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FX 62-K-153/20 AIRFOIL (fx62k153-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: FX 62-K-153/20 AIRFOIL (fx62k153-il)
Reynolds number: 100,000
Max Cl/Cd: 44.11 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx62k153-il-100000-n5.txt
Download as CSV file: xf-fx62k153-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 62-K-153/20 AIRFOIL                          
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.1125   0.10682   0.10187  -0.1001   0.9404   0.0276
 -11.750  -0.2410   0.11771   0.11264  -0.0884   0.9618   0.0283
 -11.500  -0.2290   0.11428   0.10919  -0.0896   0.9584   0.0273
 -11.250  -0.2209   0.11001   0.10490  -0.0923   0.9543   0.0264
 -11.000  -0.2136   0.10516   0.10005  -0.0958   0.9510   0.0256
 -10.750  -0.2072   0.09981   0.09471  -0.1000   0.9482   0.0248
 -10.500  -0.2053   0.09439   0.08930  -0.1037   0.9435   0.0241
 -10.000  -0.2256   0.07281   0.06767  -0.1215   0.9341   0.0214
  -9.750  -0.2349   0.06749   0.06228  -0.1257   0.9273   0.0213
  -9.500  -0.2444   0.06228   0.05693  -0.1301   0.9213   0.0211
  -9.250  -0.2579   0.05841   0.05292  -0.1320   0.9137   0.0210
  -9.000  -0.2704   0.05496   0.04928  -0.1331   0.9069   0.0210
  -8.750  -0.2798   0.05177   0.04584  -0.1337   0.9003   0.0210
  -8.500  -0.2848   0.04856   0.04232  -0.1335   0.8940   0.0210
  -8.250  -0.2795   0.04452   0.03770  -0.1348   0.8903   0.0215
  -8.000  -0.2820   0.04290   0.03598  -0.1322   0.8839   0.0221
  -7.750  -0.2672   0.04166   0.03467  -0.1323   0.8802   0.0235
  -7.500  -0.2479   0.03940   0.03205  -0.1332   0.8774   0.0251
  -7.250  -0.2247   0.03639   0.02851  -0.1343   0.8754   0.0263
  -7.000  -0.2224   0.03508   0.02691  -0.1308   0.8691   0.0270
  -6.750  -0.2007   0.03321   0.02457  -0.1305   0.8659   0.0290
  -6.500  -0.1751   0.03169   0.02297  -0.1313   0.8637   0.0314
  -6.250  -0.1466   0.03016   0.02121  -0.1318   0.8621   0.0332
  -6.000  -0.1172   0.02886   0.01967  -0.1322   0.8607   0.0357
  -5.750  -0.1128   0.02875   0.01943  -0.1283   0.8542   0.0377
  -5.500  -0.0909   0.02768   0.01838  -0.1277   0.8513   0.0404
  -5.250  -0.0647   0.02683   0.01751  -0.1277   0.8492   0.0433
  -5.000  -0.0359   0.02608   0.01666  -0.1282   0.8475   0.0478
  -4.750  -0.0050   0.02525   0.01581  -0.1294   0.8461   0.0547
  -4.500   0.0009   0.02533   0.01586  -0.1262   0.8393   0.0596
  -4.250   0.0282   0.02478   0.01529  -0.1270   0.8366   0.0725
  -4.000   0.0607   0.02403   0.01466  -0.1288   0.8345   0.1054
  -3.750   0.1033   0.02174   0.01426  -0.1347   0.8335   0.4669
  -3.500   0.1228   0.02246   0.01527  -0.1312   0.8316   0.5894
  -3.250   0.1321   0.02345   0.01618  -0.1280   0.8249   0.6271
  -2.750   0.1653   0.02538   0.01797  -0.1206   0.8186   0.6841
  -2.250   0.1875   0.02673   0.01917  -0.1134   0.8086   0.7105
  -2.000   0.2194   0.02672   0.01898  -0.1148   0.8061   0.7171
  -1.750   0.2516   0.02666   0.01876  -0.1158   0.8041   0.7219
  -1.500   0.2830   0.02658   0.01856  -0.1165   0.8025   0.7259
  -1.250   0.2920   0.02719   0.01911  -0.1144   0.7947   0.7316
  -1.000   0.3224   0.02720   0.01902  -0.1154   0.7916   0.7360
  -0.750   0.3527   0.02715   0.01887  -0.1160   0.7895   0.7392
  -0.250   0.3999   0.02768   0.01927  -0.1163   0.7797   0.7484
   0.000   0.4274   0.02770   0.01923  -0.1165   0.7765   0.7514
   0.250   0.4595   0.02758   0.01907  -0.1173   0.7743   0.7544
   0.500   0.4955   0.02743   0.01885  -0.1190   0.7728   0.7578
   1.000   0.5366   0.02816   0.01957  -0.1183   0.7607   0.7651
   1.250   0.5698   0.02797   0.01936  -0.1192   0.7588   0.7678
   1.750   0.6107   0.02868   0.02010  -0.1182   0.7465   0.7744
   2.000   0.6495   0.02844   0.01984  -0.1205   0.7445   0.7779
   2.250   0.6849   0.02809   0.01952  -0.1217   0.7429   0.7803
   2.500   0.6885   0.02905   0.02055  -0.1186   0.7318   0.7833
   2.750   0.7232   0.02873   0.02025  -0.1198   0.7298   0.7861
