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FX 60-157 AIRFOIL (fx60157-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: FX 60-157 AIRFOIL (fx60157-il)
Reynolds number: 200,000
Max Cl/Cd: 57.24 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx60157-il-200000-n5.txt
Download as CSV file: xf-fx60157-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 60-157 AIRFOIL                               
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.6122   0.08048   0.07657  -0.0695   0.9983   0.0116
 -13.000  -0.6445   0.06933   0.06512  -0.0784   0.9957   0.0115
 -12.750  -0.6662   0.06170   0.05720  -0.0842   0.9930   0.0114
 -12.500  -0.6830   0.05595   0.05116  -0.0873   0.9894   0.0114
 -12.250  -0.6964   0.05089   0.04578  -0.0897   0.9859   0.0115
 -12.000  -0.7027   0.04658   0.04111  -0.0915   0.9830   0.0117
 -11.750  -0.7061   0.04346   0.03770  -0.0915   0.9786   0.0118
 -11.500  -0.7044   0.04057   0.03449  -0.0915   0.9744   0.0120
 -11.250  -0.6950   0.03820   0.03185  -0.0919   0.9715   0.0123
 -11.000  -0.6788   0.03663   0.03017  -0.0931   0.9694   0.0126
 -10.750  -0.6755   0.03539   0.02883  -0.0910   0.9632   0.0128
 -10.500  -0.6621   0.03405   0.02733  -0.0908   0.9597   0.0133
 -10.250  -0.6439   0.03254   0.02564  -0.0911   0.9572   0.0140
 -10.000  -0.6218   0.03103   0.02389  -0.0917   0.9555   0.0148
  -9.750  -0.6192   0.03019   0.02290  -0.0883   0.9487   0.0153
  -9.500  -0.6055   0.02935   0.02207  -0.0876   0.9449   0.0163
  -9.250  -0.5848   0.02835   0.02094  -0.0877   0.9425   0.0175
  -9.000  -0.5610   0.02716   0.01960  -0.0882   0.9408   0.0191
  -8.750  -0.5606   0.02651   0.01894  -0.0844   0.9331   0.0200
  -8.500  -0.5417   0.02560   0.01796  -0.0840   0.9298   0.0217
  -8.250  -0.5183   0.02463   0.01692  -0.0843   0.9275   0.0232
  -8.000  -0.4909   0.02389   0.01614  -0.0853   0.9258   0.0251
  -7.750  -0.4838   0.02347   0.01565  -0.0822   0.9191   0.0267
  -7.500  -0.4632   0.02292   0.01508  -0.0817   0.9153   0.0284
  -7.250  -0.4367   0.02246   0.01455  -0.0821   0.9131   0.0313
  -7.000  -0.4088   0.02188   0.01392  -0.0830   0.9113   0.0341
  -6.750  -0.3787   0.02133   0.01331  -0.0841   0.9100   0.0375
  -6.500  -0.3731   0.02101   0.01295  -0.0805   0.9025   0.0392
  -6.250  -0.3506   0.02045   0.01238  -0.0803   0.8993   0.0423
  -6.000  -0.3234   0.01988   0.01175  -0.0809   0.8972   0.0454
  -5.750  -0.2940   0.01923   0.01111  -0.0820   0.8955   0.0497
  -5.500  -0.2621   0.01865   0.01051  -0.0834   0.8943   0.0558
  -5.250  -0.2502   0.01844   0.01026  -0.0808   0.8872   0.0624
  -5.000  -0.2240   0.01795   0.00978  -0.0811   0.8837   0.0733
  -4.750  -0.1931   0.01734   0.00927  -0.0824   0.8815   0.0979
  -4.500  -0.1607   0.01655   0.00871  -0.0843   0.8800   0.1520
  -4.250  -0.1261   0.01548   0.00811  -0.0870   0.8788   0.2591
  -3.750  -0.0728   0.01398   0.00768  -0.0889   0.8709   0.4991
  -3.500  -0.0445   0.01388   0.00787  -0.0888   0.8676   0.5678
  -3.250  -0.0119   0.01390   0.00797  -0.0893   0.8651   0.6073
  -3.000   0.0245   0.01393   0.00798  -0.0906   0.8633   0.6358
  -2.750   0.0625   0.01402   0.00801  -0.0923   0.8618   0.6584
  -2.500   0.0725   0.01437   0.00837  -0.0885   0.8529   0.6704
  -2.250   0.1048   0.01447   0.00841  -0.0890   0.8499   0.6817
  -2.000   0.1423   0.01445   0.00832  -0.0907   0.8476   0.6917
  -1.750   0.1795   0.01443   0.00825  -0.0922   0.8458   0.6967
  -1.500   0.1894   0.01462   0.00845  -0.0885   0.8367   0.7008
  -1.250   0.2239   0.01452   0.00829  -0.0899   0.8334   0.7056
  -1.000   0.2662   0.01428   0.00796  -0.0930   0.8309   0.7105
  -0.750   0.2838   0.01432   0.00800  -0.0908   0.8229   0.7126
  -0.500   0.3146   0.01422   0.00788  -0.0913   0.8178   0.7148
  -0.250   0.3526   0.01408   0.00772  -0.0932   0.8146   0.7175
   0.000   0.3724   0.01409   0.00771  -0.0916   0.8056   0.7218
   0.250   0.4146   0.01383   0.00738  -0.0946   0.7992   0.7269
   0.500   0.4350   0.01382   0.00739  -0.0929   0.7888   0.7291
   0.750   0.4727   0.01368   0.00722  -0.0946   0.7823   0.7312
   1.000   0.4938   0.01369   0.00724  -0.0933   0.7721   0.7338
   1.250   0.5300   0.01356   0.00709  -0.0950   0.7641   0.7361
