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AH 93-157 (ah93157-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: AH 93-157 (ah93157-il)
Reynolds number: 200,000
Max Cl/Cd: 74.88 at α=7.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-ah93157-il-200000.txt
Download as CSV file: xf-ah93157-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AH 93-157                                       
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.1738   0.11115   0.10750  -0.0925   0.9435   0.0561
 -12.000  -0.1657   0.10651   0.10282  -0.0979   0.9381   0.0592
 -11.750  -0.1824   0.09982   0.09615  -0.1094   0.9302   0.0612
 -11.500  -0.1645   0.09492   0.09120  -0.1101   0.9268   0.0625
 -11.250  -0.1406   0.09342   0.08965  -0.1092   0.9216   0.0646
 -11.000  -0.1309   0.09036   0.08657  -0.1111   0.9159   0.0669
 -10.750  -0.1268   0.08652   0.08269  -0.1142   0.9110   0.0691
 -10.500  -0.1629   0.07952   0.07574  -0.1229   0.9018   0.0728
 -10.250  -0.1966   0.07344   0.06958  -0.1285   0.8942   0.0730
 -10.000  -0.2314   0.07066   0.06671  -0.1274   0.8860   0.0732
  -9.750  -0.2588   0.06881   0.06471  -0.1242   0.8798   0.0733
  -9.500  -0.2010   0.06280   0.05893  -0.1276   0.8801   0.0761
  -9.250  -0.2096   0.06038   0.05649  -0.1263   0.8748   0.0770
  -9.000  -0.2231   0.05816   0.05422  -0.1239   0.8690   0.0779
  -8.750  -0.3260   0.04598   0.04098  -0.1135   0.8608   0.0503
  -8.500  -0.3263   0.04255   0.03744  -0.1112   0.8564   0.0487
  -8.250  -0.3306   0.03887   0.03342  -0.1077   0.8520   0.0464
  -8.000  -0.3300   0.03568   0.02977  -0.1043   0.8485   0.0459
  -7.750  -0.3224   0.03370   0.02748  -0.1017   0.8446   0.0466
  -7.500  -0.3125   0.03175   0.02520  -0.0993   0.8405   0.0471
  -7.250  -0.2981   0.02977   0.02284  -0.0972   0.8369   0.0477
  -7.000  -0.2793   0.02807   0.02079  -0.0957   0.8339   0.0486
  -6.750  -0.2577   0.02693   0.01929  -0.0945   0.8315   0.0502
  -6.500  -0.2403   0.02562   0.01782  -0.0932   0.8271   0.0522
  -6.250  -0.2184   0.02480   0.01700  -0.0925   0.8234   0.0547
  -6.000  -0.1936   0.02398   0.01605  -0.0920   0.8203   0.0572
  -5.750  -0.1679   0.02331   0.01521  -0.0915   0.8178   0.0604
  -5.500  -0.1414   0.02226   0.01413  -0.0914   0.8158   0.0647
  -5.250  -0.1245   0.02204   0.01394  -0.0898   0.8106   0.0686
  -5.000  -0.1022   0.02174   0.01354  -0.0889   0.8067   0.0732
  -4.750  -0.0791   0.02096   0.01286  -0.0882   0.8039   0.0806
  -4.500  -0.0548   0.02040   0.01226  -0.0875   0.8015   0.0889
  -4.250  -0.0334   0.02014   0.01200  -0.0865   0.7985   0.0999
  -4.000  -0.0217   0.02005   0.01203  -0.0841   0.7926   0.1117
  -3.750  -0.0018   0.01967   0.01173  -0.0829   0.7891   0.1328
  -3.500   0.0193   0.01904   0.01132  -0.0818   0.7865   0.1740
  -3.250   0.0371   0.01820   0.01099  -0.0802   0.7843   0.2807
  -3.000   0.0352   0.01805   0.01147  -0.0758   0.7769   0.4103
