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WORTMANN FX L V-152 AIRFOIL (fxlv152-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX L V-152 AIRFOIL (fxlv152-il)
Reynolds number: 500,000
Max Cl/Cd: 53.94 at α=9.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fxlv152-il-500000-n5.txt
Download as CSV file: xf-fxlv152-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX L V-152 AIRFOIL                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -18.000  -1.1121   0.11970   0.11591   0.0245   1.0005   0.0051
 -17.750  -1.1275   0.11245   0.10854   0.0207   1.0005   0.0051
 -17.500  -1.1425   0.10548   0.10144   0.0172   1.0005   0.0051
 -17.250  -1.1567   0.09873   0.09456   0.0139   1.0005   0.0051
 -17.000  -1.1706   0.09224   0.08793   0.0108   1.0005   0.0051
 -16.750  -1.1830   0.08615   0.08172   0.0079   1.0005   0.0051
 -16.500  -1.1945   0.08041   0.07585   0.0054   1.0005   0.0051
 -16.250  -1.2045   0.07508   0.07040   0.0031   1.0005   0.0051
 -16.000  -1.2126   0.07020   0.06540   0.0011   1.0005   0.0052
 -15.750  -1.2198   0.06562   0.06070  -0.0006   1.0005   0.0052
 -15.500  -1.2253   0.06145   0.05641  -0.0020   1.0005   0.0052
 -15.250  -1.2300   0.05755   0.05240  -0.0032   1.0005   0.0052
 -15.000  -1.2338   0.05398   0.04872  -0.0041   1.0005   0.0053
 -14.750  -1.2364   0.05067   0.04531  -0.0048   1.0005   0.0053
 -14.500  -1.2378   0.04759   0.04212  -0.0054   1.0005   0.0054
 -14.250  -1.2375   0.04475   0.03917  -0.0058   1.0005   0.0055
 -14.000  -1.2355   0.04214   0.03647  -0.0060   1.0005   0.0055
 -13.750  -1.2321   0.03971   0.03394  -0.0062   1.0005   0.0056
 -13.500  -1.2272   0.03749   0.03163  -0.0063   1.0005   0.0057
 -13.250  -1.2208   0.03542   0.02947  -0.0063   1.0005   0.0058
 -13.000  -1.2132   0.03349   0.02746  -0.0063   1.0005   0.0059
 -12.750  -1.2042   0.03172   0.02560  -0.0063   1.0005   0.0059
 -12.500  -1.1941   0.03008   0.02388  -0.0062   1.0005   0.0060
 -12.250  -1.1831   0.02855   0.02227  -0.0060   1.0005   0.0061
 -12.000  -1.1710   0.02713   0.02078  -0.0059   1.0005   0.0061
 -11.750  -1.1581   0.02581   0.01938  -0.0057   1.0005   0.0062
 -11.500  -1.1446   0.02459   0.01809  -0.0054   1.0005   0.0063
 -11.250  -1.1303   0.02348   0.01691  -0.0051   1.0005   0.0064
 -11.000  -1.1157   0.02246   0.01584  -0.0046   1.0005   0.0065
 -10.750  -1.0976   0.02168   0.01486  -0.0043   0.8799   0.0068
 -10.500  -1.0839   0.02103   0.01403  -0.0029   0.8443   0.0070
 -10.250  -1.0662   0.02035   0.01323  -0.0021   0.8193   0.0074
 -10.000  -1.0473   0.01968   0.01248  -0.0014   0.7983   0.0079
  -9.500  -1.0039   0.01872   0.01136  -0.0006   0.7661   0.0144
  -9.250  -0.9811   0.01828   0.01083  -0.0003   0.7563   0.0154
  -9.000  -0.9573   0.01790   0.01036  -0.0001   0.7475   0.0164
  -8.750  -0.9331   0.01754   0.00991   0.0001   0.7395   0.0171
  -8.500  -0.9094   0.01706   0.00939   0.0003   0.7312   0.0179
  -8.250  -0.8850   0.01666   0.00892   0.0005   0.7225   0.0187
  -8.000  -0.8599   0.01629   0.00849   0.0006   0.7139   0.0195
  -7.750  -0.8352   0.01587   0.00801   0.0007   0.7051   0.0205
  -7.500  -0.8101   0.01547   0.00757   0.0008   0.6980   0.0216