   3.250   0.7700   0.02955   0.02118  -0.1200   0.7171   0.7929
   3.500   0.8026   0.02918   0.02088  -0.1206   0.7150   0.7950
   4.000   0.8434   0.02997   0.02186  -0.1194   0.7018   0.8009
   4.250   0.8797   0.02955   0.02151  -0.1208   0.7001   0.8039
   4.500   0.8917   0.03068   0.02273  -0.1197   0.6887   0.8071
   4.750   0.9266   0.02992   0.02209  -0.1203   0.6863   0.8094
   5.000   0.9384   0.03057   0.02285  -0.1184   0.6747   0.8123
   5.250   0.9769   0.02952   0.02190  -0.1194   0.6717   0.8152
   5.500   0.9917   0.03012   0.02261  -0.1181   0.6598   0.8184
   6.000   1.0448   0.02978   0.02254  -0.1178   0.6445   0.8240
   6.500   1.0961   0.02943   0.02248  -0.1171   0.6288   0.8301
   6.750   1.1160   0.02964   0.02283  -0.1162   0.6158   0.8333
   7.000   1.1429   0.02929   0.02258  -0.1159   0.6010   0.8364
   7.250   1.1711   0.02855   0.02193  -0.1151   0.5842   0.8391
   7.500   1.1876   0.02883   0.02233  -0.1135   0.5634   0.8424
   7.750   1.2157   0.02834   0.02188  -0.1130   0.5411   0.8459
   8.000   1.2377   0.02843   0.02198  -0.1121   0.5135   0.8494
   8.250   1.2588   0.02854   0.02205  -0.1109   0.4823   0.8524
   8.500   1.2738   0.02904   0.02248  -0.1090   0.4489   0.8556
   8.750   1.2845   0.02991   0.02327  -0.1069   0.4117   0.8593
   9.000   1.2918   0.03114   0.02435  -0.1046   0.3728   0.8632
   9.250   1.2939   0.03272   0.02576  -0.1019   0.3294   0.8669
   9.500   1.2919   0.03458   0.02740  -0.0988   0.2898   0.8705
   9.750   1.2909   0.03658   0.02922  -0.0962   0.2516   0.8743
  10.000   1.2897   0.03873   0.03119  -0.0938   0.2168   0.8781
  10.250   1.2894   0.04079   0.03313  -0.0915   0.1844   0.8822
  10.500   1.2887   0.04290   0.03512  -0.0893   0.1578   0.8867
  10.750   1.2903   0.04497   0.03716  -0.0874   0.1374   0.8916
  11.000   1.2922   0.04700   0.03918  -0.0855   0.1214   0.8967
  11.250   1.2942   0.04902   0.04122  -0.0837   0.1083   0.9024
  11.750   1.2985   0.05317   0.04547  -0.0804   0.0887   0.9161
  12.000   1.3004   0.05523   0.04763  -0.0788   0.0812   0.9266
  12.250   1.3005   0.05727   0.04975  -0.0769   0.0753   0.9455
  12.500   1.3010   0.05938   0.05199  -0.0755   0.0694   0.9999
  12.750   1.3045   0.06207   0.05471  -0.0749   0.0642   0.9999
  13.000   1.3104   0.06453   0.05732  -0.0745   0.0590   0.9999
  13.250   1.3127   0.06737   0.06024  -0.0740   0.0554   0.9999
  13.500   1.3177   0.06995   0.06296  -0.0736   0.0511   0.9999
  13.750   1.3217   0.07275   0.06589  -0.0735   0.0463   0.9999
  14.000   1.3225   0.07593   0.06912  -0.0736   0.0420   0.9999
  14.250   1.3266   0.07885   0.07222  -0.0739   0.0370   0.9999
  14.500   1.3242   0.08253   0.07591  -0.0743   0.0335   0.9999
  14.750   1.3281   0.08554   0.07916  -0.0746   0.0293   0.9999
  15.000   1.3265   0.08925   0.08299  -0.0750   0.0268   0.9999
  15.250   1.3220   0.09336   0.08718  -0.0755   0.0249   0.9999
  15.500   1.3207   0.09712   0.09116  -0.0759   0.0226   0.9999
  15.750   1.3170   0.10131   0.09550  -0.0768   0.0207   0.9999
  16.000   1.3108   0.10597   0.10025  -0.0781   0.0193   0.9999
  16.250   1.3055   0.11049   0.10492  -0.0792   0.0180   0.9999
  16.500   1.3010   0.11511   0.10977  -0.0807   0.0163   0.9999
  16.750   1.2962   0.11983   0.11471  -0.0825   0.0155   0.9999
  17.000   1.2907   0.12484   0.11985  -0.0847   0.0148   0.9999
  17.250   1.2840   0.13021   0.12534  -0.0874   0.0141   0.9999
  17.500   1.2772   0.13557   0.13082  -0.0902   0.0137   0.9999
  17.750   1.2704   0.14119   0.13664  -0.0932   0.0132   0.9999
  18.000   1.2623   0.14737   0.14306  -0.0967   0.0128   0.9999
  18.250   1.2538   0.15385   0.14975  -0.1006   0.0125   0.9999
  18.500   1.2435   0.16109   0.15721  -0.1053   0.0122   0.9999
  18.750   1.2327   0.16879   0.16511  -0.1104   0.0122   0.9999
  19.000   1.2200   0.17748   0.17399  -0.1165   0.0122   0.9999
  19.250   1.2049   0.18755   0.18424  -0.1235   0.0123   0.9999
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