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FX 60-157 AIRFOIL (fx60157-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: FX 60-157 AIRFOIL (fx60157-il)
Reynolds number: 500,000
Max Cl/Cd: 81.15 at α=2.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx60157-il-500000.txt
Download as CSV file: xf-fx60157-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.7670   0.04987   0.04611  -0.0896   0.9930   0.0101
 -13.000  -0.7512   0.04893   0.04521  -0.0909   0.9906   0.0104
 -12.750  -0.7687   0.04326   0.03913  -0.0929   0.9871   0.0103
 -12.500  -0.7668   0.03978   0.03539  -0.0946   0.9848   0.0103
 -12.250  -0.7520   0.03792   0.03340  -0.0966   0.9832   0.0105
 -12.000  -0.7460   0.03581   0.03111  -0.0966   0.9798   0.0107
 -11.750  -0.7359   0.03424   0.02940  -0.0966   0.9757   0.0109
 -11.500  -0.7219   0.03227   0.02724  -0.0973   0.9732   0.0111
 -11.250  -0.7024   0.03073   0.02553  -0.0985   0.9714   0.0114
 -11.000  -0.6806   0.02902   0.02361  -0.0998   0.9701   0.0117
 -10.750  -0.6745   0.02803   0.02248  -0.0974   0.9643   0.0120
 -10.500  -0.6570   0.02691   0.02118  -0.0972   0.9611   0.0122
 -10.250  -0.6357   0.02555   0.01979  -0.0976   0.9592   0.0127
 -10.000  -0.6110   0.02457   0.01876  -0.0985   0.9576   0.0130
  -9.750  -0.5839   0.02367   0.01780  -0.0998   0.9564   0.0135
  -9.500  -0.5809   0.02316   0.01722  -0.0962   0.9495   0.0141
  -9.250  -0.5625   0.02238   0.01635  -0.0956   0.9461   0.0146
  -9.000  -0.5372   0.02164   0.01551  -0.0961   0.9441   0.0153
  -8.750  -0.5120   0.02043   0.01433  -0.0971   0.9425   0.0166
  -8.500  -0.4814   0.01954   0.01336  -0.0988   0.9415   0.0182
  -8.250  -0.4806   0.01903   0.01279  -0.0946   0.9335   0.0190
  -8.000  -0.4602   0.01805   0.01181  -0.0945   0.9305   0.0215
  -7.750  -0.4317   0.01731   0.01106  -0.0957   0.9289   0.0250
  -7.500  -0.3988   0.01684   0.01057  -0.0973   0.9280   0.0277
  -7.250  -0.3640   0.01649   0.01023  -0.0993   0.9272   0.0303
  -7.000  -0.3285   0.01615   0.00983  -0.1013   0.9266   0.0324
  -6.750  -0.2943   0.01556   0.00925  -0.1035   0.9259   0.0346
  -6.500  -0.2963   0.01547   0.00913  -0.0979   0.9172   0.0354
  -6.250  -0.2652   0.01508   0.00871  -0.0991   0.9154   0.0374
  -6.000  -0.2309   0.01455   0.00815  -0.1010   0.9141   0.0396
  -5.750  -0.1951   0.01398   0.00757  -0.1032   0.9131   0.0433
  -5.500  -0.1596   0.01344   0.00707  -0.1053   0.9119   0.0503
  -5.250  -0.1242   0.01293   0.00662  -0.1074   0.9109   0.0663
  -5.000  -0.0883   0.01224   0.00610  -0.1099   0.9098   0.1069
  -4.750  -0.0786   0.01178   0.00590  -0.1070   0.9024   0.1638
  -4.500  -0.0455   0.01064   0.00532  -0.1096   0.8999   0.3020
  -4.250  -0.0078   0.00981   0.00484  -0.1127   0.8981   0.4002
  -4.000   0.0321   0.00906   0.00445  -0.1160   0.8965   0.5026
  -3.750   0.0720   0.00865   0.00428  -0.1188   0.8949   0.5748