  -2.750   0.0384   0.01715   0.01191  -0.0703   0.7729   0.6923
  -2.500   0.0671   0.01813   0.01306  -0.0676   0.7709   0.8174
  -2.250   0.0918   0.01872   0.01352  -0.0655   0.7689   0.8502
  -2.000   0.0963   0.01970   0.01448  -0.0608   0.7618   0.8696
  -1.750   0.1149   0.02021   0.01491  -0.0581   0.7577   0.8890
  -1.500   0.1611   0.02053   0.01510  -0.0603   0.7560   0.9048
  -1.250   0.2513   0.02076   0.01514  -0.0711   0.7558   0.9190
  -1.000   0.3333   0.02071   0.01493  -0.0810   0.7550   0.9316
  -0.750   0.4182   0.02047   0.01455  -0.0917   0.7541   0.9458
  -0.500   0.4777   0.02014   0.01410  -0.0979   0.7525   0.9562
  -0.250   0.5246   0.02008   0.01401  -0.1023   0.7479   0.9654
   0.000   0.5701   0.01986   0.01375  -0.1063   0.7435   0.9749
   0.250   0.6128   0.01954   0.01337  -0.1096   0.7404   0.9832
   0.500   0.6579   0.01900   0.01276  -0.1133   0.7378   0.9879
   0.750   0.6932   0.01874   0.01246  -0.1152   0.7349   0.9922
   1.000   0.7230   0.01878   0.01254  -0.1166   0.7282   0.9964
   1.250   0.7586   0.01843   0.01216  -0.1185   0.7245   0.9997
   1.500   0.7852   0.01815   0.01182  -0.1184   0.7215   1.0000
   1.750   0.8008   0.01837   0.01208  -0.1167   0.7155   1.0000
   2.000   0.8205   0.01836   0.01208  -0.1155   0.7103   1.0000
   2.250   0.8456   0.01809   0.01177  -0.1150   0.7070   1.0000
   2.500   0.8687   0.01796   0.01163  -0.1143   0.7031   1.0000
   2.750   0.8828   0.01817   0.01190  -0.1122   0.6958   1.0000
   3.000   0.9082   0.01787   0.01159  -0.1118   0.6920   1.0000
   3.250   0.9368   0.01752   0.01119  -0.1119   0.6892   1.0000
   3.500   0.9461   0.01788   0.01166  -0.1090   0.6807   1.0000
   3.750   0.9724   0.01756   0.01133  -0.1086   0.6766   1.0000
   4.000   0.9950   0.01743   0.01121  -0.1078   0.6718   1.0000
   4.250   1.0106   0.01749   0.01133  -0.1058   0.6644   1.0000
   4.500   1.0385   0.01713   0.01095  -0.1057   0.6603   1.0000
   4.750   1.0529   0.01725   0.01115  -0.1034   0.6527   1.0000
   5.000   1.0765   0.01701   0.01092  -0.1026   0.6468   1.0000
   5.250   1.0982   0.01688   0.01082  -0.1016   0.6406   1.0000
   5.500   1.1151   0.01685   0.01086  -0.0997   0.6328   1.0000
   5.750   1.1407   0.01662   0.01062  -0.0992   0.6269   1.0000
   6.000   1.1534   0.01671   0.01079  -0.0966   0.6179   1.0000
   6.250   1.1746   0.01658   0.01068  -0.0954   0.6104   1.0000
   6.500   1.1907   0.01657   0.01072  -0.0932   0.6013   1.0000
   6.750   1.2043   0.01663   0.01083  -0.0907   0.5918   1.0000
   7.000   1.2278   0.01646   0.01064  -0.0898   0.5831   1.0000
   7.250   1.2333   0.01668   0.01095  -0.0859   0.5720   1.0000
   7.500   1.2446   0.01678   0.01109  -0.0829   0.5614   1.0000
   7.750   1.2587   0.01681   0.01111  -0.0804   0.5504   1.0000
   8.000   1.2655   0.01696   0.01126  -0.0766   0.5384   1.0000
   8.250   1.2637   0.01720   0.01155  -0.0712   0.5264   1.0000