  -7.250  -0.7847   0.01510   0.00714   0.0009   0.6910   0.0230
  -7.000  -0.7595   0.01469   0.00672   0.0010   0.6849   0.0254
  -6.500  -0.7083   0.01389   0.00594   0.0010   0.6755   0.0428
  -6.250  -0.6825   0.01350   0.00559   0.0010   0.6712   0.0529
  -6.000  -0.6560   0.01321   0.00528   0.0010   0.6672   0.0640
  -5.750  -0.6293   0.01290   0.00499   0.0009   0.6636   0.0727
  -5.250  -0.5769   0.01210   0.00436   0.0008   0.6554   0.1122
  -5.000  -0.5508   0.01169   0.00406   0.0008   0.6515   0.1399
  -4.750  -0.5243   0.01134   0.00378   0.0007   0.6480   0.1652
  -4.500  -0.4984   0.01083   0.00345   0.0007   0.6450   0.2037
  -4.000  -0.4453   0.00998   0.00294   0.0005   0.6386   0.2895
  -3.750  -0.4183   0.00964   0.00271   0.0004   0.6353   0.3219
  -3.500  -0.3925   0.00914   0.00246   0.0004   0.6321   0.3818
  -3.250  -0.3656   0.00885   0.00232   0.0003   0.6289   0.4305
  -3.000  -0.3377   0.00866   0.00223   0.0002   0.6260   0.4645
  -2.750  -0.3098   0.00850   0.00218   0.0001   0.6229   0.4891
  -2.500  -0.2813   0.00842   0.00217   0.0000   0.6193   0.5094
  -2.250  -0.2524   0.00840   0.00214  -0.0002   0.6155   0.5240
  -2.000  -0.2235   0.00841   0.00212  -0.0003   0.6118   0.5367
  -1.750  -0.1947   0.00839   0.00210  -0.0005   0.6085   0.5467
  -1.500  -0.1654   0.00840   0.00209  -0.0007   0.6055   0.5559
  -1.250  -0.1364   0.00837   0.00208  -0.0009   0.6025   0.5619
  -1.000  -0.1074   0.00835   0.00207  -0.0011   0.5992   0.5676
  -0.750  -0.0783   0.00835   0.00204  -0.0014   0.5957   0.5723
  -0.500  -0.0491   0.00837   0.00201  -0.0016   0.5922   0.5763
  -0.250  -0.0202   0.00835   0.00201  -0.0018   0.5886   0.5806
   0.000   0.0089   0.00833   0.00202  -0.0020   0.5839   0.5846
   0.250   0.0379   0.00833   0.00202  -0.0022   0.5790   0.5886
   0.500   0.0670   0.00835   0.00202  -0.0024   0.5750   0.5926
   1.000   0.1252   0.00836   0.00205  -0.0028   0.5654   0.5986
   1.250   0.1541   0.00836   0.00207  -0.0030   0.5594   0.6016
   1.500   0.1829   0.00839   0.00209  -0.0031   0.5538   0.6051
   1.750   0.2121   0.00839   0.00213  -0.0034   0.5458   0.6091
   2.000   0.2409   0.00842   0.00212  -0.0035   0.5339   0.6128
   2.250   0.2699   0.00842   0.00215  -0.0037   0.5205   0.6160
   2.500   0.2984   0.00844   0.00217  -0.0038   0.5038   0.6194
   2.750   0.3262   0.00855   0.00219  -0.0038   0.4795   0.6229
   3.000   0.3540   0.00870   0.00226  -0.0039   0.4564   0.6262
   3.250   0.3816   0.00889   0.00236  -0.0039   0.4231   0.6293
   3.500   0.4077   0.00929   0.00252  -0.0038   0.3636   0.6323
   3.750   0.4337   0.00969   0.00274  -0.0038   0.3201   0.6353
   4.000   0.4600   0.01004   0.00299  -0.0038   0.2861   0.6386
   4.250   0.4857   0.01051   0.00326  -0.0037   0.2342   0.6420
   4.500   0.5119   0.01090   0.00352  -0.0037   0.1966   0.6454
   4.750   0.5373   0.01141   0.00385  -0.0036   0.1597   0.6487
   5.000   0.5632   0.01183   0.00414  -0.0036   0.1319   0.6517
   5.250   0.5889   0.01222   0.00444  -0.0036   0.1052   0.6549
   5.500   0.6148   0.01258   0.00473  -0.0035   0.0855   0.6585
   5.750   0.6406   0.01294   0.00504  -0.0034   0.0722   0.6626
