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AH 94-156 (ah94156-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: AH 94-156 (ah94156-il)
Reynolds number: 200,000
Max Cl/Cd: 64.37 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ah94156-il-200000-n5.txt
Download as CSV file: xf-ah94156-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AH 94-156                                       
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.2350   0.09088   0.08655  -0.0884   0.8210   0.0173
 -11.000  -0.2451   0.08450   0.08022  -0.0915   0.8182   0.0176
 -10.750  -0.2532   0.07879   0.07454  -0.0946   0.8154   0.0175
 -10.500  -0.2641   0.07242   0.06819  -0.0984   0.8124   0.0171
 -10.250  -0.3045   0.05999   0.05568  -0.1071   0.8092   0.0169
 -10.000  -0.3333   0.05437   0.04987  -0.1083   0.8060   0.0166
  -9.750  -0.3593   0.04997   0.04531  -0.1071   0.8018   0.0164
  -9.500  -0.3828   0.04638   0.04150  -0.1040   0.7978   0.0164
  -9.250  -0.4006   0.04338   0.03824  -0.1002   0.7948   0.0163
  -9.000  -0.4102   0.04021   0.03472  -0.0971   0.7923   0.0165
  -8.750  -0.4151   0.03693   0.03105  -0.0940   0.7896   0.0167
  -8.500  -0.4128   0.03407   0.02780  -0.0915   0.7864   0.0168
  -8.250  -0.4052   0.03150   0.02481  -0.0893   0.7835   0.0171
  -8.000  -0.3927   0.02925   0.02216  -0.0875   0.7811   0.0174
  -7.750  -0.3762   0.02735   0.01983  -0.0861   0.7790   0.0179
  -7.500  -0.3564   0.02581   0.01793  -0.0851   0.7772   0.0183
  -7.250  -0.3352   0.02462   0.01662  -0.0845   0.7755   0.0191
  -7.000  -0.3134   0.02397   0.01594  -0.0840   0.7727   0.0200
  -6.750  -0.2906   0.02319   0.01503  -0.0835   0.7700   0.0211
  -6.500  -0.2668   0.02224   0.01392  -0.0830   0.7677   0.0220
  -6.250  -0.2426   0.02134   0.01286  -0.0826   0.7657   0.0228
  -6.000  -0.2190   0.02046   0.01188  -0.0821   0.7639   0.0237
  -5.750  -0.1960   0.01974   0.01115  -0.0815   0.7621   0.0248
  -5.500  -0.1723   0.01921   0.01054  -0.0810   0.7605   0.0264
  -5.250  -0.1493   0.01880   0.01009  -0.0805   0.7576   0.0286
  -5.000  -0.1274   0.01825   0.00953  -0.0798   0.7550   0.0307
  -4.750  -0.1047   0.01781   0.00908  -0.0792   0.7526   0.0330
  -4.500  -0.0813   0.01743   0.00862  -0.0786   0.7505   0.0361
  -4.250  -0.0580   0.01700   0.00817  -0.0780   0.7484   0.0411
  -4.000  -0.0338   0.01664   0.00774  -0.0775   0.7466   0.0475
  -3.750  -0.0097   0.01628   0.00738  -0.0771   0.7450   0.0582
  -3.500   0.0121   0.01596   0.00720  -0.0764   0.7419   0.0797
  -3.250   0.0336   0.01555   0.00701  -0.0757   0.7390   0.1271
  -3.000   0.0538   0.01498   0.00681  -0.0748   0.7365   0.2144
  -2.750   0.0720   0.01426   0.00660  -0.0737   0.7342   0.3442
  -2.500   0.0875   0.01339   0.00639  -0.0718   0.7322   0.5119
  -2.250   0.1037   0.01302   0.00685  -0.0685   0.7306   0.6970
  -2.000   0.1273   0.01390   0.00793  -0.0658   0.7280   0.7785
  -1.750   0.1466   0.01421   0.00816  -0.0643   0.7246   0.8153
  -1.500   0.1694   0.01457   0.00845  -0.0629   0.7217   0.8338
  -1.250   0.1933   0.01482   0.00861  -0.0617   0.7193   0.8473
  -1.000   0.2174   0.01502   0.00871  -0.0605   0.7173   0.8600
  -0.750   0.2432   0.01519   0.00879  -0.0595   0.7155   0.8709
  -0.500   0.2656   0.01540   0.00900  -0.0582   0.7120   0.8790
  -0.250   0.2853   0.01551   0.00906  -0.0566   0.7082   0.8880
   0.000   0.3129   0.01552   0.00902  -0.0564   0.7053   0.8929
   0.250   0.3385   0.01546   0.00889  -0.0559   0.7028   0.8987
   0.500   0.3657   0.01535   0.00869  -0.0558   0.7007   0.9031
   0.750   0.3885   0.01542   0.00876  -0.0550   0.6963   0.9068
   1.000   0.4108   0.01541   0.00874  -0.0542   0.6922   0.9110
   1.250   0.4327   0.01533   0.00861  -0.0533   0.6891   0.9151
   1.500   0.4624   0.01519   0.00841  -0.0537   0.6866   0.9170
   1.750   0.4876   0.01517   0.00838  -0.0535   0.6830   0.9194
   2.000   0.5084   0.01521   0.00844  -0.0525   0.6781   0.9224
   2.250   0.5330   0.01513   0.00834  -0.0521   0.6746   0.9248
