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AH 93-156 (ah93156-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: AH 93-156 (ah93156-il)
Reynolds number: 500,000
Max Cl/Cd: 103.07 at α=7.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-ah93156-il-500000.txt
Download as CSV file: xf-ah93156-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AH 93-156                                       
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.3084   0.06903   0.06583  -0.1120   0.8187   0.0205
 -12.000  -0.3671   0.05389   0.05059  -0.1230   0.8156   0.0198
 -11.750  -0.3991   0.04815   0.04470  -0.1254   0.8120   0.0197
 -11.500  -0.4292   0.04392   0.04028  -0.1245   0.8086   0.0195
 -11.250  -0.4663   0.03973   0.03580  -0.1209   0.8053   0.0196
 -11.000  -0.4931   0.03650   0.03233  -0.1163   0.8021   0.0193
 -10.750  -0.5124   0.03410   0.02969  -0.1112   0.7986   0.0195
 -10.500  -0.5279   0.03166   0.02695  -0.1060   0.7955   0.0196
 -10.250  -0.5309   0.02938   0.02435  -0.1024   0.7930   0.0196
 -10.000  -0.5270   0.02758   0.02221  -0.0994   0.7907   0.0201
  -9.750  -0.5166   0.02629   0.02064  -0.0972   0.7886   0.0203
  -9.500  -0.5071   0.02427   0.01833  -0.0950   0.7866   0.0207
  -9.250  -0.4915   0.02263   0.01657  -0.0937   0.7843   0.0213
  -9.000  -0.4720   0.02190   0.01580  -0.0927   0.7819   0.0220
  -8.750  -0.4515   0.02132   0.01513  -0.0919   0.7797   0.0227
  -8.500  -0.4302   0.02065   0.01435  -0.0911   0.7778   0.0235
  -8.250  -0.4082   0.01997   0.01352  -0.0903   0.7760   0.0244
  -8.000  -0.3853   0.01935   0.01275  -0.0896   0.7743   0.0251
  -7.750  -0.3633   0.01808   0.01133  -0.0890   0.7725   0.0261
  -7.500  -0.3408   0.01741   0.01068  -0.0884   0.7706   0.0272
  -7.250  -0.3175   0.01696   0.01020  -0.0879   0.7684   0.0284
  -7.000  -0.2935   0.01655   0.00973  -0.0874   0.7663   0.0297
  -6.750  -0.2687   0.01628   0.00939  -0.0870   0.7644   0.0310
  -6.500  -0.2470   0.01538   0.00845  -0.0862   0.7626   0.0329
  -6.250  -0.2227   0.01502   0.00807  -0.0857   0.7608   0.0347
  -6.000  -0.1980   0.01469   0.00768  -0.0853   0.7590   0.0367
  -5.750  -0.1729   0.01446   0.00737  -0.0850   0.7572   0.0386
  -5.500  -0.1512   0.01393   0.00689  -0.0841   0.7555   0.0420
  -5.250  -0.1268   0.01368   0.00663  -0.0837   0.7534   0.0451
  -5.000  -0.1031   0.01335   0.00628  -0.0831   0.7512   0.0484
  -4.750  -0.0790   0.01304   0.00599  -0.0826   0.7491   0.0537
  -4.500  -0.0540   0.01279   0.00570  -0.0822   0.7472   0.0592
  -4.250  -0.0290   0.01252   0.00545  -0.0818   0.7454   0.0671
  -4.000  -0.0040   0.01224   0.00520  -0.0815   0.7438   0.0786
  -3.750   0.0214   0.01204   0.00502  -0.0812   0.7420   0.0950
  -3.500   0.0451   0.01178   0.00490  -0.0807   0.7400   0.1215
  -3.250   0.0682   0.01147   0.00479  -0.0801   0.7378   0.1642
