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AH 94-145 (ah94145-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: AH 94-145 (ah94145-il)
Reynolds number: 500,000
Max Cl/Cd: 132.4 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ah94145-il-500000-n5.txt
Download as CSV file: xf-ah94145-il-500000-n5.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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.2489   0.11858   0.11481  -0.0500   0.6908   0.0118
 -11.500  -0.2442   0.11490   0.11113  -0.0517   0.6893   0.0121
 -11.000  -0.5539   0.03274   0.02824  -0.1119   0.6912   0.0126
 -10.750  -0.5438   0.02927   0.02440  -0.1137   0.6891   0.0128
 -10.500  -0.5273   0.02685   0.02164  -0.1148   0.6870   0.0130
 -10.250  -0.5073   0.02499   0.01950  -0.1155   0.6851   0.0132
 -10.000  -0.4851   0.02352   0.01777  -0.1160   0.6832   0.0134
  -9.750  -0.4622   0.02218   0.01626  -0.1165   0.6813   0.0136
  -9.500  -0.4372   0.02132   0.01528  -0.1170   0.6796   0.0139
  -9.250  -0.4114   0.02062   0.01447  -0.1174   0.6779   0.0142
  -9.000  -0.3851   0.01992   0.01366  -0.1178   0.6762   0.0146
  -8.750  -0.3586   0.01917   0.01280  -0.1182   0.6744   0.0150
  -8.500  -0.3318   0.01840   0.01189  -0.1186   0.6724   0.0154
  -8.250  -0.3048   0.01766   0.01101  -0.1189   0.6706   0.0157
  -8.000  -0.2774   0.01700   0.01021  -0.1193   0.6689   0.0161
  -7.750  -0.2497   0.01641   0.00949  -0.1197   0.6672   0.0164
  -7.500  -0.2222   0.01576   0.00878  -0.1201   0.6656   0.0169
  -7.250  -0.1941   0.01531   0.00825  -0.1205   0.6640   0.0174
  -7.000  -0.1658   0.01491   0.00777  -0.1209   0.6623   0.0179
  -6.750  -0.1374   0.01451   0.00729  -0.1212   0.6606   0.0186
  -6.500  -0.1086   0.01413   0.00685  -0.1217   0.6590   0.0194
  -6.250  -0.0798   0.01374   0.00640  -0.1221   0.6575   0.0202
  -6.000  -0.0509   0.01340   0.00605  -0.1226   0.6559   0.0212
  -5.750  -0.0219   0.01310   0.00571  -0.1230   0.6541   0.0222
  -5.500   0.0073   0.01282   0.00536  -0.1234   0.6524   0.0233
  -5.250   0.0364   0.01251   0.00503  -0.1239   0.6506   0.0245
  -5.000   0.0657   0.01227   0.00475  -0.1243   0.6490   0.0261
  -4.750   0.0950   0.01207   0.00450  -0.1247   0.6475   0.0280
  -4.500   0.1243   0.01186   0.00427  -0.1252   0.6461   0.0306
  -4.250   0.1538   0.01169   0.00406  -0.1257   0.6446   0.0335
  -4.000   0.1833   0.01149   0.00389  -0.1262   0.6430   0.0370
  -3.750   0.2129   0.01132   0.00374  -0.1267   0.6413   0.0412
  -3.500   0.2426   0.01118   0.00360  -0.1272   0.6395   0.0464
  -3.250   0.2722   0.01105   0.00349  -0.1277   0.6379   0.0521
  -3.000   0.3018   0.01093   0.00338  -0.1282   0.6363   0.0583
  -2.750   0.3315   0.01083   0.00327  -0.1286   0.6348   0.0643
  -2.500   0.3611   0.01073   0.00318  -0.1292   0.6333   0.0714
  -2.250   0.3908   0.01064   0.00309  -0.1296   0.6317   0.0790
  -2.000   0.4204   0.01058   0.00301  -0.1301   0.6301   0.0870
  -1.750   0.4502   0.01049   0.00295  -0.1307   0.6285   0.0982
  -1.500   0.4800   0.01038   0.00291  -0.1313   0.6269   0.1131
  -1.250   0.5098   0.01025   0.00287  -0.1319   0.6251   0.1391
  -1.000   0.5399   0.01007   0.00285  -0.1326   0.6232   0.1873
  -0.750   0.5701   0.00982   0.00283  -0.1335   0.6214   0.2680
  -0.500   0.6007   0.00952   0.00283  -0.1344   0.6197   0.3750
  -0.250   0.6315   0.00919   0.00286  -0.1355   0.6181   0.5044
   0.000   0.6618   0.00898   0.00292  -0.1363   0.6166   0.6023
   0.250   0.6914   0.00887   0.00297  -0.1368   0.6150   0.6740
   0.500   0.7203   0.00881   0.00305  -0.1371   0.6133   0.7269
   0.750   0.7477   0.00874   0.00318  -0.1370   0.6115   0.7847
   1.000   0.7719   0.00873   0.00333  -0.1360   0.6096   0.8488
   1.250   0.7961   0.00877   0.00345  -0.1350   0.6077   0.8858
   1.500   0.8207   0.00881   0.00352  -0.1342   0.6058   0.9056
   1.750   0.8468   0.00885   0.00356  -0.1339   0.6039   0.9187
   2.000   0.8719   0.00888   0.00359  -0.1333   0.6019   0.9289
   2.250   0.8978   0.00892   0.00361  -0.1329   0.6001   0.9378
   2.500   0.9241   0.00898   0.00365  -0.1326   0.5984   0.9470
   2.750   0.9488   0.00898   0.00371  -0.1320   0.5962   0.9570