  -3.500   0.1072   0.00855   0.00424  -0.1203   0.8924   0.6094
  -3.250   0.1290   0.00859   0.00428  -0.1190   0.8866   0.6269
  -3.000   0.1603   0.00857   0.00425  -0.1197   0.8833   0.6406
  -2.750   0.1951   0.00854   0.00419  -0.1210   0.8805   0.6523
  -2.500   0.2315   0.00852   0.00412  -0.1227   0.8781   0.6636
  -2.250   0.2556   0.00865   0.00425  -0.1218   0.8725   0.6744
  -2.000   0.2839   0.00874   0.00434  -0.1216   0.8675   0.6831
  -1.750   0.3186   0.00876   0.00431  -0.1228   0.8635   0.6917
  -1.500   0.3459   0.00878   0.00433  -0.1225   0.8578   0.6963
  -1.250   0.3720   0.00885   0.00441  -0.1219   0.8517   0.7007
  -1.000   0.4042   0.00887   0.00439  -0.1226   0.8474   0.7058
  -0.750   0.4325   0.00888   0.00437  -0.1227   0.8411   0.7108
  -0.500   0.4578   0.00894   0.00446  -0.1219   0.8343   0.7143
  -0.250   0.4879   0.00900   0.00450  -0.1221   0.8285   0.7180
   0.000   0.5118   0.00903   0.00453  -0.1212   0.8195   0.7221
   0.250   0.5423   0.00898   0.00441  -0.1218   0.8103   0.7256
   0.500   0.5700   0.00891   0.00429  -0.1216   0.7985   0.7279
   0.750   0.5939   0.00889   0.00427  -0.1207   0.7853   0.7296
   1.000   0.6186   0.00892   0.00428  -0.1199   0.7712   0.7317
   1.250   0.6440   0.00897   0.00431  -0.1194   0.7583   0.7341
   1.500   0.6698   0.00903   0.00433  -0.1189   0.7446   0.7370
   1.750   0.6957   0.00909   0.00433  -0.1186   0.7284   0.7402
   2.000   0.7213   0.00918   0.00433  -0.1182   0.7079   0.7431
   2.250   0.7430   0.00927   0.00434  -0.1169   0.6850   0.7448
   2.500   0.7634   0.00943   0.00440  -0.1153   0.6586   0.7465
   2.750   0.7823   0.00964   0.00451  -0.1135   0.6295   0.7485
   3.000   0.7981   0.00994   0.00465  -0.1111   0.5942   0.7508
   3.250   0.8135   0.01026   0.00480  -0.1087   0.5583   0.7533
   3.500   0.8270   0.01061   0.00496  -0.1059   0.5224   0.7560
   3.750   0.8421   0.01100   0.00516  -0.1037   0.4865   0.7584
   4.000   0.8585   0.01132   0.00534  -0.1017   0.4550   0.7602
   4.250   0.8751   0.01167   0.00556  -0.0997   0.4238   0.7618
   4.500   0.8930   0.01203   0.00583  -0.0980   0.3983   0.7635
   5.000   0.9304   0.01278   0.00638  -0.0950   0.3476   0.7674
   5.250   0.9504   0.01316   0.00666  -0.0939   0.3248   0.7694
   5.500   0.9704   0.01356   0.00696  -0.0928   0.3016   0.7713
   5.750   0.9912   0.01394   0.00726  -0.0919   0.2831   0.7733
   6.000   1.0119   0.01436   0.00758  -0.0910   0.2614   0.7751
   6.500   1.0497   0.01519   0.00827  -0.0885   0.2251   0.7785
   6.750   1.0684   0.01562   0.00865  -0.0872   0.2067   0.7804
   7.000   1.0871   0.01609   0.00905  -0.0859   0.1884   0.7824
   7.250   1.1060   0.01656   0.00947  -0.0848   0.1759   0.7847
   7.500   1.1258   0.01700   0.00988  -0.0838   0.1641   0.7870
   7.750   1.1456   0.01747   0.01031  -0.0828   0.1488   0.7891
