (sd7034-il)
Reynolds number: 100,000
Max Cl/Cd: 54.29 at α=7°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-sd7034-il-100000.txt
Download as CSV file: xf-sd7034-il-100000.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 =     0.100 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -8.250  -0.3036   0.09482   0.09025  -0.0351   1.0000   0.0997
  -8.000  -0.3288   0.09431   0.08994  -0.0377   1.0000   0.1013
  -7.750  -0.3559   0.09407   0.08988  -0.0355   1.0000   0.1015
  -7.500  -0.3836   0.09363   0.08956  -0.0343   1.0000   0.1017
  -7.250  -0.4069   0.09253   0.08853  -0.0349   1.0000   0.1019
  -7.000  -0.3806   0.08756   0.08361  -0.0249   1.0000   0.1045
  -6.750  -0.3886   0.08611   0.08222  -0.0216   1.0000   0.1060
  -6.500  -0.3994   0.08468   0.08086  -0.0195   1.0000   0.1077
  -6.250  -0.3991   0.08203   0.07824  -0.0215   0.9977   0.1112
  -6.000  -0.3714   0.07464   0.07076  -0.0380   0.9872   0.1189
  -5.750  -0.3434   0.07149   0.06760  -0.0392   0.9816   0.1261
  -5.500  -0.3143   0.06606   0.06206  -0.0484   0.9731   0.1367
  -5.250  -0.2864   0.06117   0.05701  -0.0568   0.9636   0.1502
  -5.000  -0.2508   0.05664   0.05231  -0.0642   0.9571   0.1652
  -4.750  -0.2100   0.04060   0.03476  -0.0774   0.9479   0.0890
  -4.500  -0.1673   0.03595   0.02959  -0.0817   0.9435   0.0851
  -4.250  -0.1396   0.03258   0.02571  -0.0828   0.9343   0.0841
  -4.000  -0.0948   0.02946   0.02183  -0.0862   0.9296   0.0862
  -3.750  -0.0651   0.02735   0.01936  -0.0869   0.9208   0.0903
  -3.500  -0.0207   0.02574   0.01749  -0.0899   0.9156   0.0982
  -3.250   0.0127   0.02434   0.01587  -0.0908   0.9076   0.1064
  -3.000   0.0527   0.02314   0.01454  -0.0928   0.9012   0.1206
  -2.750   0.0856   0.02224   0.01364  -0.0935   0.8932   0.1380
  -2.500   0.1215   0.02140   0.01280  -0.0946   0.8858   0.1643
  -2.250   0.1507   0.02072   0.01230  -0.0948   0.8771   0.1963
  -2.000   0.1837   0.01985   0.01174  -0.0954   0.8697   0.2508
  -1.750   0.2075   0.01881   0.01151  -0.0946   0.8602   0.3978
  -1.500   0.2291   0.01761   0.01149  -0.0918   0.8533   0.7077
  -1.250   0.2881   0.01690   0.01103  -0.0958   0.8469   1.0000
  -1.000   0.3172   0.01692   0.01078  -0.0956   0.8379   1.0000
  -0.750   0.3410   0.01711   0.01075  -0.0948   0.8269   1.0000
  -0.500   0.3723   0.01702   0.01043  -0.0946   0.8200   1.0000
  -0.250   0.3951   0.01724   0.01049  -0.0936   0.8080   1.0000
   0.000   0.4204   0.01737   0.01047  -0.0928   0.7978   1.0000
   0.250   0.4492   0.01730   0.01023  -0.0922   0.7898   1.0000
   0.500   0.4730   0.01749   0.01032  -0.0913   0.7781   1.0000
   0.750   0.4996   0.01754   0.01024  -0.0905   0.7686   1.0000
   1.000   0.5269   0.01750   0.01009  -0.0897   0.7593   1.0000
   1.250   0.5515   0.01767   0.01017  -0.0888   0.7477   1.0000
   1.500   0.5786   0.01767   0.01007  -0.0880   0.7383   1.0000
   1.750   0.6055   0.01765   0.00996  -0.0872   0.7282   1.0000
   2.000   0.6305   0.01781   0.01007  -0.0864   0.7163   1.0000
   2.250   0.6571   0.01785   0.01004  -0.0856   0.7058   1.0000
   2.500   0.6851   0.01775   0.00985  -0.0849   0.6963   1.0000
   2.750   0.7102   0.01791   0.00997  -0.0841   0.6836   1.0000
   3.000   0.7361   0.01802   0.01006  -0.0833   0.6715   1.0000
   3.250   0.7631   0.01803   0.01001  -0.0826   0.6603   1.0000
   3.500   0.7910   0.01798   0.00987  -0.0819   0.6496   1.0000
   3.750   0.8164   0.01813   0.01001  -0.0812   0.6361   1.0000