   3.000   0.9750   0.00900   0.00376  -0.1317   0.5939   0.9679
   3.250   1.0039   0.00903   0.00381  -0.1321   0.5915   0.9805
   3.500   1.0350   0.00908   0.00386  -0.1330   0.5891   0.9998
   3.750   1.0651   0.00917   0.00395  -0.1338   0.5869   0.9998
   4.000   1.0951   0.00927   0.00404  -0.1345   0.5847   0.9998
   4.250   1.1249   0.00937   0.00416  -0.1351   0.5821   0.9998
   4.500   1.1543   0.00947   0.00430  -0.1358   0.5787   0.9998
   4.750   1.1835   0.00955   0.00442  -0.1363   0.5747   0.9998
   5.000   1.2124   0.00963   0.00447  -0.1368   0.5698   0.9998
   5.250   1.2409   0.00971   0.00459  -0.1372   0.5631   0.9998
   5.500   1.2689   0.00980   0.00467  -0.1375   0.5551   0.9998
   5.750   1.2966   0.00991   0.00480  -0.1378   0.5461   0.9998
   6.000   1.3237   0.01005   0.00493  -0.1380   0.5372   0.9998
   6.250   1.3505   0.01021   0.00511  -0.1381   0.5264   0.9998
   6.500   1.3770   0.01040   0.00530  -0.1382   0.5154   0.9998
   6.750   1.4026   0.01063   0.00552  -0.1381   0.5042   0.9998
   7.000   1.4272   0.01092   0.00578  -0.1379   0.4907   0.9998
   7.250   1.4502   0.01127   0.00610  -0.1374   0.4731   0.9998
   7.500   1.4690   0.01184   0.00655  -0.1363   0.4465   0.9998
   7.750   1.4820   0.01269   0.00723  -0.1343   0.4094   0.9998
   8.000   1.4873   0.01388   0.00821  -0.1313   0.3683   0.9998
   8.250   1.4858   0.01523   0.00939  -0.1272   0.3334   0.9998
   8.500   1.4842   0.01687   0.01088  -0.1238   0.3021   0.9998
   8.750   1.4831   0.01875   0.01264  -0.1210   0.2738   0.9998
   9.000   1.4823   0.02084   0.01462  -0.1186   0.2480   0.9998
   9.250   1.4811   0.02309   0.01677  -0.1165   0.2236   0.9998
   9.500   1.4811   0.02533   0.01892  -0.1146   0.2015   0.9998
   9.750   1.4812   0.02756   0.02108  -0.1128   0.1817   0.9998
  10.000   1.4818   0.02977   0.02321  -0.1110   0.1644   0.9998
  10.500   1.4856   0.03395   0.02730  -0.1077   0.1360   0.9998
  10.750   1.4894   0.03589   0.02922  -0.1062   0.1244   0.9998
  11.000   1.4937   0.03779   0.03110  -0.1047   0.1147   0.9998
  11.250   1.4974   0.03979   0.03308  -0.1033   0.1059   0.9998
  11.500   1.5015   0.04176   0.03504  -0.1020   0.0973   0.9998
  11.750   1.5073   0.04366   0.03695  -0.1009   0.0901   0.9998
  12.000   1.5121   0.04565   0.03894  -0.0997   0.0832   0.9998
  12.250   1.5182   0.04759   0.04089  -0.0987   0.0771   0.9998
  12.500   1.5234   0.04959   0.04290  -0.0976   0.0716   0.9998
  12.750   1.5290   0.05160   0.04492  -0.0967   0.0661   0.9998
  13.000   1.5342   0.05368   0.04701  -0.0957   0.0614   0.9998
  13.250   1.5404   0.05567   0.04903  -0.0949   0.0570   0.9998
  13.500   1.5448   0.05787   0.05125  -0.0940   0.0531   0.9998
  13.750   1.5514   0.05985   0.05327  -0.0932   0.0498   0.9998
  14.000   1.5557   0.06211   0.05555  -0.0924   0.0465   0.9998
  14.250   1.5612   0.06426   0.05774  -0.0917   0.0437   0.9998
  14.500   1.5666   0.06644   0.05997  -0.0910   0.0411   0.9998
  14.750   1.5701   0.06886   0.06241  -0.0904   0.0388   0.9998
  15.000   1.5755   0.07106   0.06468  -0.0898   0.0368   0.9998
  15.250   1.5796   0.07344   0.06712  -0.0892   0.0349   0.9998
  15.500   1.5829   0.07593   0.06965  -0.0887   0.0331   0.9998
  15.750   1.5859   0.07848   0.07225  -0.0882   0.0315   0.9998
  16.000   1.5902   0.08092   0.07476  -0.0878   0.0300   0.9998
  16.250   1.5933   0.08348   0.07738  -0.0874   0.0286   0.9998
  16.500   1.5946   0.08630   0.08025  -0.0871   0.0273   0.9998
  16.750   1.5969   0.08900   0.08302  -0.0868   0.0261   0.9998
  17.000   1.5995   0.09172   0.08582  -0.0866   0.0251   0.9998
  17.250   1.6017   0.09447   0.08864  -0.0865   0.0240   0.9998
  17.500   1.6019   0.09754   0.09177  -0.0865   0.0229   0.9998
  17.750   1.6016   0.10068   0.09496  -0.0865   0.0220   0.9998
  18.000   1.6030   0.10361   0.09799  -0.0866   0.0212   0.9998
  18.250   1.6042   0.10657   0.10104  -0.0867   0.0204   0.9998
  18.500   1.6039   0.10980   0.10434  -0.0870   0.0196   0.9998
  18.750   1.6030   0.11310   0.10771  -0.0874   0.0189   0.9998
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