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AH 94-145 (ah94145-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: AH 94-145 (ah94145-il)
Reynolds number: 1,000,000
Max Cl/Cd: 177.42 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-ah94145-il-1000000.txt
Download as CSV file: xf-ah94145-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AH 94-145                                       
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.500  -0.1234   0.10524   0.10239  -0.0627   0.6864   0.0171
 -11.250  -0.5610   0.03498   0.03151  -0.1101   0.6974   0.0132
 -11.000  -0.5563   0.03101   0.02720  -0.1129   0.6949   0.0133
 -10.750  -0.5413   0.02865   0.02458  -0.1142   0.6930   0.0134
 -10.500  -0.5349   0.02399   0.01943  -0.1159   0.6915   0.0136
 -10.250  -0.5149   0.02202   0.01725  -0.1165   0.6898   0.0138
 -10.000  -0.4910   0.02088   0.01599  -0.1170   0.6878   0.0141
  -9.750  -0.4658   0.01996   0.01497  -0.1174   0.6859   0.0143
  -9.500  -0.4400   0.01915   0.01405  -0.1178   0.6840   0.0145
  -9.250  -0.4138   0.01836   0.01313  -0.1182   0.6821   0.0148
  -9.000  -0.3873   0.01760   0.01224  -0.1186   0.6802   0.0151
  -8.750  -0.3604   0.01691   0.01141  -0.1190   0.6780   0.0154
  -8.500  -0.3331   0.01623   0.01062  -0.1194   0.6765   0.0158
  -8.250  -0.3052   0.01563   0.00992  -0.1197   0.6751   0.0161
  -8.000  -0.2769   0.01517   0.00936  -0.1201   0.6735   0.0163
  -7.750  -0.2499   0.01410   0.00817  -0.1206   0.6718   0.0170
  -7.500  -0.2215   0.01364   0.00768  -0.1210   0.6702   0.0175
  -7.250  -0.1929   0.01326   0.00725  -0.1215   0.6686   0.0180
  -7.000  -0.1641   0.01287   0.00680  -0.1219   0.6670   0.0185
  -6.750  -0.1352   0.01251   0.00636  -0.1223   0.6652   0.0191
  -6.500  -0.1062   0.01221   0.00599  -0.1227   0.6633   0.0196
  -6.250  -0.0773   0.01173   0.00543  -0.1231   0.6610   0.0203
  -6.000  -0.0480   0.01136   0.00505  -0.1237   0.6600   0.0212
  -5.750  -0.0185   0.01109   0.00477  -0.1241   0.6588   0.0222
  -5.500   0.0111   0.01086   0.00451  -0.1246   0.6573   0.0232
  -5.250   0.0407   0.01052   0.00414  -0.1251   0.6557   0.0246
  -5.000   0.0704   0.01031   0.00392  -0.1256   0.6541   0.0263
  -4.750   0.1001   0.01014   0.00372  -0.1261   0.6525   0.0278
  -4.500   0.1300   0.00986   0.00344  -0.1266   0.6510   0.0305
  -4.250   0.1598   0.00973   0.00328  -0.1271   0.6495   0.0329
  -4.000   0.1896   0.00954   0.00310  -0.1277   0.6478   0.0371
  -3.750   0.2194   0.00944   0.00299  -0.1282   0.6459   0.0422
  -3.500   0.2493   0.00932   0.00289  -0.1287   0.6444   0.0481
  -3.250   0.2793   0.00922   0.00281  -0.1292   0.6432   0.0535
  -3.000   0.3093   0.00908   0.00271  -0.1298   0.6417   0.0610
  -2.750   0.3393   0.00897   0.00262  -0.1303   0.6401   0.0679
  -2.500   0.3693   0.00890   0.00256  -0.1309   0.6385   0.0737
  -2.250   0.3993   0.00878   0.00247  -0.1314   0.6368   0.0825
  -2.000   0.4293   0.00870   0.00239  -0.1320   0.6352   0.0901
  -1.750   0.4593   0.00862   0.00233  -0.1325   0.6336   0.1012
  -1.500   0.4895   0.00851   0.00228  -0.1332   0.6320   0.1245
  -1.250   0.5198   0.00837   0.00228  -0.1339   0.6300   0.1758
  -1.000   0.5507   0.00806   0.00228  -0.1350   0.6286   0.2802
  -0.750   0.5822   0.00762   0.00228  -0.1363   0.6273   0.4294
  -0.500   0.6138   0.00724   0.00231  -0.1375   0.6257   0.5776
  -0.250   0.6445   0.00706   0.00235  -0.1383   0.6240   0.6627
   0.000   0.6747   0.00694   0.00240  -0.1389   0.6223   0.7224
   0.250   0.7042   0.00686   0.00245  -0.1392   0.6207   0.7753
   0.500   0.7330   0.00684   0.00251  -0.1395   0.6191   0.8134
   0.750   0.7614   0.00686   0.00257  -0.1396   0.6173   0.8422
   1.000   0.7897   0.00694   0.00265  -0.1397   0.6153   0.8617
   1.250   0.8173   0.00702   0.00275  -0.1396   0.6133   0.8823
   1.500   0.8443   0.00705   0.00282  -0.1394   0.6118   0.9032
   1.750   0.8692   0.00706   0.00289  -0.1386   0.6100   0.9202
   2.000   0.8949   0.00708   0.00293  -0.1381   0.6081   0.9325
   2.250   0.9192   0.00708   0.00295  -0.1373   0.6061   0.9425
