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AH 82-150 A (ah82150a-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: AH 82-150 A (ah82150a-il)
Reynolds number: 1,000,000
Max Cl/Cd: 137.58 at α=5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-ah82150a-il-1000000.txt
Download as CSV file: xf-ah82150a-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AH 82-150 A                                     
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.6101   0.05210   0.05007  -0.1073   0.9391   0.0082
 -13.500  -0.6140   0.04156   0.03906  -0.1232   0.9177   0.0085
 -13.250  -0.6262   0.03635   0.03344  -0.1272   0.8874   0.0083
 -13.000  -0.6337   0.03368   0.03051  -0.1268   0.8686   0.0086
 -12.750  -0.6446   0.03102   0.02759  -0.1254   0.8548   0.0086
 -12.500  -0.6493   0.02897   0.02533  -0.1236   0.8443   0.0087
 -12.250  -0.6505   0.02724   0.02340  -0.1218   0.8359   0.0088
 -12.000  -0.6446   0.02614   0.02215  -0.1201   0.8287   0.0090
 -11.750  -0.6476   0.02425   0.02004  -0.1175   0.8219   0.0090
 -11.500  -0.6310   0.02410   0.01982  -0.1164   0.8163   0.0093
 -11.250  -0.6204   0.02353   0.01914  -0.1146   0.8111   0.0093
 -11.000  -0.6352   0.02064   0.01589  -0.1097   0.8056   0.0097
 -10.750  -0.6249   0.01945   0.01454  -0.1078   0.8012   0.0101
 -10.500  -0.6091   0.01871   0.01368  -0.1066   0.7971   0.0103
 -10.250  -0.5898   0.01825   0.01318  -0.1057   0.7935   0.0107
 -10.000  -0.5702   0.01771   0.01258  -0.1049   0.7898   0.0110
  -9.750  -0.5506   0.01709   0.01185  -0.1040   0.7863   0.0114
  -9.500  -0.5303   0.01650   0.01115  -0.1033   0.7830   0.0118
  -9.250  -0.5090   0.01593   0.01049  -0.1026   0.7801   0.0122
  -9.000  -0.4868   0.01545   0.00993  -0.1021   0.7771   0.0126
  -8.750  -0.4635   0.01508   0.00949  -0.1016   0.7740   0.0129
  -8.500  -0.4462   0.01399   0.00826  -0.1004   0.7709   0.0139
  -8.250  -0.4228   0.01362   0.00785  -0.1000   0.7678   0.0148
  -8.000  -0.3980   0.01336   0.00759  -0.0998   0.7654   0.0156
  -7.750  -0.3728   0.01313   0.00731  -0.0997   0.7627   0.0166
  -7.500  -0.3467   0.01298   0.00713  -0.0996   0.7600   0.0175
  -7.250  -0.3254   0.01229   0.00635  -0.0989   0.7573   0.0188
  -7.000  -0.3006   0.01199   0.00603  -0.0987   0.7545   0.0202
  -6.750  -0.2747   0.01178   0.00581  -0.0986   0.7522   0.0216
  -6.500  -0.2486   0.01158   0.00559  -0.0986   0.7497   0.0229
  -6.250  -0.2219   0.01144   0.00541  -0.0986   0.7472   0.0238
  -6.000  -0.1990   0.01085   0.00476  -0.0981   0.7446   0.0262
  -5.750  -0.1727   0.01066   0.00457  -0.0982   0.7422   0.0282
  -5.500  -0.1459   0.01051   0.00438  -0.0982   0.7397   0.0301
  -5.250  -0.1188   0.01037   0.00423  -0.0983   0.7375   0.0316
  -5.000  -0.0930   0.01006   0.00388  -0.0983   0.7351   0.0335
  -4.750  -0.0670   0.00974   0.00354  -0.0982   0.7327   0.0368
  -4.500  -0.0400   0.00955   0.00334  -0.0983   0.7304   0.0396
  -4.250  -0.0125   0.00943   0.00318  -0.0985   0.7281   0.0419
  -4.000   0.0145   0.00922   0.00293  -0.0986   0.7257   0.0466