   2.500   0.5599   0.01499   0.00816  -0.0521   0.6717   0.9270
   2.750   0.5795   0.01501   0.00820  -0.0509   0.6671   0.9295
   3.000   0.6022   0.01501   0.00823  -0.0502   0.6621   0.9313
   3.250   0.6299   0.01491   0.00812  -0.0504   0.6584   0.9326
   3.500   0.6592   0.01479   0.00797  -0.0509   0.6554   0.9340
   3.750   0.6748   0.01491   0.00818  -0.0491   0.6488   0.9363
   4.000   0.7000   0.01483   0.00811  -0.0488   0.6442   0.9380
   4.250   0.7264   0.01473   0.00801  -0.0488   0.6399   0.9395
   4.500   0.7420   0.01483   0.00816  -0.0469   0.6327   0.9414
   4.750   0.7689   0.01471   0.00806  -0.0470   0.6278   0.9426
   5.000   0.7887   0.01478   0.00819  -0.0459   0.6207   0.9443
   5.250   0.8136   0.01474   0.00817  -0.0456   0.6144   0.9454
   5.500   0.8348   0.01477   0.00827  -0.0448   0.6068   0.9467
   5.750   0.8590   0.01474   0.00825  -0.0444   0.5992   0.9479
   6.000   0.8776   0.01482   0.00839  -0.0431   0.5902   0.9500
   6.250   0.9035   0.01476   0.00834  -0.0430   0.5821   0.9511
   6.500   0.9184   0.01489   0.00852  -0.0411   0.5715   0.9530
   6.750   0.9362   0.01500   0.00866  -0.0397   0.5609   0.9546
   7.000   0.9564   0.01511   0.00878  -0.0387   0.5501   0.9561
   7.250   0.9787   0.01524   0.00893  -0.0382   0.5382   0.9578
   7.500   0.9977   0.01550   0.00921  -0.0372   0.5249   0.9599
   7.750   1.0167   0.01580   0.00952  -0.0363   0.5111   0.9617
   8.000   1.0354   0.01615   0.00988  -0.0355   0.4966   0.9637
   8.250   1.0536   0.01657   0.01031  -0.0347   0.4817   0.9659
   8.500   1.0716   0.01705   0.01080  -0.0339   0.4669   0.9683
   8.750   1.0889   0.01764   0.01137  -0.0333   0.4497   0.9711
   9.000   1.1046   0.01838   0.01209  -0.0326   0.4299   0.9750
   9.250   1.1180   0.01925   0.01293  -0.0318   0.4079   0.9812
   9.500   1.1265   0.02018   0.01379  -0.0301   0.3879   1.0000
   9.750   1.1335   0.02117   0.01475  -0.0282   0.3677   1.0000
  10.000   1.1398   0.02227   0.01580  -0.0264   0.3474   1.0000
  10.250   1.1450   0.02349   0.01695  -0.0245   0.3268   1.0000
  10.500   1.1500   0.02479   0.01820  -0.0227   0.3038   1.0000
  10.750   1.1527   0.02627   0.01961  -0.0209   0.2803   1.0000
  11.000   1.1550   0.02786   0.02111  -0.0191   0.2557   1.0000
  11.250   1.1566   0.02956   0.02271  -0.0175   0.2306   1.0000
  11.500   1.1579   0.03138   0.02442  -0.0159   0.2062   1.0000
  11.750   1.1578   0.03338   0.02630  -0.0144   0.1805   1.0000
  12.000   1.1581   0.03544   0.02824  -0.0130   0.1550   1.0000
  12.250   1.1583   0.03761   0.03029  -0.0118   0.1297   1.0000
  12.500   1.1586   0.03985   0.03242  -0.0106   0.1068   1.0000
  13.000   1.1602   0.04448   0.03691  -0.0088   0.0716   1.0000
  13.250   1.1624   0.04678   0.03917  -0.0082   0.0590   1.0000
  13.500   1.1647   0.04913   0.04152  -0.0076   0.0491   1.0000
  13.750   1.1673   0.05154   0.04394  -0.0072   0.0422   1.0000
  14.000   1.1699   0.05401   0.04644  -0.0068   0.0361   1.0000
  14.250   1.1728   0.05650   0.04900  -0.0066   0.0318   1.0000
  14.500   1.1736   0.05930   0.05184  -0.0064   0.0282   1.0000
  14.750   1.1760   0.06200   0.05464  -0.0064   0.0254   1.0000
  15.000   1.1778   0.06482   0.05755  -0.0065   0.0232   1.0000
  15.250   1.1760   0.06813   0.06091  -0.0066   0.0214   1.0000
  15.500   1.1775   0.07115   0.06407  -0.0069   0.0202   1.0000
  15.750   1.1783   0.07431   0.06735  -0.0073   0.0192   1.0000
  16.000   1.1778   0.07770   0.07083  -0.0079   0.0180   1.0000
  16.250   1.1748   0.08148   0.07469  -0.0086   0.0171   1.0000
  16.500   1.1742   0.08500   0.07832  -0.0094   0.0162   1.0000
  16.750   1.1726   0.08872   0.08217  -0.0103   0.0159   1.0000
  17.000   1.1727   0.09229   0.08586  -0.0112   0.0148   1.0000
  17.250   1.1720   0.09600   0.08968  -0.0124   0.0142   1.0000
  17.500   1.1708   0.09985   0.09364  -0.0136   0.0137   1.0000
  17.750   1.1678   0.10397   0.09785  -0.0150   0.0133   1.0000
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