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NACA 63A210 (naca63a210-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: NACA 63A210 (naca63a210-il)
Reynolds number: 50,000
Max Cl/Cd: 31.28 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca63a210-il-50000-n5.txt
Download as CSV file: xf-naca63a210-il-50000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63A210                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
  -9.500  -0.5806   0.09172   0.08522  -0.0203   1.0000   0.0520
  -9.250  -0.5856   0.08558   0.07913  -0.0247   1.0000   0.0509
  -9.000  -0.5956   0.07916   0.07274  -0.0300   1.0000   0.0499
  -8.750  -0.6097   0.07370   0.06725  -0.0335   1.0000   0.0490
  -8.500  -0.6209   0.06847   0.06189  -0.0359   1.0000   0.0482
  -8.250  -0.6282   0.06360   0.05681  -0.0371   1.0000   0.0475
  -8.000  -0.6315   0.05900   0.05193  -0.0376   1.0000   0.0470
  -7.750  -0.6305   0.05474   0.04733  -0.0373   1.0000   0.0467
  -7.500  -0.6255   0.05084   0.04306  -0.0366   1.0000   0.0466
  -7.250  -0.6172   0.04729   0.03912  -0.0356   1.0000   0.0468
  -7.000  -0.6059   0.04417   0.03564  -0.0345   1.0000   0.0476
  -6.750  -0.5923   0.04161   0.03277  -0.0333   1.0000   0.0499
  -6.500  -0.5773   0.03907   0.02982  -0.0321   1.0000   0.0525
  -6.250  -0.5600   0.03651   0.02674  -0.0307   1.0000   0.0544
  -6.000  -0.5404   0.03407   0.02386  -0.0294   1.0000   0.0555
  -5.750  -0.5189   0.03195   0.02133  -0.0281   1.0000   0.0569
  -5.500  -0.4968   0.02988   0.01905  -0.0269   1.0000   0.0588
  -5.250  -0.4757   0.02827   0.01742  -0.0258   1.0000   0.0629
  -5.000  -0.4540   0.02703   0.01600  -0.0245   1.0000   0.0696
  -4.750  -0.4326   0.02567   0.01449  -0.0231   1.0000   0.0748
  -4.500  -0.4126   0.02445   0.01323  -0.0216   1.0000   0.0817
  -4.250  -0.3929   0.02334   0.01208  -0.0204   1.0000   0.0949
  -4.000  -0.3727   0.02215   0.01089  -0.0193   1.0000   0.1131
  -3.750  -0.3513   0.02056   0.00965  -0.0190   0.9987   0.1644
  -3.500  -0.3324   0.01811   0.00906  -0.0184   0.9919   0.4750
  -3.250  -0.3112   0.01786   0.00923  -0.0158   0.9844   0.6362
  -3.000  -0.2922   0.01795   0.00950  -0.0120   0.9757   0.7345
  -2.750  -0.2729   0.01806   0.00965  -0.0078   0.9684   0.8065
  -2.500  -0.2447   0.01802   0.00948  -0.0063   0.9620   0.8470
  -2.250  -0.2091   0.01791   0.00909  -0.0074   0.9566   0.8744
  -2.000  -0.1705   0.01777   0.00874  -0.0094   0.9504   0.8960
  -1.750  -0.1271   0.01764   0.00839  -0.0126   0.9451   0.9167
  -1.500  -0.0812   0.01752   0.00803  -0.0166   0.9399   0.9366
  -1.250  -0.0356   0.01738   0.00772  -0.0206   0.9330   0.9562
  -1.000   0.0152   0.01723   0.00742  -0.0259   0.9269   0.9735
  -0.750   0.0642   0.01706   0.00712  -0.0310   0.9186   0.9920
  -0.500   0.1002   0.01690   0.00688  -0.0336   0.9062   1.0000
  -0.250   0.1252   0.01680   0.00670  -0.0340   0.8905   1.0000
