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AH 83-159 (ah83159-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: AH 83-159 (ah83159-il)
Reynolds number: 1,000,000
Max Cl/Cd: 133.8 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ah83159-il-1000000-n5.txt
Download as CSV file: xf-ah83159-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AH 83-159                                       
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.5292   0.03966   0.03640  -0.1163   0.7343   0.0044
 -12.000  -0.5669   0.03461   0.03104  -0.1137   0.7311   0.0044
 -11.750  -0.5806   0.03192   0.02814  -0.1110   0.7281   0.0044
 -11.500  -0.5840   0.03010   0.02616  -0.1086   0.7255   0.0045
 -11.250  -0.5847   0.02852   0.02443  -0.1061   0.7227   0.0046
 -11.000  -0.5937   0.02642   0.02210  -0.1022   0.7199   0.0047
 -10.750  -0.5909   0.02537   0.02091  -0.0992   0.7172   0.0048
 -10.500  -0.5856   0.02386   0.01919  -0.0967   0.7149   0.0048
 -10.000  -0.5611   0.02146   0.01645  -0.0934   0.7107   0.0050
  -9.750  -0.5456   0.02035   0.01518  -0.0921   0.7085   0.0051
  -9.500  -0.5275   0.01949   0.01418  -0.0911   0.7062   0.0051
  -9.250  -0.5088   0.01860   0.01315  -0.0901   0.7038   0.0052
  -9.000  -0.4890   0.01779   0.01220  -0.0892   0.7015   0.0053
  -8.750  -0.4683   0.01706   0.01135  -0.0885   0.6995   0.0053
  -8.500  -0.4467   0.01640   0.01057  -0.0878   0.6976   0.0054
  -8.250  -0.4239   0.01584   0.00993  -0.0874   0.6959   0.0054
  -8.000  -0.4014   0.01520   0.00920  -0.0868   0.6940   0.0055
  -7.750  -0.3777   0.01473   0.00866  -0.0865   0.6919   0.0055
  -7.500  -0.3542   0.01422   0.00807  -0.0861   0.6898   0.0056
  -7.250  -0.3322   0.01351   0.00726  -0.0854   0.6877   0.0057
  -7.000  -0.3095   0.01293   0.00660  -0.0848   0.6857   0.0059
  -6.500  -0.2600   0.01218   0.00577  -0.0843   0.6823   0.0064
  -6.250  -0.2347   0.01184   0.00540  -0.0842   0.6806   0.0066
  -6.000  -0.2092   0.01152   0.00504  -0.0841   0.6786   0.0068
  -5.750  -0.1835   0.01121   0.00470  -0.0839   0.6766   0.0070
  -5.500  -0.1576   0.01094   0.00439  -0.0839   0.6746   0.0074
  -5.250  -0.1314   0.01069   0.00410  -0.0838   0.6727   0.0077
  -5.000  -0.1050   0.01048   0.00383  -0.0838   0.6710   0.0080
  -4.750  -0.0788   0.01024   0.00355  -0.0837   0.6692   0.0087
  -4.500  -0.0519   0.01001   0.00334  -0.0838   0.6676   0.0097
  -4.250  -0.0246   0.00983   0.00315  -0.0840   0.6657   0.0110
  -4.000   0.0026   0.00964   0.00296  -0.0841   0.6638   0.0130
  -3.750   0.0300   0.00949   0.00280  -0.0843   0.6620   0.0158
  -3.500   0.0573   0.00933   0.00266  -0.0845   0.6601   0.0204
  -3.250   0.0846   0.00917   0.00252  -0.0847   0.6581   0.0273
  -3.000   0.1119   0.00903   0.00239  -0.0848   0.6563   0.0371
  -2.750   0.1392   0.00885   0.00228  -0.0850   0.6546   0.0551
