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AH 83-159 (ah83159-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: AH 83-159 (ah83159-il)
Reynolds number: 500,000
Max Cl/Cd: 105.52 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ah83159-il-500000-n5.txt
Download as CSV file: xf-ah83159-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.2115   0.08648   0.08301  -0.0949   0.7500   0.0072
 -11.000  -0.2202   0.08067   0.07722  -0.0976   0.7476   0.0071
 -10.750  -0.2350   0.07359   0.07017  -0.1013   0.7453   0.0071
 -10.500  -0.2653   0.06202   0.05861  -0.1099   0.7429   0.0069
 -10.250  -0.3063   0.05302   0.04949  -0.1139   0.7403   0.0068
 -10.000  -0.3466   0.04643   0.04272  -0.1127   0.7373   0.0066
  -9.750  -0.3932   0.03986   0.03586  -0.1080   0.7342   0.0066
  -9.500  -0.4244   0.03506   0.03071  -0.1025   0.7314   0.0067
  -9.250  -0.4412   0.03042   0.02558  -0.0982   0.7290   0.0068
  -8.750  -0.4320   0.02499   0.01939  -0.0933   0.7247   0.0071
  -8.500  -0.4175   0.02321   0.01734  -0.0919   0.7222   0.0072
  -8.250  -0.3999   0.02176   0.01564  -0.0908   0.7197   0.0074
  -8.000  -0.3805   0.02047   0.01412  -0.0899   0.7175   0.0075
  -7.750  -0.3584   0.01968   0.01315  -0.0893   0.7155   0.0078
  -7.500  -0.3360   0.01887   0.01216  -0.0887   0.7137   0.0080
  -7.250  -0.3130   0.01813   0.01126  -0.0882   0.7120   0.0081
  -7.000  -0.2916   0.01695   0.00997  -0.0875   0.7099   0.0084
  -6.750  -0.2691   0.01616   0.00910  -0.0870   0.7077   0.0086
  -6.500  -0.2460   0.01553   0.00841  -0.0865   0.7054   0.0088
  -6.250  -0.2225   0.01499   0.00779  -0.0860   0.7033   0.0090
  -6.000  -0.1985   0.01451   0.00726  -0.0857   0.7014   0.0094
  -5.750  -0.1745   0.01406   0.00674  -0.0853   0.6997   0.0097
  -5.500  -0.1500   0.01367   0.00627  -0.0850   0.6981   0.0103
  -5.250  -0.1253   0.01328   0.00584  -0.0847   0.6961   0.0109
  -5.000  -0.1001   0.01295   0.00546  -0.0845   0.6940   0.0114
  -4.750  -0.0754   0.01254   0.00503  -0.0842   0.6918   0.0125
  -4.500  -0.0496   0.01227   0.00474  -0.0841   0.6898   0.0139
  -4.250  -0.0235   0.01203   0.00446  -0.0841   0.6880   0.0160
  -4.000   0.0025   0.01178   0.00420  -0.0840   0.6862   0.0198
  -3.750   0.0288   0.01155   0.00396  -0.0840   0.6845   0.0252
  -3.500   0.0553   0.01134   0.00375  -0.0840   0.6826   0.0323
  -3.250   0.0817   0.01112   0.00358  -0.0841   0.6806   0.0450
  -3.000   0.1078   0.01083   0.00341  -0.0842   0.6786   0.0752
  -2.750   0.1329   0.01043   0.00325  -0.0842   0.6766   0.1362
  -2.500   0.1574   0.00992   0.00307  -0.0842   0.6746   0.2344
  -2.250   0.1810   0.00926   0.00287  -0.0842   0.6726   0.3732
  -2.000   0.2038   0.00842   0.00264  -0.0841   0.6709   0.5512
  -1.750   0.2260   0.00798   0.00278  -0.0831   0.6693   0.7068
  -1.500   0.2518   0.00820   0.00313  -0.0824   0.6672   0.7571
  -1.250   0.2797   0.00843   0.00334  -0.0824   0.6651   0.7789
  -1.000   0.3077   0.00866   0.00354  -0.0824   0.6630   0.7924
  -0.750   0.3356   0.00886   0.00371  -0.0823   0.6609   0.8006
  -0.500   0.3636   0.00902   0.00382  -0.0824   0.6589   0.8063
  -0.250   0.3911   0.00918   0.00394  -0.0823   0.6570   0.8101
   0.000   0.4196   0.00929   0.00399  -0.0826   0.6553   0.8143
   0.250   0.4490   0.00932   0.00399  -0.0833   0.6532   0.8184
   0.500   0.4767   0.00937   0.00404  -0.0834   0.6509   0.8197
   0.750   0.5047   0.00941   0.00408  -0.0836   0.6486   0.8209
   1.000   0.5327   0.00945   0.00411  -0.0839   0.6463   0.8223
   1.250   0.5609   0.00949   0.00412  -0.0842   0.6440   0.8237
   1.500   0.5894   0.00953   0.00413  -0.0846   0.6420   0.8253
   1.750   0.6178   0.00957   0.00416  -0.0850   0.6397   0.8268
   2.000   0.6460   0.00960   0.00420  -0.0854   0.6369   0.8285
   2.250   0.6745   0.00962   0.00423  -0.0859   0.6338   0.8303
   2.500   0.7032   0.00964   0.00423  -0.0864   0.6308   0.8318
   2.750   0.7318   0.00967   0.00424  -0.0869   0.6279   0.8332
   3.000   0.7592   0.00971   0.00429  -0.0871   0.6247   0.8340
   3.250   0.7863   0.00973   0.00436  -0.0872   0.6204   0.8349
