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AH 95-160 (ah95160-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: AH 95-160 (ah95160-il)
Reynolds number: 200,000
Max Cl/Cd: 73.66 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ah95160-il-200000-n5.txt
Download as CSV file: xf-ah95160-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AH 95-160                                       
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -10.250  -0.1990   0.09273   0.08775  -0.0730   0.7161   0.0243
 -10.000  -0.3811   0.04498   0.03967  -0.1114   0.7165   0.0232
  -9.750  -0.4033   0.03708   0.03104  -0.1156   0.7143   0.0234
  -9.500  -0.3880   0.03525   0.02907  -0.1163   0.7121   0.0237
  -9.250  -0.3704   0.03362   0.02727  -0.1168   0.7099   0.0241
  -9.000  -0.3513   0.03213   0.02557  -0.1172   0.7076   0.0247
  -8.750  -0.3323   0.03032   0.02348  -0.1176   0.7054   0.0255
  -8.500  -0.3132   0.02814   0.02086  -0.1178   0.7034   0.0265
  -8.250  -0.2922   0.02617   0.01842  -0.1180   0.7017   0.0274
  -7.750  -0.2426   0.02447   0.01654  -0.1184   0.6981   0.0287
  -7.500  -0.2173   0.02356   0.01548  -0.1187   0.6961   0.0296
  -7.250  -0.1917   0.02258   0.01430  -0.1188   0.6940   0.0307
  -7.000  -0.1657   0.02175   0.01330  -0.1190   0.6919   0.0320
  -6.750  -0.1389   0.02129   0.01282  -0.1192   0.6898   0.0333
  -6.500  -0.1120   0.02073   0.01213  -0.1194   0.6878   0.0351
  -6.250  -0.0851   0.02006   0.01130  -0.1195   0.6862   0.0368
  -6.000  -0.0580   0.01962   0.01083  -0.1197   0.6847   0.0384
  -5.750  -0.0304   0.01920   0.01030  -0.1199   0.6833   0.0408
  -5.500  -0.0030   0.01880   0.00987  -0.1202   0.6814   0.0434
  -5.250   0.0246   0.01849   0.00956  -0.1205   0.6792   0.0463
  -5.000   0.0521   0.01811   0.00913  -0.1207   0.6770   0.0495
  -4.750   0.0800   0.01787   0.00888  -0.1210   0.6749   0.0534
  -4.500   0.1079   0.01758   0.00856  -0.1212   0.6731   0.0575
  -4.250   0.1361   0.01736   0.00830  -0.1215   0.6714   0.0624
  -4.000   0.1642   0.01711   0.00803  -0.1218   0.6698   0.0674
  -3.750   0.1927   0.01693   0.00779  -0.1221   0.6683   0.0734
  -3.500   0.2211   0.01670   0.00754  -0.1224   0.6668   0.0795
  -3.250   0.2494   0.01656   0.00737  -0.1227   0.6650   0.0863
  -3.000   0.2771   0.01638   0.00726  -0.1230   0.6629   0.0939
  -2.750   0.3052   0.01625   0.00714  -0.1234   0.6609   0.1021
  -2.500   0.3335   0.01614   0.00704  -0.1237   0.6589   0.1125
  -2.250   0.3618   0.01598   0.00694  -0.1241   0.6570   0.1261
  -2.000   0.3903   0.01582   0.00683  -0.1245   0.6551   0.1466
  -1.750   0.4189   0.01558   0.00673  -0.1250   0.6534   0.1863
  -1.500   0.4474   0.01523   0.00665  -0.1256   0.6518   0.2693
  -1.250   0.4756   0.01476   0.00663  -0.1262   0.6505   0.4090
  -1.000   0.5027   0.01440   0.00674  -0.1263   0.6492   0.5537
  -0.750   0.5280   0.01436   0.00700  -0.1260   0.6469   0.6411
  -0.500   0.5535   0.01440   0.00720  -0.1255   0.6445   0.6963
  -0.250   0.5787   0.01444   0.00735  -0.1249   0.6422   0.7399
   0.000   0.6038   0.01450   0.00748  -0.1243   0.6401   0.7766
   0.250   0.6270   0.01455   0.00760  -0.1230   0.6384   0.8201
   0.500   0.6459   0.01456   0.00770  -0.1207   0.6367   0.8709
   0.750   0.6651   0.01454   0.00771  -0.1184   0.6352   0.9133
   1.000   0.6912   0.01452   0.00765  -0.1177   0.6338   0.9415
   1.250   0.7227   0.01461   0.00773  -0.1187   0.6318   0.9641
   1.500   0.7574   0.01481   0.00794  -0.1206   0.6292   0.9906
   1.750   0.7858   0.01502   0.00815  -0.1213   0.6268   0.9998
   2.000   0.8138   0.01521   0.00831  -0.1218   0.6245   0.9998
   2.250   0.8424   0.01536   0.00841  -0.1223   0.6224   0.9998
   2.500   0.8716   0.01548   0.00850  -0.1229   0.6206   0.9998
   2.750   0.9011   0.01561   0.00857  -0.1235   0.6190   0.9998
   3.000   0.9309   0.01572   0.00864  -0.1241   0.6177   0.9998
   3.250   0.9571   0.01602   0.00896  -0.1243   0.6151   0.9998