   8.500   1.2629   0.01741   0.01177  -0.0661   0.5148   1.0000
   8.750   1.2579   0.01754   0.01189  -0.0601   0.5032   1.0000
   9.000   1.2471   0.01766   0.01195  -0.0530   0.4912   1.0000
   9.250   1.2283   0.01793   0.01224  -0.0450   0.4790   1.0000
   9.500   1.2231   0.01834   0.01261  -0.0397   0.4635   1.0000
   9.750   1.2237   0.01890   0.01310  -0.0359   0.4462   1.0000
  10.000   1.2266   0.01959   0.01374  -0.0326   0.4290   1.0000
  10.250   1.2298   0.02042   0.01456  -0.0298   0.4124   1.0000
  10.500   1.2332   0.02136   0.01550  -0.0271   0.3954   1.0000
  10.750   1.2369   0.02238   0.01651  -0.0246   0.3784   1.0000
  11.000   1.2402   0.02350   0.01761  -0.0223   0.3610   1.0000
  11.250   1.2427   0.02474   0.01883  -0.0200   0.3429   1.0000
  11.500   1.2440   0.02611   0.02015  -0.0178   0.3244   1.0000
  11.750   1.2454   0.02756   0.02156  -0.0157   0.3065   1.0000
  12.000   1.2463   0.02912   0.02311  -0.0137   0.2876   1.0000
  12.250   1.2454   0.03089   0.02484  -0.0117   0.2667   1.0000
  12.500   1.2430   0.03285   0.02673  -0.0098   0.2462   1.0000
  12.750   1.2402   0.03497   0.02880  -0.0081   0.2224   1.0000
  13.000   1.2348   0.03742   0.03114  -0.0063   0.1982   1.0000
  13.250   1.2266   0.04023   0.03382  -0.0047   0.1702   1.0000
  13.500   1.2162   0.04340   0.03682  -0.0032   0.1400   1.0000
  13.750   1.2029   0.04701   0.04023  -0.0018   0.1097   1.0000
  14.000   1.1899   0.05077   0.04382  -0.0007   0.0862   1.0000
  14.250   1.1785   0.05457   0.04750   0.0002   0.0711   1.0000
  14.500   1.1713   0.05807   0.05098   0.0008   0.0618   1.0000
  14.750   1.1637   0.06173   0.05464   0.0011   0.0554   1.0000
  15.000   1.1597   0.06510   0.05806   0.0013   0.0504   1.0000
  15.250   1.1538   0.06872   0.06170   0.0014   0.0468   1.0000
  15.500   1.1535   0.07180   0.06487   0.0013   0.0432   1.0000
  15.750   1.1498   0.07525   0.06831   0.0012   0.0405   1.0000
  16.000   1.1506   0.07819   0.07131   0.0012   0.0382   1.0000
  16.250   1.1540   0.08089   0.07410   0.0011   0.0362   1.0000
  16.500   1.1557   0.08381   0.07704   0.0007   0.0341   1.0000
  16.750   1.1608   0.08594   0.07912   0.0011   0.0321   1.0000
  17.000   1.1672   0.08832   0.08163   0.0009   0.0308   1.0000
  17.250   1.1737   0.09065   0.08407   0.0007   0.0295   1.0000
  17.500   1.1808   0.09286   0.08633   0.0006   0.0283   1.0000
  17.750   1.1905   0.09455   0.08799   0.0006   0.0270   1.0000
  18.000   1.2019   0.09608   0.08959   0.0011   0.0259   1.0000
  18.250   1.2049   0.09911   0.09281   0.0005   0.0252   1.0000
  18.500   1.2074   0.10220   0.09607  -0.0003   0.0245   1.0000
  18.750   1.2103   0.10524   0.09925  -0.0011   0.0238   1.0000
  19.000   1.2124   0.10841   0.10255  -0.0020   0.0231   1.0000
  19.250   1.2142   0.11163   0.10592  -0.0030   0.0228   1.0000
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