  -3.000   0.0907   0.01110   0.00467  -0.0794   0.7354   0.2287
  -2.750   0.1117   0.01062   0.00455  -0.0786   0.7331   0.3244
  -2.500   0.1309   0.01001   0.00439  -0.0774   0.7310   0.4503
  -2.250   0.1428   0.00904   0.00421  -0.0746   0.7290   0.6594
  -2.000   0.1629   0.00911   0.00474  -0.0721   0.7272   0.7979
  -1.750   0.1888   0.00940   0.00500  -0.0715   0.7250   0.8281
  -1.500   0.2140   0.00966   0.00524  -0.0708   0.7224   0.8435
  -1.250   0.2398   0.00998   0.00555  -0.0699   0.7196   0.8522
  -1.000   0.2659   0.01018   0.00571  -0.0693   0.7169   0.8615
  -0.750   0.2926   0.01041   0.00589  -0.0686   0.7144   0.8694
  -0.500   0.3195   0.01058   0.00600  -0.0680   0.7122   0.8767
  -0.250   0.3455   0.01079   0.00618  -0.0673   0.7098   0.8824
   0.000   0.3681   0.01093   0.00634  -0.0660   0.7067   0.8905
   0.250   0.3923   0.01113   0.00653  -0.0646   0.7037   0.8987
   0.500   0.4182   0.01124   0.00663  -0.0636   0.7010   0.9077
   0.750   0.4431   0.01134   0.00669  -0.0626   0.6986   0.9177
   1.000   0.4822   0.01136   0.00666  -0.0645   0.6964   0.9219
   1.250   0.5082   0.01135   0.00666  -0.0643   0.6933   0.9259
   1.500   0.5214   0.01129   0.00661  -0.0616   0.6896   0.9309
   1.750   0.5503   0.01114   0.00645  -0.0620   0.6864   0.9323
   2.000   0.5808   0.01103   0.00629  -0.0627   0.6836   0.9335
   2.250   0.6114   0.01095   0.00617  -0.0635   0.6810   0.9347
   2.500   0.6351   0.01090   0.00616  -0.0629   0.6771   0.9369
   2.750   0.6579   0.01081   0.00608  -0.0621   0.6731   0.9391
   3.000   0.6808   0.01070   0.00596  -0.0613   0.6694   0.9416
   3.250   0.7041   0.01062   0.00584  -0.0607   0.6662   0.9436
   3.500   0.7258   0.01051   0.00578  -0.0597   0.6615   0.9452
   3.750   0.7520   0.01038   0.00567  -0.0596   0.6565   0.9467
   4.000   0.7798   0.01028   0.00555  -0.0598   0.6523   0.9479
   4.250   0.8037   0.01022   0.00552  -0.0593   0.6473   0.9493
   4.500   0.8266   0.01014   0.00547  -0.0585   0.6414   0.9511
   4.750   0.8526   0.01005   0.00536  -0.0584   0.6362   0.9527
   5.000   0.8703   0.00999   0.00536  -0.0566   0.6290   0.9547
   5.250   0.8925   0.00992   0.00527  -0.0557   0.6224   0.9562
   5.500   0.9124   0.00986   0.00526  -0.0545   0.6146   0.9580
   5.750   0.9368   0.00982   0.00520  -0.0541   0.6068   0.9592
   6.000   0.9575   0.00981   0.00524  -0.0530   0.5972   0.9607
   6.250   0.9791   0.00982   0.00526  -0.0521   0.5878   0.9621
   6.500   0.9990   0.00986   0.00529  -0.0508   0.5770   0.9639
   6.750   1.0158   0.00992   0.00537  -0.0490   0.5646   0.9662
   7.000   1.0306   0.01000   0.00545  -0.0468   0.5520   0.9683
   7.250   1.0420   0.01011   0.00555  -0.0440   0.5380   0.9705
   7.500   1.0587   0.01034   0.00577  -0.0425   0.5229   0.9727
   7.750   1.0763   0.01067   0.00607  -0.0412   0.5070   0.9753