  -3.750   0.0419   0.00904   0.00277  -0.0988   0.7235   0.0529
  -3.500   0.0691   0.00882   0.00260  -0.0990   0.7213   0.0655
  -3.250   0.0959   0.00851   0.00243  -0.0992   0.7189   0.1024
  -3.000   0.1221   0.00806   0.00226  -0.0994   0.7165   0.1819
  -2.750   0.1484   0.00755   0.00209  -0.0998   0.7142   0.2855
  -2.500   0.1739   0.00664   0.00181  -0.1005   0.7118   0.4851
  -2.250   0.2009   0.00611   0.00182  -0.1009   0.7095   0.6601
  -2.000   0.2300   0.00613   0.00184  -0.1012   0.7072   0.6829
  -1.750   0.2590   0.00617   0.00188  -0.1016   0.7047   0.6953
  -1.500   0.2880   0.00623   0.00192  -0.1019   0.7021   0.7054
  -1.250   0.3172   0.00630   0.00193  -0.1023   0.6996   0.7124
  -1.000   0.3458   0.00648   0.00210  -0.1024   0.6967   0.7261
  -0.750   0.3736   0.00663   0.00229  -0.1023   0.6939   0.7372
  -0.500   0.4024   0.00671   0.00235  -0.1026   0.6905   0.7431
  -0.250   0.4304   0.00674   0.00240  -0.1026   0.6871   0.7474
   0.000   0.4587   0.00684   0.00248  -0.1028   0.6839   0.7521
   0.250   0.4876   0.00691   0.00251  -0.1032   0.6808   0.7550
   0.500   0.5166   0.00691   0.00251  -0.1036   0.6779   0.7561
   0.750   0.5456   0.00691   0.00250  -0.1041   0.6748   0.7570
   1.000   0.5744   0.00689   0.00246  -0.1045   0.6716   0.7580
   1.250   0.6031   0.00690   0.00244  -0.1049   0.6684   0.7589
   1.500   0.6317   0.00690   0.00245  -0.1053   0.6652   0.7597
   1.750   0.6602   0.00689   0.00246  -0.1056   0.6616   0.7606
   2.000   0.6887   0.00689   0.00247  -0.1060   0.6580   0.7615
   2.250   0.7171   0.00693   0.00250  -0.1063   0.6543   0.7626
   2.500   0.7455   0.00695   0.00253  -0.1066   0.6507   0.7635
   2.750   0.7740   0.00696   0.00256  -0.1070   0.6465   0.7644
   3.000   0.8022   0.00698   0.00260  -0.1073   0.6424   0.7653
   3.250   0.8303   0.00704   0.00264  -0.1076   0.6382   0.7663
   3.500   0.8585   0.00704   0.00269  -0.1079   0.6335   0.7673
   3.750   0.8864   0.00708   0.00273  -0.1081   0.6282   0.7682
   4.000   0.9141   0.00714   0.00280  -0.1083   0.6228   0.7693
   4.250   0.9419   0.00717   0.00287  -0.1086   0.6163   0.7704
   4.500   0.9688   0.00724   0.00293  -0.1086   0.6080   0.7713
   4.750   0.9946   0.00732   0.00298  -0.1084   0.5942   0.7721
   5.000   1.0195   0.00741   0.00306  -0.1081   0.5755   0.7733
   5.250   1.0421   0.00761   0.00318  -0.1073   0.5498   0.7744
   5.500   1.0619   0.00795   0.00339  -0.1060   0.5140   0.7755
   5.750   1.0766   0.00852   0.00373  -0.1038   0.4629   0.7767
   6.000   1.0905   0.00914   0.00413  -0.1015   0.4157   0.7780
   6.250   1.1047   0.00972   0.00453  -0.0993   0.3758   0.7793
   6.500   1.1139   0.01045   0.00502  -0.0962   0.3261   0.7809
   6.750   1.1126   0.01138   0.00562  -0.0912   0.2657   0.7828
   7.000   1.1018   0.01260   0.00645  -0.0846   0.1964   0.7847
   7.250   1.0883   0.01410   0.00756  -0.0780   0.1260   0.7863
   7.500   1.0767   0.01569   0.00882  -0.0723   0.0628   0.7885
   7.750   1.0714   0.01721   0.01011  -0.0679   0.0194   0.7903