   3.500   0.8135   0.00976   0.00441  -0.0874   0.6161   0.8357
   3.750   0.8410   0.00980   0.00443  -0.0876   0.6125   0.8366
   4.000   0.8680   0.00985   0.00454  -0.0878   0.6084   0.8377
   4.250   0.8950   0.00990   0.00462  -0.0879   0.6040   0.8389
   4.500   0.9221   0.00995   0.00470  -0.0881   0.6000   0.8400
   4.750   0.9491   0.01001   0.00479  -0.0883   0.5955   0.8411
   5.000   0.9758   0.01007   0.00489  -0.0885   0.5903   0.8422
   5.250   1.0024   0.01014   0.00499  -0.0886   0.5852   0.8433
   5.500   1.0288   0.01022   0.00511  -0.0887   0.5796   0.8447
   5.750   1.0546   0.01031   0.00522  -0.0887   0.5723   0.8459
   6.000   1.0799   0.01041   0.00535  -0.0887   0.5640   0.8469
   6.250   1.1032   0.01052   0.00548  -0.0881   0.5536   0.8477
   6.500   1.1248   0.01066   0.00564  -0.0873   0.5402   0.8485
   6.750   1.1444   0.01087   0.00583  -0.0861   0.5228   0.8494
   7.000   1.1606   0.01116   0.00608  -0.0843   0.5023   0.8506
   7.250   1.1724   0.01156   0.00642  -0.0817   0.4787   0.8520
   7.500   1.1753   0.01206   0.00682  -0.0775   0.4529   0.8535
   7.750   1.1694   0.01284   0.00747  -0.0720   0.4221   0.8554
   8.000   1.1616   0.01393   0.00843  -0.0668   0.3913   0.8574
   8.250   1.1550   0.01522   0.00956  -0.0622   0.3605   0.8595
   8.500   1.1510   0.01657   0.01078  -0.0583   0.3314   0.8609
   8.750   1.1497   0.01785   0.01196  -0.0550   0.3064   0.8620
   9.000   1.1499   0.01916   0.01318  -0.0520   0.2826   0.8631
   9.250   1.1515   0.02047   0.01442  -0.0493   0.2589   0.8642
   9.500   1.1533   0.02184   0.01571  -0.0468   0.2363   0.8656
   9.750   1.1510   0.02350   0.01723  -0.0440   0.2054   0.8669
  10.000   1.1524   0.02504   0.01865  -0.0417   0.1809   0.8679
  10.250   1.1513   0.02677   0.02024  -0.0393   0.1515   0.8689
  10.500   1.1498   0.02862   0.02192  -0.0371   0.1213   0.8699
  10.750   1.1490   0.03053   0.02366  -0.0350   0.0932   0.8707
  11.000   1.1508   0.03234   0.02534  -0.0334   0.0711   0.8716
  11.250   1.1557   0.03398   0.02691  -0.0320   0.0551   0.8724
  11.500   1.1626   0.03553   0.02842  -0.0309   0.0443   0.8733
  12.000   1.1769   0.03874   0.03159  -0.0290   0.0271   0.8747
  12.250   1.1858   0.04022   0.03309  -0.0282   0.0229   0.8753
  12.500   1.1934   0.04185   0.03473  -0.0275   0.0186   0.8759
  12.750   1.2030   0.04335   0.03629  -0.0269   0.0158   0.8765
  13.000   1.2102   0.04510   0.03806  -0.0262   0.0130   0.8771
  13.250   1.2189   0.04676   0.03977  -0.0257   0.0107   0.8777
  13.500   1.2258   0.04862   0.04167  -0.0251   0.0088   0.8783
  13.750   1.2339   0.05040   0.04354  -0.0247   0.0078   0.8789
  14.000   1.2393   0.05251   0.04568  -0.0242   0.0065   0.8795
  14.250   1.2464   0.05448   0.04774  -0.0239   0.0059   0.8801
  14.500   1.2532   0.05653   0.04988  -0.0237   0.0055   0.8807
  14.750   1.2594   0.05868   0.05211  -0.0234   0.0052   0.8815
  15.000   1.2649   0.06096   0.05447  -0.0233   0.0050   0.8823
  15.250   1.2678   0.06358   0.05717  -0.0232   0.0045   0.8830
  15.500   1.2721   0.06612   0.05980  -0.0233   0.0044   0.8836
  15.750   1.2742   0.06899   0.06277  -0.0234   0.0042   0.8841
  16.000   1.2786   0.07160   0.06548  -0.0236   0.0041   0.8846
  16.250   1.2815   0.07448   0.06848  -0.0239   0.0039   0.8852
  16.500   1.2849   0.07733   0.07143  -0.0244   0.0038   0.8857
  16.750   1.2865   0.08050   0.07470  -0.0249   0.0037   0.8861
  17.000   1.2883   0.08368   0.07799  -0.0256   0.0035   0.8866
  17.250   1.2897   0.08696   0.08137  -0.0263   0.0034   0.8871
  17.500   1.2899   0.09047   0.08498  -0.0272   0.0033   0.8875
  17.750   1.2879   0.09441   0.08903  -0.0283   0.0032   0.8879
  18.000   1.2878   0.09810   0.09282  -0.0294   0.0032   0.8883
  18.500   1.2834   0.10625   0.10121  -0.0322   0.0030   0.8892
  18.750   1.2801   0.11060   0.10567  -0.0338   0.0030   0.8897
  19.000   1.2744   0.11541   0.11060  -0.0357   0.0029   0.8901
  19.250   1.2702   0.12005   0.11536  -0.0377   0.0029   0.8906
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