   8.000   1.0929   0.01108   0.00645  -0.0400   0.4900   0.9778
   8.250   1.1090   0.01161   0.00693  -0.0389   0.4723   0.9803
   8.500   1.1262   0.01224   0.00753  -0.0383   0.4541   0.9828
   8.750   1.1450   0.01303   0.00827  -0.0383   0.4323   0.9853
   9.000   1.1612   0.01398   0.00915  -0.0381   0.4105   0.9890
   9.250   1.1763   0.01496   0.01008  -0.0377   0.3882   0.9988
   9.500   1.1780   0.01589   0.01095  -0.0346   0.3692   1.0000
   9.750   1.1811   0.01687   0.01187  -0.0318   0.3513   1.0000
  10.000   1.1848   0.01796   0.01290  -0.0293   0.3327   1.0000
  10.250   1.1913   0.01903   0.01391  -0.0273   0.3128   1.0000
  10.500   1.1941   0.02037   0.01515  -0.0251   0.2891   1.0000
  10.750   1.2002   0.02159   0.01630  -0.0233   0.2696   1.0000
  11.000   1.2030   0.02305   0.01764  -0.0213   0.2452   1.0000
  11.250   1.2059   0.02455   0.01904  -0.0194   0.2213   1.0000
  11.500   1.2087   0.02613   0.02050  -0.0176   0.1988   1.0000
  11.750   1.2114   0.02779   0.02204  -0.0159   0.1737   1.0000
  12.000   1.2145   0.02947   0.02362  -0.0144   0.1519   1.0000
  12.250   1.2159   0.03133   0.02534  -0.0128   0.1283   1.0000
  12.500   1.2172   0.03327   0.02715  -0.0113   0.1049   1.0000
  12.750   1.2193   0.03520   0.02899  -0.0100   0.0862   1.0000
  13.000   1.2208   0.03725   0.03094  -0.0088   0.0681   1.0000
  13.250   1.2215   0.03942   0.03302  -0.0076   0.0531   1.0000
  13.500   1.2229   0.04159   0.03515  -0.0065   0.0410   1.0000
  13.750   1.2241   0.04387   0.03738  -0.0055   0.0322   1.0000
  14.000   1.2256   0.04618   0.03970  -0.0047   0.0262   1.0000
  14.250   1.2276   0.04850   0.04205  -0.0040   0.0225   1.0000
  14.500   1.2295   0.05091   0.04448  -0.0034   0.0198   1.0000
  14.750   1.2309   0.05344   0.04709  -0.0029   0.0176   1.0000
  15.000   1.2329   0.05597   0.04967  -0.0025   0.0161   1.0000
  15.250   1.2296   0.05910   0.05287  -0.0021   0.0149   1.0000
  15.500   1.2346   0.06142   0.05527  -0.0020   0.0141   1.0000
  15.750   1.2343   0.06440   0.05834  -0.0020   0.0133   1.0000
  16.000   1.2363   0.06716   0.06115  -0.0021   0.0125   1.0000
  16.250   1.2301   0.07094   0.06501  -0.0022   0.0120   1.0000
  16.500   1.2266   0.07448   0.06866  -0.0025   0.0115   1.0000
  16.750   1.2256   0.07782   0.07209  -0.0028   0.0112   1.0000
  17.000   1.2241   0.08127   0.07563  -0.0034   0.0110   1.0000
  17.250   1.2237   0.08463   0.07909  -0.0040   0.0107   1.0000
  17.500   1.2217   0.08823   0.08278  -0.0048   0.0102   1.0000
  17.750   1.2200   0.09184   0.08648  -0.0056   0.0103   1.0000
  18.000   1.2177   0.09560   0.09031  -0.0065   0.0099   1.0000
  18.250   1.2145   0.09950   0.09428  -0.0076   0.0097   1.0000
  18.500   1.2128   0.10323   0.09809  -0.0087   0.0096   1.0000
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