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SD7034 (sd7034-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: SD7034 (sd7034-il)
Reynolds number: 50,000
Max Cl/Cd: 37.39 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sd7034-il-50000-n5.txt
Download as CSV file: xf-sd7034-il-50000-n5.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 =     0.050 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -8.500  -0.3312   0.09505   0.08843  -0.0404   1.0000   0.0588
  -8.250  -0.3236   0.09200   0.08543  -0.0395   1.0000   0.0578
  -8.000  -0.3246   0.08907   0.08261  -0.0396   1.0000   0.0572
  -7.750  -0.3311   0.08658   0.08024  -0.0391   1.0000   0.0568
  -7.500  -0.3428   0.08445   0.07826  -0.0380   1.0000   0.0564
  -7.250  -0.3555   0.08219   0.07613  -0.0371   1.0000   0.0562
  -7.000  -0.3681   0.07998   0.07404  -0.0362   1.0000   0.0558
  -6.750  -0.3807   0.07733   0.07145  -0.0360   1.0000   0.0559
  -6.500  -0.3898   0.07449   0.06867  -0.0360   1.0000   0.0554
  -6.250  -0.3678   0.06760   0.06161  -0.0456   0.9890   0.0560
  -6.000  -0.3445   0.06086   0.05462  -0.0539   0.9788   0.0562
  -5.750  -0.3184   0.05441   0.04779  -0.0612   0.9697   0.0561
  -5.500  -0.2910   0.04826   0.04108  -0.0674   0.9606   0.0570
  -5.250  -0.2626   0.04310   0.03521  -0.0719   0.9518   0.0596
  -5.000  -0.2297   0.04061   0.03253  -0.0748   0.9450   0.0627
  -4.750  -0.2001   0.03750   0.02890  -0.0769   0.9366   0.0655
  -4.500  -0.1624   0.03433   0.02481  -0.0799   0.9302   0.0710
  -4.250  -0.1330   0.03253   0.02288  -0.0810   0.9219   0.0747
  -4.000  -0.0957   0.03079   0.02069  -0.0830   0.9156   0.0823
  -3.750  -0.0656   0.02940   0.01911  -0.0836   0.9072   0.0885
  -3.500  -0.0301   0.02817   0.01753  -0.0849   0.9003   0.0991
  -3.250  -0.0013   0.02728   0.01656  -0.0851   0.8915   0.1105
  -3.000   0.0335   0.02637   0.01551  -0.0863   0.8845   0.1271
  -2.750   0.0608   0.02570   0.01481  -0.0862   0.8751   0.1455
  -2.500   0.0953   0.02496   0.01404  -0.0872   0.8682   0.1730
  -2.250   0.1213   0.02440   0.01357  -0.0870   0.8581   0.2069
  -2.000   0.1549   0.02357   0.01301  -0.0880   0.8515   0.2708
  -1.750   0.1775   0.02290   0.01287  -0.0873   0.8408   0.3787
  -1.500   0.2011   0.02210   0.01281  -0.0858   0.8329   0.5635
  -1.250   0.2198   0.02145   0.01280  -0.0823   0.8237   0.7732
  -1.000   0.2725   0.02111   0.01230  -0.0861   0.8161   1.0000
  -0.750   0.3005   0.02125   0.01212  -0.0860   0.8065   1.0000
  -0.500   0.3258   0.02147   0.01208  -0.0856   0.7959   1.0000
  -0.250   0.3573   0.02153   0.01186  -0.0858   0.7883   1.0000
   0.000   0.3806   0.02180   0.01193  -0.0851   0.7767   1.0000
   0.250   0.4067   0.02201   0.01195  -0.0847   0.7666   1.0000
   0.500   0.4360   0.02209   0.01184  -0.0845   0.7580   1.0000
   0.750   0.4598   0.02237   0.01198  -0.0838   0.7465   1.0000
   1.000   0.4865   0.02254   0.01201  -0.0833   0.7366   1.0000
   1.250   0.5144   0.02264   0.01198  -0.0829   0.7272   1.0000
   1.500   0.5384   0.02292   0.01217  -0.0821   0.7155   1.0000
   1.750   0.5648   0.02309   0.01225  -0.0816   0.7053   1.0000
   2.000   0.5928   0.02317   0.01223  -0.0811   0.6957   1.0000
   2.250   0.6166   0.02346   0.01248  -0.0803   0.6836   1.0000
   2.500   0.6420   0.02368   0.01263  -0.0796   0.6724   1.0000
   2.750   0.6714   0.02365   0.01252  -0.0791   0.6635   1.0000