   6.000   0.6667   0.01328   0.00535  -0.0034   0.0611   0.6668
   6.250   0.6923   0.01365   0.00568  -0.0033   0.0466   0.6713
   6.500   0.7177   0.01400   0.00604  -0.0032   0.0396   0.6765
   6.750   0.7433   0.01433   0.00639  -0.0031   0.0314   0.6819
   7.250   0.7924   0.01522   0.00727  -0.0027   0.0215   0.6924
   7.500   0.8172   0.01561   0.00771  -0.0025   0.0204   0.6988
   7.750   0.8422   0.01597   0.00811  -0.0023   0.0198   0.7056
   8.000   0.8669   0.01633   0.00854  -0.0021   0.0190   0.7126
   8.250   0.8910   0.01675   0.00901  -0.0019   0.0181   0.7206
   8.500   0.9145   0.01719   0.00951  -0.0016   0.0173   0.7284
   8.750   0.9387   0.01753   0.00993  -0.0014   0.0165   0.7372
   9.000   0.9623   0.01792   0.01038  -0.0011   0.0156   0.7455
   9.250   0.9852   0.01833   0.01088  -0.0007   0.0146   0.7548
   9.500   1.0082   0.01869   0.01135  -0.0003   0.0133   0.7652
  10.000   1.0482   0.01982   0.01260   0.0009   0.0076   0.7995
  10.250   1.0663   0.02046   0.01335   0.0018   0.0071   0.8209
  10.500   1.0822   0.02110   0.01412   0.0029   0.0068   0.8464
  10.750   1.0953   0.02174   0.01495   0.0045   0.0066   0.8854
  11.000   1.1123   0.02251   0.01589   0.0050   0.0065   0.9995
  11.250   1.1269   0.02352   0.01697   0.0054   0.0064   0.9995
  11.500   1.1408   0.02464   0.01815   0.0058   0.0063   0.9995
  11.750   1.1541   0.02585   0.01943   0.0062   0.0062   0.9995
  12.000   1.1666   0.02716   0.02082   0.0064   0.0061   0.9995
  12.250   1.1783   0.02858   0.02231   0.0067   0.0061   0.9995
  12.500   1.1889   0.03009   0.02390   0.0069   0.0060   0.9995
  12.750   1.1986   0.03171   0.02559   0.0071   0.0059   0.9995
  13.000   1.2072   0.03345   0.02742   0.0072   0.0059   0.9995
  13.250   1.2145   0.03533   0.02938   0.0073   0.0058   0.9995
  13.500   1.2204   0.03736   0.03150   0.0074   0.0057   0.9995
  13.750   1.2249   0.03953   0.03376   0.0075   0.0057   0.9995
  14.000   1.2280   0.04188   0.03621   0.0074   0.0056   0.9995
  14.250   1.2296   0.04442   0.03884   0.0073   0.0055   0.9995
  14.500   1.2296   0.04717   0.04169   0.0071   0.0055   0.9995
  14.750   1.2280   0.05014   0.04476   0.0068   0.0054   0.9995
  15.000   1.2251   0.05333   0.04805   0.0063   0.0054   0.9995
  15.250   1.2210   0.05679   0.05162   0.0056   0.0053   0.9995
  15.500   1.2158   0.06059   0.05553   0.0045   0.0053   0.9995
  15.750   1.2095   0.06470   0.05975   0.0033   0.0052   0.9995
  16.000   1.2024   0.06905   0.06423   0.0018   0.0052   0.9995
  16.250   1.1941   0.07376   0.06905   0.0001   0.0052   0.9995
  16.500   1.1845   0.07877   0.07418  -0.0019   0.0052   0.9995
  16.750   1.1734   0.08420   0.07973  -0.0041   0.0052   0.9995
  17.000   1.1611   0.08998   0.08564  -0.0066   0.0052   0.9995
  17.250   1.1477   0.09610   0.09189  -0.0094   0.0052   0.9995
  17.500   1.1329   0.10263   0.09854  -0.0124   0.0052   0.9995
  17.750   1.1181   0.10927   0.10531  -0.0156   0.0052   0.9995
  18.000   1.1023   0.11624   0.11240  -0.0190   0.0052   0.9995
  18.250   1.0866   0.12335   0.11963  -0.0225   0.0052   0.9995
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