   0.000   0.1504   0.01674   0.00657  -0.0343   0.8751   1.0000
   0.250   0.1758   0.01672   0.00650  -0.0345   0.8601   1.0000
   0.500   0.2008   0.01674   0.00647  -0.0345   0.8447   1.0000
   0.750   0.2263   0.01680   0.00648  -0.0345   0.8294   1.0000
   1.000   0.2526   0.01687   0.00653  -0.0345   0.8140   1.0000
   1.250   0.2796   0.01695   0.00660  -0.0346   0.7979   1.0000
   1.500   0.3071   0.01703   0.00666  -0.0346   0.7811   1.0000
   1.750   0.3345   0.01713   0.00674  -0.0345   0.7649   1.0000
   2.000   0.3616   0.01726   0.00688  -0.0344   0.7498   1.0000
   2.250   0.3885   0.01742   0.00710  -0.0343   0.7367   1.0000
   2.500   0.4155   0.01761   0.00733  -0.0342   0.7243   1.0000
   2.750   0.4426   0.01780   0.00757  -0.0340   0.7117   1.0000
   3.000   0.4687   0.01804   0.00789  -0.0337   0.6985   1.0000
   3.250   0.4945   0.01830   0.00829  -0.0333   0.6843   1.0000
   3.500   0.5203   0.01855   0.00863  -0.0327   0.6684   1.0000
   3.750   0.5464   0.01878   0.00893  -0.0320   0.6515   1.0000
   4.000   0.5734   0.01904   0.00921  -0.0313   0.6338   1.0000
   4.250   0.5989   0.01942   0.00967  -0.0303   0.6094   1.0000
   4.500   0.6177   0.01975   0.01015  -0.0284   0.5691   1.0000
   4.750   0.6621   0.02367   0.01255  -0.0298   0.5109   1.0000
   5.000   0.6597   0.02150   0.01193  -0.0252   0.4643   1.0000
   5.250   0.6796   0.02190   0.01229  -0.0233   0.3904   1.0000
   5.500   0.6903   0.02311   0.01257  -0.0206   0.2198   1.0000
   5.750   0.7016   0.02535   0.01392  -0.0189   0.1295   1.0000
   6.000   0.7173   0.02704   0.01546  -0.0173   0.1026   1.0000
   6.250   0.7338   0.02858   0.01692  -0.0159   0.0859   1.0000
   6.500   0.7517   0.03005   0.01851  -0.0144   0.0762   1.0000
   6.750   0.7685   0.03175   0.02015  -0.0129   0.0693   1.0000
   7.000   0.7900   0.03317   0.02184  -0.0117   0.0623   1.0000
   7.250   0.8112   0.03486   0.02364  -0.0107   0.0575   1.0000
   7.500   0.8353   0.03722   0.02600  -0.0101   0.0548   1.0000
   7.750   0.8597   0.03956   0.02875  -0.0092   0.0530   1.0000
   8.000   0.8810   0.04215   0.03179  -0.0082   0.0509   1.0000
   8.250   0.8983   0.04474   0.03478  -0.0070   0.0481   1.0000
   8.500   0.9132   0.04729   0.03764  -0.0059   0.0455   1.0000
   8.750   0.9256   0.05023   0.04089  -0.0047   0.0441   1.0000
   9.000   0.9347   0.05362   0.04469  -0.0033   0.0434   1.0000
   9.250   0.9400   0.05725   0.04867  -0.0019   0.0429   1.0000
   9.500   0.9412   0.06107   0.05283  -0.0005   0.0426   1.0000
   9.750   0.9378   0.06503   0.05712   0.0008   0.0425   1.0000
  10.000   0.9294   0.06908   0.06147   0.0019   0.0425   1.0000
  10.250   0.9146   0.07309   0.06574   0.0030   0.0427   1.0000
  10.500   0.8945   0.07763   0.07050   0.0028   0.0430   1.0000
  10.750   0.8664   0.08385   0.07694  -0.0003   0.0436   1.0000
  11.000   0.8314   0.09351   0.08668  -0.0082   0.0448   1.0000
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