   2.500   0.9442   0.00708   0.00296  -0.1367   0.6042   0.9514
   3.000   0.9927   0.00712   0.00299  -0.1352   0.6000   0.9700
   3.250   1.0178   0.00713   0.00301  -0.1347   0.5977   0.9815
   3.500   1.0489   0.00710   0.00302  -0.1356   0.5956   0.9998
   3.750   1.0802   0.00715   0.00307  -0.1365   0.5929   0.9998
   4.000   1.1112   0.00718   0.00311  -0.1374   0.5897   0.9998
   4.250   1.1418   0.00723   0.00314  -0.1383   0.5857   0.9998
   4.500   1.1722   0.00729   0.00320  -0.1391   0.5812   0.9998
   4.750   1.2025   0.00730   0.00324  -0.1398   0.5761   0.9998
   5.000   1.2323   0.00736   0.00328  -0.1405   0.5706   0.9998
   5.250   1.2621   0.00743   0.00337  -0.1412   0.5654   0.9998
   5.500   1.2917   0.00749   0.00345  -0.1418   0.5592   0.9998
   5.750   1.3204   0.00762   0.00354  -0.1423   0.5532   0.9998
   6.000   1.3499   0.00769   0.00366  -0.1429   0.5477   0.9998
   6.250   1.3784   0.00781   0.00378  -0.1433   0.5413   0.9998
   6.500   1.4069   0.00793   0.00392  -0.1438   0.5345   0.9998
   6.750   1.4343   0.00811   0.00407  -0.1440   0.5245   0.9998
   7.000   1.4616   0.00828   0.00425  -0.1443   0.5121   0.9998
   7.250   1.4880   0.00851   0.00446  -0.1444   0.4988   0.9998
   7.500   1.5133   0.00880   0.00471  -0.1443   0.4831   0.9998
   7.750   1.5363   0.00923   0.00505  -0.1439   0.4603   0.9998
   8.000   1.5549   0.00992   0.00557  -0.1428   0.4242   0.9998
   8.250   1.5666   0.01099   0.00638  -0.1406   0.3761   0.9998
   8.500   1.5739   0.01221   0.00735  -0.1378   0.3303   0.9998
   8.750   1.5766   0.01339   0.00834  -0.1342   0.2942   0.9998
   9.000   1.5770   0.01473   0.00953  -0.1305   0.2635   0.9998
   9.250   1.5770   0.01633   0.01099  -0.1274   0.2357   0.9998
   9.500   1.5778   0.01811   0.01267  -0.1248   0.2105   0.9998
   9.750   1.5788   0.02008   0.01453  -0.1226   0.1882   0.9998
  10.000   1.5807   0.02207   0.01645  -0.1207   0.1688   0.9998
  10.250   1.5827   0.02412   0.01843  -0.1189   0.1521   0.9998
  10.500   1.5853   0.02614   0.02039  -0.1172   0.1378   0.9998
  10.750   1.5878   0.02816   0.02237  -0.1155   0.1244   0.9998
  11.000   1.5902   0.03017   0.02434  -0.1138   0.1125   0.9998
  11.250   1.5938   0.03209   0.02624  -0.1122   0.1026   0.9998
  11.500   1.5971   0.03404   0.02817  -0.1106   0.0940   0.9998
  11.750   1.5999   0.03603   0.03013  -0.1090   0.0863   0.9998
  12.000   1.6053   0.03782   0.03193  -0.1076   0.0797   0.9998
  12.250   1.6081   0.03991   0.03400  -0.1062   0.0728   0.9998
  12.500   1.6142   0.04171   0.03581  -0.1050   0.0677   0.9998
  12.750   1.6179   0.04377   0.03787  -0.1037   0.0623   0.9998
  13.000   1.6246   0.04558   0.03970  -0.1027   0.0581   0.9998
  13.250   1.6278   0.04777   0.04188  -0.1015   0.0533   0.9998
  13.500   1.6347   0.04959   0.04373  -0.1005   0.0499   0.9998
  13.750   1.6375   0.05184   0.04598  -0.0994   0.0460   0.9998
  14.000   1.6443   0.05373   0.04791  -0.0985   0.0434   0.9998
  14.250   1.6488   0.05587   0.05006  -0.0975   0.0406   0.9998
  14.500   1.6521   0.05816   0.05237  -0.0966   0.0378   0.9998
  14.750   1.6591   0.06006   0.05432  -0.0958   0.0361   0.9998
  15.000   1.6625   0.06238   0.05667  -0.0950   0.0341   0.9998
  15.250   1.6645   0.06486   0.05916  -0.0941   0.0319   0.9998
  15.500   1.6712   0.06688   0.06124  -0.0935   0.0307   0.9998
  15.750   1.6755   0.06917   0.06359  -0.0929   0.0293   0.9998
  16.000   1.6780   0.07163   0.06607  -0.0922   0.0278   0.9998
  16.250   1.6787   0.07437   0.06886  -0.0915   0.0264   0.9998
  16.500   1.6848   0.07648   0.07104  -0.0910   0.0255   0.9998
  16.750   1.6878   0.07900   0.07361  -0.0906   0.0244   0.9998
  17.000   1.6896   0.08167   0.07631  -0.0901   0.0233   0.9998
  17.250   1.6875   0.08483   0.07952  -0.0896   0.0221   0.9998
  17.500   1.6914   0.08726   0.08203  -0.0893   0.0215   0.9998
  17.750   1.6944   0.08983   0.08467  -0.0891   0.0207   0.9998
  18.000   1.6952   0.09270   0.08760  -0.0889   0.0199   0.9998
  18.250   1.6948   0.09575   0.09069  -0.0887   0.0191   0.9998
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