   4.000   0.8421   0.01828   0.01016  -0.0804   0.6228   1.0000
   4.250   0.8681   0.01841   0.01026  -0.0797   0.6094   1.0000
   4.500   0.8943   0.01854   0.01036  -0.0790   0.5962   1.0000
   4.750   0.9206   0.01866   0.01046  -0.0784   0.5827   1.0000
   5.000   0.9469   0.01880   0.01056  -0.0777   0.5691   1.0000
   5.250   0.9731   0.01896   0.01068  -0.0770   0.5549   1.0000
   5.500   0.9989   0.01916   0.01086  -0.0763   0.5403   1.0000
   5.750   1.0243   0.01939   0.01108  -0.0756   0.5252   1.0000
   6.000   1.0493   0.01967   0.01134  -0.0749   0.5096   1.0000
   6.250   1.0739   0.01998   0.01165  -0.0742   0.4937   1.0000
   6.500   1.0981   0.02032   0.01201  -0.0734   0.4776   1.0000
   6.750   1.1220   0.02070   0.01239  -0.0726   0.4613   1.0000
   7.000   1.1455   0.02110   0.01280  -0.0718   0.4448   1.0000
   7.250   1.1688   0.02153   0.01326  -0.0710   0.4284   1.0000
   7.500   1.1917   0.02199   0.01373  -0.0701   0.4118   1.0000
   7.750   1.2142   0.02248   0.01422  -0.0692   0.3953   1.0000
   8.000   1.2363   0.02299   0.01475  -0.0682   0.3787   1.0000
   8.250   1.2578   0.02352   0.01528  -0.0673   0.3621   1.0000
   8.500   1.2788   0.02408   0.01582  -0.0662   0.3454   1.0000
   8.750   1.2992   0.02469   0.01639  -0.0651   0.3288   1.0000
   9.000   1.3174   0.02537   0.01713  -0.0638   0.3118   1.0000
   9.250   1.3344   0.02609   0.01792  -0.0624   0.2947   1.0000
   9.500   1.3504   0.02686   0.01874  -0.0609   0.2776   1.0000
   9.750   1.3653   0.02768   0.01959  -0.0592   0.2608   1.0000
  10.000   1.3787   0.02856   0.02050  -0.0574   0.2441   1.0000
  10.250   1.3906   0.02952   0.02146  -0.0555   0.2278   1.0000
  10.500   1.4004   0.03058   0.02250  -0.0534   0.2118   1.0000
  10.750   1.4084   0.03176   0.02365  -0.0512   0.1964   1.0000
  11.000   1.4132   0.03303   0.02491  -0.0486   0.1820   1.0000
  11.250   1.4145   0.03440   0.02631  -0.0457   0.1689   1.0000
  11.500   1.4160   0.03596   0.02795  -0.0432   0.1565   1.0000
  11.750   1.4178   0.03771   0.02975  -0.0409   0.1451   1.0000
  12.000   1.4202   0.03959   0.03164  -0.0390   0.1348   1.0000
  12.250   1.4262   0.04149   0.03345  -0.0374   0.1252   1.0000
  12.500   1.4264   0.04357   0.03568  -0.0357   0.1171   1.0000
  12.750   1.4304   0.04584   0.03801  -0.0343   0.1094   1.0000
  13.000   1.4363   0.04788   0.04002  -0.0332   0.1024   1.0000
  13.250   1.4375   0.05056   0.04290  -0.0320   0.0967   1.0000
  13.500   1.4413   0.05285   0.04526  -0.0310   0.0911   1.0000
  13.750   1.4471   0.05564   0.04814  -0.0301   0.0860   1.0000
  14.000   1.4421   0.05876   0.05152  -0.0293   0.0824   1.0000
  14.250   1.4629   0.06095   0.05349  -0.0288   0.0765   1.0000
  14.500   1.4497   0.06476   0.05769  -0.0282   0.0748   1.0000
  14.750   1.4381   0.06882   0.06207  -0.0281   0.0728   1.0000
  15.000   1.4280   0.07296   0.06645  -0.0284   0.0707   1.0000
  15.250   1.4238   0.07656   0.07017  -0.0286   0.0682   1.0000
  15.500   1.4334   0.08008   0.07365  -0.0283   0.0651   1.0000
  15.750   1.4113   0.08576   0.07966  -0.0298   0.0647   1.0000
  16.000   1.3877   0.09209   0.08629  -0.0320   0.0644   1.0000
  16.250   1.3622   0.09918   0.09367  -0.0351   0.0643   1.0000
  16.500   1.3344   0.10722   0.10197  -0.0392   0.0644   1.0000
  16.750   1.3051   0.11625   0.11124  -0.0443   0.0647   1.0000
  17.000   1.2740   0.12637   0.12155  -0.0505   0.0651   1.0000
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