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WORTMANN FX 3 AIRFOIL (fx3-il) Xfoil prediction polar at RE=500,000 Ncrit=0


Details Polar file
Airfoil: WORTMANN FX 3 AIRFOIL (fx3-il)
Reynolds number: 500,000
Max Cl/Cd: 40.93 at α=7.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx3-il-500000.txt
Download as CSV file: xf-fx3-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 3 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
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -0.4499   0.11374   0.11061  -0.1246   0.8401   0.0147
 -17.500  -0.4948   0.09957   0.09624  -0.1325   0.8405   0.0144
 -17.250  -0.5371   0.08763   0.08408  -0.1394   0.8410   0.0142
 -17.000  -0.5638   0.07949   0.07575  -0.1442   0.8414   0.0141
 -16.750  -0.5825   0.07319   0.06927  -0.1477   0.8419   0.0141
 -16.500  -0.5963   0.06807   0.06398  -0.1504   0.8424   0.0142
 -16.250  -0.6059   0.06384   0.05958  -0.1524   0.8429   0.0143
 -16.000  -0.6122   0.06027   0.05585  -0.1539   0.8434   0.0144
 -15.750  -0.6191   0.05689   0.05230  -0.1549   0.8439   0.0145
 -15.500  -0.6331   0.05287   0.04805  -0.1551   0.8445   0.0147
 -15.250  -0.6376   0.05004   0.04507  -0.1552   0.8451   0.0150
 -15.000  -0.6357   0.04800   0.04292  -0.1552   0.8457   0.0153
 -14.750  -0.6307   0.04635   0.04120  -0.1551   0.8462   0.0156
 -14.500  -0.6238   0.04491   0.03968  -0.1551   0.8464   0.0159
 -14.250  -0.6161   0.04361   0.03830  -0.1549   0.8467   0.0163
 -14.000  -0.6074   0.04250   0.03710  -0.1546   0.8473   0.0167
 -13.750  -0.5984   0.04154   0.03602  -0.1541   0.8478   0.0171
 -13.500  -0.5895   0.04095   0.03533  -0.1533   0.8487   0.0176
 -13.250  -0.5749   0.03967   0.03395  -0.1534   0.8493   0.0181
 -13.000  -0.5542   0.03947   0.03376  -0.1570   0.8571   0.0186
 -12.750  -0.5478   0.03874   0.03296  -0.1557   0.8603   0.0195
 -12.500  -0.5387   0.03838   0.03257  -0.1544   0.8622   0.0203
 -11.500  -0.7522   0.04425   0.03849  -0.1028   0.8738   0.0185
 -11.250  -0.7527   0.04324   0.03739  -0.0992   0.8710   0.0191
 -11.000  -0.7477   0.04236   0.03647  -0.0967   0.8694   0.0200
 -10.750  -0.7379   0.04179   0.03587  -0.0950   0.8683   0.0207
 -10.500  -0.7258   0.04132   0.03536  -0.0936   0.8675   0.0216
 -10.250  -0.7117   0.04088   0.03486  -0.0925   0.8668   0.0226
 -10.000  -0.6953   0.04052   0.03440  -0.0917   0.8661   0.0235
  -9.750  -0.6822   0.04000   0.03382  -0.0904   0.8656   0.0248
  -9.500  -0.7416   0.03969   0.03348  -0.0755   0.8563   0.0238
  -9.250  -0.7418   0.03887   0.03263  -0.0717   0.8544   0.0250
  -9.000  -0.7356   0.03836   0.03212  -0.0691   0.8530   0.0265
  -8.750  -0.7244   0.03808   0.03180  -0.0671   0.8520   0.0281
  -8.500  -0.7138   0.03786   0.03153  -0.0650   0.8512   0.0298
  -8.250  -0.7011   0.03749   0.03112  -0.0635   0.8506   0.0320
  -8.000  -0.6808   0.03739   0.03105  -0.0633   0.8502   0.0348
  -7.750  -0.7308   0.03616   0.02979  -0.0510   0.8412   0.0339
  -7.500  -0.7107   0.03592   0.02952  -0.0508   0.8398   0.0369
  -7.250  -0.6894   0.03551   0.02908  -0.0509   0.8386   0.0403
  -7.000  -0.6632   0.03542   0.02901  -0.0518   0.8377   0.0442
  -6.750  -0.6349   0.03553   0.02906  -0.0528   0.8370   0.0472
  -6.500  -0.6090   0.03509   0.02867  -0.0539   0.8365   0.0517