   3.500   0.9818   0.01638   0.00938  -0.1243   0.6118   0.9998
   3.750   1.0081   0.01664   0.00967  -0.1244   0.6091   0.9998
   4.000   1.0356   0.01682   0.00986  -0.1247   0.6068   0.9998
   4.250   1.0639   0.01695   0.00999  -0.1251   0.6048   0.9998
   4.500   1.0932   0.01704   0.01007  -0.1256   0.6031   0.9998
   4.750   1.1231   0.01711   0.01012  -0.1261   0.6015   0.9998
   5.000   1.1437   0.01763   0.01076  -0.1255   0.5974   0.9998
   5.250   1.1673   0.01798   0.01117  -0.1253   0.5939   0.9998
   5.500   1.1937   0.01813   0.01137  -0.1253   0.5909   0.9998
   5.750   1.2223   0.01816   0.01140  -0.1257   0.5884   0.9998
   6.000   1.2529   0.01808   0.01132  -0.1262   0.5862   0.9998
   6.250   1.2702   0.01861   0.01199  -0.1251   0.5806   0.9998
   6.500   1.2939   0.01874   0.01218  -0.1247   0.5758   0.9998
   6.750   1.3239   0.01852   0.01194  -0.1250   0.5719   0.9998
   7.000   1.3419   0.01885   0.01238  -0.1238   0.5651   0.9998
   7.250   1.3653   0.01882   0.01239  -0.1232   0.5584   0.9998
   7.500   1.3857   0.01895   0.01258  -0.1222   0.5509   0.9998
   7.750   1.4055   0.01908   0.01275  -0.1212   0.5427   0.9998
   8.000   1.4201   0.01946   0.01320  -0.1194   0.5344   0.9998
   8.250   1.4384   0.01964   0.01341  -0.1181   0.5265   0.9998
   8.500   1.4470   0.02039   0.01425  -0.1157   0.5171   0.9998
   8.750   1.4630   0.02080   0.01469  -0.1144   0.5077   0.9998
   9.000   1.4735   0.02159   0.01552  -0.1125   0.4965   0.9998
   9.250   1.4813   0.02266   0.01663  -0.1106   0.4839   0.9998
   9.500   1.4903   0.02371   0.01771  -0.1089   0.4693   0.9998
   9.750   1.4984   0.02486   0.01884  -0.1072   0.4522   0.9998
  10.000   1.5044   0.02619   0.02010  -0.1053   0.4321   0.9998
  10.250   1.5058   0.02792   0.02175  -0.1032   0.4079   0.9998
  10.500   1.5031   0.02999   0.02368  -0.1007   0.3816   0.9998
  10.750   1.4958   0.03247   0.02601  -0.0981   0.3548   0.9998
  11.000   1.4868   0.03519   0.02859  -0.0955   0.3287   0.9998
  11.250   1.4776   0.03798   0.03127  -0.0930   0.3045   0.9998
  11.500   1.4691   0.04087   0.03404  -0.0907   0.2817   0.9998
  11.750   1.4619   0.04376   0.03682  -0.0888   0.2607   0.9998
  12.000   1.4569   0.04656   0.03955  -0.0870   0.2405   0.9998
  12.250   1.4524   0.04940   0.04231  -0.0855   0.2220   0.9998
  12.500   1.4490   0.05221   0.04505  -0.0841   0.2051   0.9998
  12.750   1.4470   0.05495   0.04774  -0.0828   0.1895   0.9998
  13.000   1.4458   0.05766   0.05041  -0.0817   0.1753   0.9998
  13.250   1.4460   0.06028   0.05299  -0.0807   0.1623   0.9998
  13.500   1.4465   0.06290   0.05560  -0.0797   0.1507   0.9998
  13.750   1.4474   0.06551   0.05819  -0.0789   0.1402   0.9998
  14.250   1.4507   0.07069   0.06338  -0.0774   0.1220   0.9998
  14.500   1.4522   0.07332   0.06603  -0.0768   0.1145   0.9998
  14.750   1.4541   0.07596   0.06867  -0.0762   0.1072   0.9998
  15.000   1.4569   0.07852   0.07127  -0.0757   0.1010   0.9998
  15.250   1.4585   0.08124   0.07401  -0.0753   0.0952   0.9998
  15.500   1.4612   0.08384   0.07667  -0.0749   0.0900   0.9998
  15.750   1.4633   0.08654   0.07941  -0.0746   0.0849   0.9998
  16.000   1.4644   0.08938   0.08228  -0.0743   0.0807   0.9998
  16.250   1.4677   0.09198   0.08496  -0.0741   0.0764   0.9998
  16.500   1.4681   0.09497   0.08798  -0.0740   0.0725   0.9998
  16.750   1.4706   0.09772   0.09081  -0.0739   0.0690   0.9998
  17.000   1.4725   0.10054   0.09371  -0.0739   0.0656   0.9998
  17.250   1.4719   0.10372   0.09691  -0.0740   0.0627   0.9998
  17.500   1.4743   0.10653   0.09981  -0.0741   0.0598   0.9998
  17.750   1.4760   0.10943   0.10280  -0.0743   0.0570   0.9998
  18.000   1.4753   0.11272   0.10613  -0.0747   0.0546   0.9998
  18.250   1.4762   0.11578   0.10926  -0.0751   0.0525   0.9998
  18.500   1.4781   0.11873   0.11232  -0.0756   0.0502   0.9998
  18.750   1.4784   0.12193   0.11559  -0.0762   0.0481   0.9998
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