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FX 62-K-153/20 AIRFOIL (fx62k153-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: FX 62-K-153/20 AIRFOIL (fx62k153-il)
Reynolds number: 200,000
Max Cl/Cd: 77.46 at α=7.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx62k153-il-200000.txt
Download as CSV file: xf-fx62k153-il-200000.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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.500  -0.1632   0.09673   0.09316  -0.1093   0.9614   0.0443
 -10.250  -0.1590   0.09217   0.08861  -0.1133   0.9566   0.0462
 -10.000  -0.1611   0.08466   0.08111  -0.1237   0.9517   0.0486
  -9.750  -0.1686   0.07593   0.07229  -0.1367   0.9476   0.0491
  -9.500  -0.1837   0.07197   0.06823  -0.1404   0.9392   0.0492
  -9.250  -0.1941   0.06799   0.06408  -0.1455   0.9334   0.0493
  -9.000  -0.2095   0.06596   0.06192  -0.1455   0.9248   0.0494
  -8.750  -0.2065   0.05820   0.05426  -0.1473   0.9222   0.0510
  -8.500  -0.1903   0.05512   0.05119  -0.1488   0.9200   0.0526
  -8.250  -0.1953   0.05328   0.04929  -0.1474   0.9134   0.0537
  -8.000  -0.1939   0.05089   0.04675  -0.1474   0.9086   0.0557
  -7.500  -0.2069   0.04672   0.04186  -0.1450   0.8961   0.0640
  -7.250  -0.1863   0.04420   0.03951  -0.1455   0.8941   0.0680
  -7.000  -0.1681   0.03427   0.02828  -0.1453   0.8912   0.0354
  -6.750  -0.1738   0.03299   0.02677  -0.1402   0.8841   0.0344
  -6.500  -0.1548   0.03039   0.02377  -0.1394   0.8808   0.0341
  -6.250  -0.1225   0.02921   0.02218  -0.1406   0.8790   0.0375
  -6.000  -0.0906   0.02645   0.01908  -0.1416   0.8777   0.0393
  -5.750  -0.0579   0.02520   0.01783  -0.1431   0.8765   0.0435
  -5.500  -0.0627   0.02546   0.01805  -0.1376   0.8695   0.0444
  -5.250  -0.0390   0.02464   0.01712  -0.1369   0.8664   0.0464
  -5.000  -0.0072   0.02403   0.01638  -0.1377   0.8646   0.0494
  -4.750   0.0241   0.02263   0.01507  -0.1388   0.8633   0.0547
  -4.500   0.0609   0.02183   0.01422  -0.1409   0.8622   0.0614
  -4.250   0.1023   0.02065   0.01311  -0.1446   0.8612   0.0805
  -4.000   0.1644   0.01771   0.01240  -0.1551   0.8611   0.5747
  -3.750   0.1648   0.01900   0.01373  -0.1503   0.8530   0.6166
  -3.500   0.1864   0.01982   0.01449  -0.1480   0.8501   0.6484
  -3.250   0.2090   0.02058   0.01520  -0.1456   0.8481   0.6672
  -3.000   0.2339   0.02121   0.01576  -0.1435   0.8466   0.6814
  -2.750   0.2277   0.02254   0.01710  -0.1379   0.8372   0.6916
  -2.500   0.2446   0.02329   0.01782  -0.1342   0.8345   0.7062
  -2.250   0.2598   0.02402   0.01856  -0.1293   0.8326   0.7215
  -2.000   0.2442   0.02532   0.01991  -0.1214   0.8225   0.7293
  -1.750   0.2706   0.02544   0.01994  -0.1206   0.8202   0.7382
  -1.500   0.3064   0.02526   0.01967  -0.1219   0.8188   0.7430
  -1.250   0.3522   0.02495   0.01921  -0.1261   0.8179   0.7495
  -1.000   0.3422   0.02593   0.02023  -0.1198   0.8077   0.7530
  -0.750   0.3755   0.02577   0.02001  -0.1209   0.8056   0.7572
  -0.500   0.4214   0.02548   0.01962  -0.1249   0.8045   0.7626
  -0.250   0.4576   0.02515   0.01923  -0.1263   0.8033   0.7657
   0.000   0.4538   0.02611   0.02022  -0.1215   0.7931   0.7694
   0.250   0.4906   0.02588   0.01995  -0.1234   0.7911   0.7732
   0.500   0.5376   0.02552   0.01952  -0.1276   0.7899   0.7776
   0.750   0.5742   0.02507   0.01905  -0.1290   0.7887   0.7802
   1.000   0.6119   0.02460   0.01856  -0.1304   0.7877   0.7829
   1.250   0.6146   0.02548   0.01948  -0.1270   0.7766   0.7869
   1.500   0.6576   0.02504   0.01901  -0.1301   0.7753   0.7904
   1.750   0.7000   0.02461   0.01857  -0.1330   0.7741   0.7936