  -6.250  -0.5789   0.03518   0.02874  -0.0554   0.8360   0.0553
  -6.000  -0.5476   0.03540   0.02891  -0.0570   0.8355   0.0576
  -5.750  -0.5174   0.03503   0.02856  -0.0591   0.8352   0.0625
  -5.500  -0.5358   0.03418   0.02771  -0.0528   0.8269   0.0632
  -5.250  -0.5068   0.03406   0.02757  -0.0543   0.8252   0.0666
  -5.000  -0.4759   0.03405   0.02752  -0.0559   0.8240   0.0694
  -4.750  -0.4419   0.03382   0.02726  -0.0585   0.8232   0.0735
  -4.500  -0.4072   0.03372   0.02719  -0.0612   0.8225   0.0792
  -4.250  -0.3725   0.03379   0.02723  -0.0636   0.8219   0.0839
  -4.000  -0.3348   0.03377   0.02722  -0.0668   0.8214   0.0916
  -3.750  -0.2960   0.03382   0.02732  -0.0702   0.8210   0.1050
  -3.500  -0.2215   0.03301   0.02918  -0.0845   0.8212   0.5999
  -3.000  -0.1891   0.03391   0.02989  -0.0825   0.8111   0.6603
  -2.750  -0.1689   0.03494   0.03091  -0.0799   0.8090   0.6690
  -2.500  -0.1056   0.03889   0.03483  -0.0835   0.8191   0.6800
  -2.000  -0.1269   0.03716   0.03317  -0.0687   0.7962   0.6835
  -1.750  -0.0835   0.03758   0.03347  -0.0727   0.7948   0.6926
  -1.500  -0.0612   0.03794   0.03385  -0.0700   0.7936   0.6940
  -1.250  -0.0526   0.03774   0.03366  -0.0653   0.7839   0.6957
  -1.000  -0.0323   0.03810   0.03402  -0.0625   0.7821   0.6983
  -0.750   0.0071   0.03842   0.03427  -0.0654   0.7812   0.7078
  -0.500   0.0265   0.03866   0.03453  -0.0622   0.7804   0.7095
  -0.250   0.0438   0.03916   0.03506  -0.0579   0.7797   0.7132
   0.000   0.0523   0.03911   0.03499  -0.0553   0.7701   0.7236
   0.250   0.0680   0.03919   0.03510  -0.0513   0.7690   0.7263
   0.500   0.0968   0.03915   0.03504  -0.0512   0.7683   0.7288
   0.750   0.1334   0.03906   0.03492  -0.0535   0.7678   0.7318
   1.000   0.1410   0.03962   0.03553  -0.0461   0.7672   0.7473
   1.250   0.1542   0.04067   0.03658  -0.0447   0.7577   0.7686
   1.500   0.1762   0.03973   0.03564  -0.0432   0.7569   0.7696
   1.750   0.1920   0.03919   0.03510  -0.0408   0.7535   0.7708
   2.000   0.2260   0.03868   0.03459  -0.0416   0.7549   0.7720
   2.250   0.2321   0.03838   0.03431  -0.0382   0.7467   0.7742
   2.500   0.2858   0.03902   0.03492  -0.0452   0.7461   0.7853
   2.750   0.3102   0.03812   0.03404  -0.0444   0.7453   0.7862
   3.000   0.3370   0.03743   0.03336  -0.0441   0.7446   0.7873
   3.250   0.3652   0.03684   0.03278  -0.0440   0.7441   0.7886
   3.500   0.3697   0.03670   0.03267  -0.0404   0.7349   0.7909
   3.750   0.4015   0.03626   0.03225  -0.0415   0.7339   0.7933
   4.000   0.4483   0.03633   0.03234  -0.0466   0.7333   0.8025
   4.250   0.4554   0.03599   0.03203  -0.0433   0.7256   0.8038
   4.500   0.4810   0.03541   0.03148  -0.0430   0.7234   0.8051
   4.750   0.5096   0.03484   0.03094  -0.0433   0.7221   0.8069
   5.000   0.5413   0.03429   0.03044  -0.0442   0.7211   0.8094
   5.250   0.5883   0.03421   0.03038  -0.0491   0.7203   0.8184
   5.500   0.6171   0.03325   0.02947  -0.0491   0.7195   0.8194
   5.750   0.6247   0.03316   0.02943  -0.0461   0.7093   0.8210
   6.000   0.6572   0.03229   0.02861  -0.0469   0.7077   0.8226
   7.000   0.9027   0.03004   0.02644  -0.0845   0.6712   0.7649
   7.250   0.9564   0.02811   0.02448  -0.0888   0.6546   0.7637