   8.000   1.0829   0.01800   0.01092  -0.0660   0.0144   0.7920
   8.250   1.0936   0.01887   0.01185  -0.0640   0.0122   0.7937
   8.500   1.1084   0.01955   0.01257  -0.0626   0.0117   0.7954
   8.750   1.1220   0.02031   0.01338  -0.0612   0.0111   0.7972
   9.000   1.1356   0.02109   0.01420  -0.0599   0.0104   0.7989
   9.250   1.1478   0.02200   0.01514  -0.0584   0.0098   0.8005
   9.500   1.1573   0.02307   0.01627  -0.0567   0.0092   0.8027
   9.750   1.1613   0.02455   0.01787  -0.0544   0.0087   0.8049
  10.000   1.1716   0.02565   0.01904  -0.0529   0.0084   0.8072
  10.250   1.1835   0.02667   0.02012  -0.0516   0.0081   0.8094
  10.500   1.1937   0.02783   0.02134  -0.0503   0.0079   0.8117
  10.750   1.2022   0.02916   0.02273  -0.0489   0.0076   0.8139
  11.000   1.2105   0.03054   0.02418  -0.0475   0.0075   0.8162
  11.250   1.2197   0.03184   0.02555  -0.0463   0.0072   0.8188
  11.500   1.2268   0.03336   0.02715  -0.0450   0.0070   0.8215
  11.750   1.2336   0.03496   0.02884  -0.0438   0.0069   0.8244
  12.000   1.2407   0.03660   0.03053  -0.0427   0.0066   0.8274
  12.250   1.2458   0.03845   0.03244  -0.0415   0.0064   0.8303
  12.500   1.2467   0.04072   0.03480  -0.0402   0.0062   0.8337
  12.750   1.2372   0.04410   0.03831  -0.0382   0.0059   0.8369
  13.000   1.2461   0.04580   0.04009  -0.0376   0.0058   0.8409
  13.250   1.2553   0.04751   0.04189  -0.0370   0.0057   0.8452
  13.500   1.2640   0.04927   0.04375  -0.0365   0.0056   0.8506
  13.750   1.2714   0.05122   0.04580  -0.0360   0.0054   0.8566
  14.000   1.2769   0.05340   0.04809  -0.0353   0.0054   0.8633
  14.250   1.2835   0.05551   0.05032  -0.0348   0.0053   0.8723
  14.500   1.2892   0.05766   0.05263  -0.0343   0.0052   0.8862
  14.750   1.2926   0.05968   0.05492  -0.0332   0.0051   0.9603
  15.000   1.2981   0.06207   0.05740  -0.0331   0.0050   1.0000
  15.250   1.3036   0.06457   0.05999  -0.0331   0.0049   1.0000
  15.500   1.3076   0.06736   0.06288  -0.0330   0.0049   1.0000
  15.750   1.3112   0.07021   0.06585  -0.0330   0.0048   1.0000
  16.000   1.3139   0.07321   0.06894  -0.0334   0.0047   1.0000
  16.250   1.3153   0.07648   0.07232  -0.0337   0.0046   1.0000
  16.500   1.3151   0.08005   0.07603  -0.0342   0.0046   1.0000
  16.750   1.3147   0.08367   0.07975  -0.0350   0.0045   1.0000
  17.000   1.3126   0.08767   0.08388  -0.0359   0.0045   1.0000
  17.250   1.3096   0.09184   0.08818  -0.0370   0.0045   1.0000
  17.500   1.3069   0.09604   0.09249  -0.0385   0.0044   1.0000
  17.750   1.2995   0.10116   0.09777  -0.0401   0.0044   1.0000
  18.000   1.2905   0.10668   0.10346  -0.0421   0.0044   1.0000
  18.250   1.2859   0.11149   0.10836  -0.0444   0.0043   1.0000
  18.500   1.2779   0.11703   0.11403  -0.0469   0.0043   1.0000
  18.750   1.2667   0.12328   0.12044  -0.0499   0.0043   1.0000
  19.000   1.2573   0.12934   0.12663  -0.0531   0.0042   1.0000
  19.250   1.2467   0.13577   0.13319  -0.0567   0.0042   1.0000
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