   3.000   0.6948   0.02397   0.01284  -0.0783   0.6507   1.0000
   3.250   0.7191   0.02425   0.01311  -0.0775   0.6385   1.0000
   3.500   0.7447   0.02444   0.01328  -0.0768   0.6269   1.0000
   3.750   0.7730   0.02446   0.01325  -0.0762   0.6168   1.0000
   4.000   0.7968   0.02476   0.01359  -0.0754   0.6037   1.0000
   4.250   0.8207   0.02508   0.01392  -0.0746   0.5907   1.0000
   4.500   0.8451   0.02535   0.01421  -0.0738   0.5778   1.0000
   4.750   0.8702   0.02559   0.01449  -0.0730   0.5653   1.0000
   5.000   0.8959   0.02578   0.01468  -0.0722   0.5529   1.0000
   5.250   0.9218   0.02596   0.01487  -0.0714   0.5403   1.0000
   5.500   0.9448   0.02634   0.01531  -0.0705   0.5262   1.0000
   5.750   0.9678   0.02674   0.01578  -0.0696   0.5122   1.0000
   6.000   0.9908   0.02714   0.01624  -0.0687   0.4981   1.0000
   6.250   1.0137   0.02756   0.01671  -0.0678   0.4839   1.0000
   6.500   1.0364   0.02800   0.01723  -0.0669   0.4698   1.0000
   6.750   1.0588   0.02847   0.01776  -0.0659   0.4555   1.0000
   7.000   1.0808   0.02896   0.01831  -0.0649   0.4411   1.0000
   7.250   1.1023   0.02948   0.01892  -0.0639   0.4266   1.0000
   7.500   1.1234   0.03005   0.01955  -0.0628   0.4122   1.0000
   7.750   1.1438   0.03065   0.02022  -0.0617   0.3976   1.0000
   8.000   1.1636   0.03130   0.02094  -0.0605   0.3831   1.0000
   8.250   1.1826   0.03200   0.02173  -0.0593   0.3686   1.0000
   8.500   1.2008   0.03274   0.02254  -0.0580   0.3541   1.0000
   8.750   1.2180   0.03353   0.02340  -0.0567   0.3396   1.0000
   9.000   1.2342   0.03437   0.02431  -0.0553   0.3252   1.0000
   9.250   1.2490   0.03527   0.02530  -0.0537   0.3109   1.0000
   9.500   1.2621   0.03625   0.02638  -0.0521   0.2966   1.0000
   9.750   1.2723   0.03738   0.02761  -0.0503   0.2825   1.0000
  10.000   1.2804   0.03861   0.02894  -0.0483   0.2687   1.0000
  10.250   1.2854   0.03993   0.03037  -0.0461   0.2556   1.0000
  10.500   1.2897   0.04140   0.03195  -0.0441   0.2429   1.0000
  10.750   1.2931   0.04298   0.03361  -0.0422   0.2306   1.0000
  11.000   1.2962   0.04466   0.03534  -0.0405   0.2187   1.0000
  11.250   1.2994   0.04639   0.03709  -0.0389   0.2072   1.0000
  11.500   1.2984   0.04864   0.03949  -0.0376   0.1959   1.0000
  11.750   1.2968   0.05112   0.04209  -0.0365   0.1852   1.0000
  12.000   1.2966   0.05355   0.04459  -0.0356   0.1752   1.0000
  12.250   1.2974   0.05589   0.04692  -0.0348   0.1657   1.0000
  12.500   1.2917   0.05927   0.05054  -0.0346   0.1564   1.0000
  12.750   1.2900   0.06224   0.05357  -0.0343   0.1482   1.0000
  13.000   1.2872   0.06543   0.05685  -0.0342   0.1402   1.0000
  13.250   1.2815   0.06925   0.06082  -0.0345   0.1331   1.0000
  13.500   1.2800   0.07243   0.06404  -0.0346   0.1262   1.0000
  13.750   1.2721   0.07691   0.06871  -0.0355   0.1205   1.0000
  14.000   1.2667   0.08098   0.07291  -0.0363   0.1148   1.0000
  14.250   1.2623   0.08502   0.07702  -0.0371   0.1097   1.0000
  14.500   1.2474   0.09118   0.08345  -0.0393   0.1057   1.0000
  14.750   1.2455   0.09499   0.08731  -0.0403   0.1010   1.0000
  15.000   1.2364   0.10039   0.09284  -0.0423   0.0975   1.0000
  15.250   1.2098   0.10969   0.10244  -0.0469   0.0956   1.0000
  15.500   1.1715   0.12236   0.11536  -0.0539   0.0947   1.0000
  15.750   1.1044   0.14434   0.13740  -0.0669   0.0947   1.0000
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