  -2.500   0.1662   0.00858   0.00216  -0.0853   0.6529   0.0953
  -2.250   0.1928   0.00824   0.00204  -0.0855   0.6510   0.1608
  -2.000   0.2191   0.00787   0.00193  -0.0857   0.6490   0.2416
  -1.750   0.2451   0.00742   0.00181  -0.0860   0.6470   0.3462
  -1.500   0.2708   0.00689   0.00168  -0.0862   0.6450   0.4747
  -1.250   0.2949   0.00613   0.00153  -0.0862   0.6431   0.6617
  -1.000   0.3212   0.00602   0.00165  -0.0860   0.6412   0.7427
  -0.750   0.3496   0.00610   0.00178  -0.0862   0.6394   0.7678
  -0.500   0.3786   0.00618   0.00187  -0.0865   0.6375   0.7804
  -0.250   0.4080   0.00625   0.00190  -0.0870   0.6354   0.7888
   0.000   0.4367   0.00635   0.00200  -0.0873   0.6333   0.7936
   0.250   0.4655   0.00645   0.00208  -0.0876   0.6311   0.7987
   0.500   0.4945   0.00654   0.00212  -0.0881   0.6288   0.8034
   0.750   0.5229   0.00662   0.00217  -0.0884   0.6267   0.8056
   1.000   0.5519   0.00666   0.00223  -0.0888   0.6245   0.8071
   1.250   0.5808   0.00670   0.00227  -0.0893   0.6219   0.8084
   1.500   0.6095   0.00674   0.00231  -0.0897   0.6190   0.8098
   1.750   0.6381   0.00679   0.00234  -0.0901   0.6158   0.8111
   2.000   0.6664   0.00685   0.00237  -0.0904   0.6128   0.8124
   2.250   0.6952   0.00688   0.00241  -0.0909   0.6094   0.8136
   2.500   0.7238   0.00692   0.00245  -0.0914   0.6050   0.8148
   2.750   0.7520   0.00698   0.00249  -0.0917   0.6004   0.8161
   3.000   0.7803   0.00703   0.00253  -0.0921   0.5968   0.8172
   3.250   0.8090   0.00707   0.00258  -0.0926   0.5930   0.8181
   3.500   0.8371   0.00712   0.00264  -0.0930   0.5886   0.8189
   3.750   0.8645   0.00719   0.00270  -0.0932   0.5843   0.8197
   4.000   0.8925   0.00724   0.00278  -0.0935   0.5797   0.8205
   4.250   0.9200   0.00731   0.00287  -0.0937   0.5742   0.8212
   4.500   0.9469   0.00740   0.00296  -0.0939   0.5690   0.8220
   4.750   0.9745   0.00747   0.00305  -0.0942   0.5628   0.8227
   5.000   1.0006   0.00759   0.00316  -0.0942   0.5547   0.8235
   5.250   1.0267   0.00770   0.00329  -0.0942   0.5445   0.8244
   5.500   1.0517   0.00786   0.00343  -0.0940   0.5320   0.8254
   5.750   1.0748   0.00809   0.00360  -0.0934   0.5148   0.8264
   6.000   1.0961   0.00838   0.00383  -0.0926   0.4936   0.8273
   6.250   1.1147   0.00877   0.00411  -0.0913   0.4682   0.8283
   6.500   1.1306   0.00923   0.00445  -0.0895   0.4397   0.8294
   6.750   1.1422   0.00980   0.00488  -0.0869   0.4065   0.8307
   7.000   1.1469   0.01046   0.00537  -0.0831   0.3716   0.8320
   7.250   1.1436   0.01116   0.00592  -0.0778   0.3401   0.8332
   7.500   1.1377   0.01209   0.00672  -0.0724   0.3092   0.8345
   7.750   1.1359   0.01307   0.00759  -0.0682   0.2819   0.8357
   8.000   1.1384   0.01403   0.00846  -0.0649   0.2584   0.8370
   8.250   1.1394   0.01513   0.00946  -0.0615   0.2330   0.8382