   1.500   0.5578   0.01349   0.00700  -0.0951   0.7521   0.7389
   1.750   0.5894   0.01340   0.00686  -0.0961   0.7387   0.7422
   2.000   0.6182   0.01335   0.00679  -0.0962   0.7235   0.7444
   2.250   0.6450   0.01336   0.00678  -0.0958   0.7073   0.7466
   2.500   0.6727   0.01339   0.00677  -0.0957   0.6895   0.7490
   2.750   0.7017   0.01342   0.00675  -0.0960   0.6713   0.7513
   3.000   0.7296   0.01349   0.00674  -0.0961   0.6501   0.7539
   3.250   0.7559   0.01361   0.00674  -0.0959   0.6221   0.7567
   3.500   0.7811   0.01380   0.00677  -0.0956   0.5930   0.7594
   3.750   0.7991   0.01403   0.00689  -0.0937   0.5641   0.7611
   4.000   0.8168   0.01431   0.00706  -0.0918   0.5381   0.7629
   4.250   0.8345   0.01458   0.00725  -0.0899   0.5122   0.7648
   4.500   0.8511   0.01493   0.00747  -0.0880   0.4855   0.7668
   4.750   0.8686   0.01528   0.00772  -0.0863   0.4592   0.7690
   5.000   0.8863   0.01568   0.00801  -0.0848   0.4317   0.7713
   5.250   0.9046   0.01612   0.00833  -0.0835   0.4069   0.7736
   5.500   0.9235   0.01655   0.00868  -0.0823   0.3822   0.7759
   5.750   0.9384   0.01702   0.00907  -0.0802   0.3576   0.7777
   6.000   0.9528   0.01756   0.00950  -0.0781   0.3311   0.7797
   6.500   0.9840   0.01869   0.01043  -0.0747   0.2811   0.7838
   6.750   1.0016   0.01923   0.01091  -0.0735   0.2596   0.7862
   7.000   1.0189   0.01984   0.01142  -0.0723   0.2395   0.7887
   7.250   1.0372   0.02045   0.01195  -0.0713   0.2233   0.7910
   7.500   1.0558   0.02096   0.01247  -0.0703   0.2084   0.7928
   7.750   1.0726   0.02150   0.01302  -0.0689   0.1933   0.7945
   8.000   1.0893   0.02208   0.01360  -0.0676   0.1822   0.7966
   8.250   1.1066   0.02267   0.01421  -0.0664   0.1717   0.7988
   8.500   1.1237   0.02331   0.01486  -0.0653   0.1608   0.8010
   8.750   1.1420   0.02393   0.01550  -0.0644   0.1481   0.8031
   9.000   1.1594   0.02463   0.01620  -0.0635   0.1386   0.8053
   9.250   1.1765   0.02539   0.01697  -0.0626   0.1303   0.8074
   9.500   1.1924   0.02610   0.01773  -0.0614   0.1221   0.8092
   9.750   1.2079   0.02683   0.01853  -0.0602   0.1148   0.8110
  10.000   1.2232   0.02761   0.01937  -0.0590   0.1051   0.8131
  10.250   1.2366   0.02854   0.02033  -0.0577   0.0969   0.8155
  10.500   1.2495   0.02956   0.02136  -0.0564   0.0882   0.8181
  10.750   1.2621   0.03067   0.02248  -0.0552   0.0781   0.8206
  11.000   1.2749   0.03182   0.02364  -0.0542   0.0652   0.8230
  11.250   1.2840   0.03317   0.02498  -0.0527   0.0572   0.8249
  11.500   1.2928   0.03454   0.02640  -0.0512   0.0510   0.8269
  11.750   1.3039   0.03577   0.02775  -0.0500   0.0441   0.8292
  12.000   1.3114   0.03735   0.02937  -0.0487   0.0373   0.8315
  12.250   1.3183   0.03905   0.03110  -0.0475   0.0341   0.8340
  12.500   1.3248   0.04086   0.03298  -0.0464   0.0320   0.8365
  12.750   1.3302   0.04284   0.03505  -0.0454   0.0304   0.8392
  13.000   1.3337   0.04493   0.03725  -0.0443   0.0291   0.8416
  13.250   1.3387   0.04691   0.03940  -0.0433   0.0282   0.8443
  13.500   1.3425   0.04912   0.04177  -0.0425   0.0273   0.8472
  13.750   1.3452   0.05156   0.04436  -0.0419   0.0266   0.8502
  14.000   1.3468   0.05425   0.04719  -0.0415   0.0258   0.8531
  14.250   1.3468   0.05722   0.05029  -0.0413   0.0252   0.8559
  14.500   1.3443   0.06043   0.05365  -0.0411   0.0247   0.8584
  14.750   1.3401   0.06403   0.05737  -0.0412   0.0242   0.8612
  15.000   1.3407   0.06719   0.06072  -0.0415   0.0237   0.8643
  15.250   1.3397   0.07072   0.06441  -0.0421   0.0232   0.8677
  15.750   1.3354   0.07830   0.07231  -0.0438   0.0221   0.8746
  16.000   1.3316   0.08243   0.07660  -0.0449   0.0216   0.8785
  16.250   1.3273   0.08681   0.08113  -0.0464   0.0211   0.8826
  16.500   1.3223   0.09149   0.08596  -0.0481   0.0207   0.8866
  16.750   1.3157   0.09629   0.09091  -0.0499   0.0204   0.8908
  17.000   1.3083   0.10136   0.09613  -0.0519   0.0201   0.8955
  17.250   1.3008   0.10659   0.10149  -0.0542   0.0198   0.9005
  17.500   1.2940   0.11149   0.10656  -0.0562   0.0196   0.9068
  17.750   1.2870   0.11640   0.11163  -0.0582   0.0194   0.9153
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