   7.500   1.0177   0.02567   0.02183  -0.0940   0.6193   0.7624
   7.750   1.0465   0.02557   0.02140  -0.0955   0.5670   0.7584
   8.000   1.0676   0.02713   0.02251  -0.0981   0.5009   0.7509
   8.250   1.0671   0.02847   0.02360  -0.0945   0.4514   0.7502
   8.500   1.0683   0.02985   0.02469  -0.0914   0.3984   0.7495
   8.750   1.0703   0.03129   0.02580  -0.0886   0.3385   0.7487
   9.000   1.0730   0.03278   0.02692  -0.0860   0.2749   0.7480
   9.250   1.0770   0.03425   0.02802  -0.0837   0.2126   0.7473
   9.500   1.0848   0.03557   0.02903  -0.0819   0.1627   0.7465
  10.000   1.1125   0.03761   0.03078  -0.0802   0.1090   0.7457
  10.250   1.1278   0.03855   0.03164  -0.0795   0.0919   0.7454
  10.500   1.1439   0.03950   0.03251  -0.0790   0.0767   0.7447
  10.750   1.1585   0.04059   0.03351  -0.0784   0.0592   0.7439
  11.000   1.1688   0.04201   0.03474  -0.0772   0.0372   0.7432
  11.250   1.1817   0.04330   0.03597  -0.0764   0.0292   0.7425
  11.500   1.1961   0.04449   0.03719  -0.0757   0.0257   0.7418
  11.750   1.2107   0.04568   0.03842  -0.0752   0.0237   0.7412
  12.000   1.2213   0.04721   0.03996  -0.0741   0.0218   0.7406
  12.250   1.2302   0.04889   0.04171  -0.0729   0.0205   0.7401
  12.500   1.2442   0.05018   0.04307  -0.0723   0.0196   0.7397
  12.750   1.2561   0.05162   0.04457  -0.0716   0.0187   0.7392
  13.000   1.2664   0.05317   0.04619  -0.0706   0.0179   0.7389
  13.250   1.2748   0.05489   0.04795  -0.0695   0.0171   0.7385
  13.500   1.2779   0.05709   0.05021  -0.0679   0.0164   0.7382
  13.750   1.2780   0.05956   0.05277  -0.0660   0.0158   0.7379
  14.000   1.2882   0.06120   0.05449  -0.0652   0.0155   0.7376
  14.250   1.2969   0.06297   0.05634  -0.0642   0.0151   0.7373
  14.500   1.3043   0.06484   0.05830  -0.0632   0.0147   0.7371
  14.750   1.3110   0.06680   0.06034  -0.0622   0.0143   0.7369
  15.000   1.3180   0.06876   0.06239  -0.0614   0.0139   0.7367
  15.250   1.3243   0.07086   0.06456  -0.0606   0.0135   0.7366
  15.500   1.3302   0.07300   0.06676  -0.0599   0.0131   0.7366
  15.750   1.3344   0.07533   0.06914  -0.0592   0.0128   0.7366
  16.000   1.3357   0.07778   0.07166  -0.0580   0.0124   0.7365
  16.250   1.3391   0.08011   0.07410  -0.0570   0.0121   0.7364
  16.500   1.3444   0.08250   0.07662  -0.0566   0.0119   0.7363
  16.750   1.3489   0.08500   0.07924  -0.0563   0.0117   0.7362
  17.000   1.3526   0.08759   0.08197  -0.0561   0.0116   0.7360
  17.250   1.3553   0.09033   0.08484  -0.0558   0.0114   0.7359
  17.500   1.3572   0.09318   0.08781  -0.0557   0.0112   0.7358
  17.750   1.3581   0.09620   0.09097  -0.0558   0.0110   0.7356
  18.000   1.3582   0.09935   0.09424  -0.0559   0.0108   0.7355
  18.250   1.3579   0.10262   0.09763  -0.0563   0.0107   0.7354
  18.500   1.3567   0.10605   0.10119  -0.0568   0.0105   0.7352
  18.750   1.3546   0.10970   0.10497  -0.0576   0.0104   0.7351
  19.000   1.3515   0.11356   0.10896  -0.0587   0.0103   0.7350
  19.250   1.3483   0.11752   0.11305  -0.0600   0.0101   0.7349
  19.500   1.3438   0.12172   0.11738  -0.0615   0.0100   0.7347
  19.750   1.3407   0.12576   0.12151  -0.0633   0.0099   0.7346
  20.000   1.3352   0.13025   0.12613  -0.0652   0.0098   0.7345
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