   8.000   1.1644   0.01803   0.01080  -0.0818   0.1361   0.7911
   8.250   1.1835   0.01849   0.01126  -0.0808   0.1265   0.7929
   8.500   1.2010   0.01902   0.01178  -0.0795   0.1179   0.7947
   9.000   1.2353   0.02018   0.01291  -0.0770   0.0959   0.7982
   9.250   1.2518   0.02082   0.01355  -0.0756   0.0869   0.8004
   9.500   1.2683   0.02150   0.01423  -0.0744   0.0786   0.8025
   9.750   1.2824   0.02237   0.01502  -0.0729   0.0625   0.8045
  10.000   1.2960   0.02331   0.01591  -0.0714   0.0528   0.8064
  10.250   1.3107   0.02417   0.01678  -0.0701   0.0415   0.8081
  10.500   1.3197   0.02537   0.01791  -0.0681   0.0328   0.8098
  10.750   1.3304   0.02647   0.01903  -0.0664   0.0292   0.8116
  11.000   1.3439   0.02739   0.02005  -0.0650   0.0273   0.8135
  11.250   1.3555   0.02848   0.02121  -0.0635   0.0257   0.8155
  11.500   1.3650   0.02976   0.02256  -0.0618   0.0244   0.8175
  11.750   1.3775   0.03084   0.02372  -0.0606   0.0237   0.8198
  12.000   1.3905   0.03192   0.02487  -0.0595   0.0228   0.8221
  12.250   1.4027   0.03307   0.02610  -0.0584   0.0219   0.8242
  12.500   1.4135   0.03429   0.02740  -0.0572   0.0210   0.8263
  12.750   1.4224   0.03570   0.02887  -0.0560   0.0203   0.8283
  13.000   1.4295   0.03731   0.03057  -0.0547   0.0198   0.8305
  13.250   1.4389   0.03879   0.03214  -0.0537   0.0194   0.8328
  13.500   1.4471   0.04043   0.03387  -0.0527   0.0190   0.8353
  13.750   1.4547   0.04220   0.03574  -0.0519   0.0187   0.8376
  14.000   1.4617   0.04409   0.03771  -0.0511   0.0183   0.8399
  14.250   1.4674   0.04607   0.03981  -0.0504   0.0180   0.8422
  14.500   1.4721   0.04823   0.04207  -0.0497   0.0177   0.8447
  14.750   1.4757   0.05060   0.04453  -0.0492   0.0174   0.8473
  15.000   1.4782   0.05320   0.04723  -0.0488   0.0171   0.8501
  15.250   1.4787   0.05616   0.05029  -0.0486   0.0169   0.8530
  15.500   1.4774   0.05949   0.05373  -0.0487   0.0166   0.8557
  15.750   1.4736   0.06314   0.05752  -0.0489   0.0164   0.8584
  16.000   1.4721   0.06665   0.06117  -0.0493   0.0163   0.8613
  16.250   1.4705   0.07033   0.06498  -0.0500   0.0161   0.8643
  16.500   1.4682   0.07428   0.06906  -0.0509   0.0160   0.8673
  16.750   1.4657   0.07842   0.07333  -0.0522   0.0157   0.8702
  17.000   1.4619   0.08277   0.07782  -0.0535   0.0155   0.8731
  17.250   1.4572   0.08735   0.08253  -0.0551   0.0152   0.8761
  17.500   1.4514   0.09225   0.08758  -0.0570   0.0150   0.8792
  17.750   1.4445   0.09746   0.09292  -0.0592   0.0148   0.8826
  18.000   1.4369   0.10294   0.09852  -0.0616   0.0146   0.8860
  18.250   1.4284   0.10853   0.10425  -0.0642   0.0144   0.8893
  18.500   1.4186   0.11441   0.11026  -0.0670   0.0142   0.8931
  18.750   1.4091   0.12032   0.11629  -0.0700   0.0140   0.8973
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