   8.500   1.1419   0.01625   0.01048  -0.0585   0.2098   0.8393
   8.750   1.1394   0.01769   0.01175  -0.0551   0.1776   0.8404
   9.000   1.1380   0.01915   0.01306  -0.0519   0.1476   0.8414
   9.250   1.1405   0.02047   0.01427  -0.0494   0.1249   0.8425
   9.500   1.1411   0.02195   0.01562  -0.0468   0.0991   0.8436
   9.750   1.1438   0.02338   0.01694  -0.0445   0.0775   0.8445
  10.000   1.1466   0.02485   0.01829  -0.0424   0.0568   0.8452
  10.250   1.1542   0.02607   0.01946  -0.0408   0.0450   0.8458
  10.500   1.1628   0.02727   0.02062  -0.0395   0.0361   0.8463
  10.750   1.1722   0.02846   0.02179  -0.0382   0.0287   0.8468
  11.000   1.1821   0.02964   0.02296  -0.0371   0.0236   0.8474
  11.250   1.1928   0.03078   0.02412  -0.0360   0.0197   0.8481
  11.500   1.2035   0.03195   0.02531  -0.0351   0.0168   0.8489
  11.750   1.2129   0.03325   0.02661  -0.0340   0.0130   0.8496
  12.000   1.2234   0.03450   0.02789  -0.0332   0.0106   0.8501
  12.250   1.2339   0.03579   0.02919  -0.0324   0.0089   0.8506
  12.500   1.2425   0.03725   0.03067  -0.0315   0.0065   0.8512
  12.750   1.2530   0.03860   0.03206  -0.0308   0.0055   0.8517
  13.000   1.2621   0.04008   0.03357  -0.0300   0.0045   0.8522
  13.250   1.2717   0.04156   0.03510  -0.0294   0.0040   0.8527
  13.500   1.2818   0.04302   0.03661  -0.0288   0.0037   0.8532
  13.750   1.2908   0.04462   0.03826  -0.0283   0.0034   0.8537
  14.000   1.2984   0.04636   0.04005  -0.0277   0.0029   0.8542
  14.250   1.3056   0.04819   0.04194  -0.0271   0.0027   0.8547
  14.500   1.3147   0.04987   0.04367  -0.0268   0.0026   0.8552
  14.750   1.3229   0.05167   0.04554  -0.0264   0.0026   0.8558
  15.000   1.3309   0.05353   0.04746  -0.0261   0.0025   0.8565
  15.250   1.3375   0.05556   0.04956  -0.0259   0.0024   0.8570
  15.500   1.3451   0.05752   0.05158  -0.0257   0.0023   0.8575
  15.750   1.3502   0.05980   0.05395  -0.0255   0.0023   0.8579
  16.000   1.3566   0.06198   0.05620  -0.0255   0.0022   0.8583
  16.250   1.3613   0.06439   0.05869  -0.0255   0.0021   0.8587
  16.500   1.3663   0.06682   0.06119  -0.0256   0.0021   0.8590
  16.750   1.3702   0.06943   0.06388  -0.0258   0.0020   0.8594
  17.000   1.3738   0.07210   0.06662  -0.0260   0.0020   0.8597
  17.250   1.3767   0.07494   0.06954  -0.0264   0.0020   0.8600
  17.500   1.3785   0.07797   0.07266  -0.0268   0.0019   0.8603
  17.750   1.3774   0.08148   0.07626  -0.0274   0.0018   0.8606
  18.250   1.3777   0.08828   0.08324  -0.0289   0.0017   0.8612
  18.500   1.3775   0.09182   0.08689  -0.0299   0.0017   0.8616
  18.750   1.3748   0.09583   0.09100  -0.0310   0.0017   0.8619
  19.000   1.3691   0.10037   0.09565  -0.0324   0.0017   0.8622
  19.250   1.3656   0.10461   0.10000  -0.0339   0.0016   0.8626
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