   2.000   0.7352   0.02420   0.01817  -0.1341   0.7729   0.7959
   2.250   0.7369   0.02516   0.01920  -0.1305   0.7620   0.7990
   2.500   0.7763   0.02472   0.01878  -0.1326   0.7605   0.8021
   2.750   0.8197   0.02427   0.01834  -0.1357   0.7593   0.8054
   3.000   0.8617   0.02385   0.01794  -0.1385   0.7581   0.8080
   3.250   0.8629   0.02473   0.01891  -0.1346   0.7474   0.8106
   3.500   0.9007   0.02419   0.01843  -0.1361   0.7457   0.8133
   3.750   0.9437   0.02343   0.01770  -0.1386   0.7442   0.8161
   4.000   0.9639   0.02354   0.01789  -0.1378   0.7348   0.8192
   4.250   1.0148   0.02233   0.01672  -0.1415   0.7319   0.8219
   4.500   1.0561   0.02133   0.01576  -0.1433   0.7295   0.8241
   4.750   1.0684   0.02163   0.01618  -0.1409   0.7204   0.8270
   5.000   1.1071   0.02098   0.01561  -0.1427   0.7169   0.8295
   5.250   1.1409   0.02048   0.01519  -0.1437   0.7109   0.8323
   5.500   1.1763   0.01977   0.01456  -0.1450   0.7027   0.8354
   5.750   1.2023   0.01921   0.01409  -0.1443   0.6925   0.8381
   6.000   1.2328   0.01841   0.01336  -0.1443   0.6821   0.8405
   6.250   1.2612   0.01782   0.01283  -0.1440   0.6702   0.8431
   6.500   1.2855   0.01754   0.01264  -0.1433   0.6565   0.8461
   6.750   1.3073   0.01747   0.01265  -0.1423   0.6406   0.8495
   7.000   1.3264   0.01744   0.01270  -0.1408   0.6234   0.8523
   7.250   1.3430   0.01741   0.01270  -0.1386   0.6032   0.8549
   7.500   1.3586   0.01754   0.01280  -0.1363   0.5766   0.8578
   7.750   1.3727   0.01792   0.01309  -0.1340   0.5430   0.8611
   8.000   1.3822   0.01864   0.01366  -0.1312   0.5035   0.8646
   8.250   1.3844   0.01959   0.01444  -0.1272   0.4641   0.8677
   8.500   1.3832   0.02082   0.01551  -0.1231   0.4235   0.8708
   8.750   1.3801   0.02239   0.01688  -0.1191   0.3808   0.8741
   9.000   1.3752   0.02430   0.01858  -0.1154   0.3328   0.8774
   9.500   1.3620   0.02860   0.02244  -0.1081   0.2485   0.8840
   9.750   1.3570   0.03085   0.02449  -0.1049   0.2093   0.8874
  10.000   1.3533   0.03320   0.02662  -0.1022   0.1707   0.8907
  10.250   1.3507   0.03561   0.02886  -0.0998   0.1423   0.8938
  10.500   1.3497   0.03771   0.03087  -0.0974   0.1215   0.8970
  10.750   1.3495   0.03984   0.03293  -0.0951   0.1061   0.9009
  11.000   1.3515   0.04193   0.03500  -0.0933   0.0930   0.9051
  11.250   1.3557   0.04391   0.03699  -0.0917   0.0818   0.9092
  11.500   1.3581   0.04589   0.03902  -0.0898   0.0733   0.9136
  11.750   1.3580   0.04825   0.04135  -0.0880   0.0665   0.9182
  12.000   1.3654   0.05001   0.04324  -0.0868   0.0605   0.9234
  12.250   1.3660   0.05219   0.04543  -0.0850   0.0556   0.9297
  12.500   1.3714   0.05399   0.04736  -0.0837   0.0507   0.9380
  12.750   1.3747   0.05574   0.04922  -0.0822   0.0460   0.9520
  13.000   1.3714   0.05803   0.05156  -0.0803   0.0426   0.9999
  13.250   1.3837   0.06004   0.05371  -0.0806   0.0370   0.9999
  13.500   1.3846   0.06314   0.05685  -0.0802   0.0325   0.9999
  13.750   1.3871   0.06622   0.05999  -0.0801   0.0264   0.9999
  14.000   1.3842   0.06984   0.06372  -0.0794   0.0220   0.9999
  14.250   1.3815   0.07348   0.06740  -0.0791   0.0196   0.9999
  14.500   1.3776   0.07717   0.07119  -0.0783   0.0179   0.9999
  14.750   1.3796   0.08033   0.07451  -0.0780   0.0165   0.9999
  15.000   1.3809   0.08352   0.07781  -0.0778   0.0156   0.9999
  15.250   1.3819   0.08677   0.08115  -0.0778   0.0148   0.9999
  15.500   1.3819   0.09008   0.08452  -0.0776   0.0142   0.9999
  15.750   1.3813   0.09323   0.08779  -0.0766   0.0135   0.9999
  16.000   1.3807   0.09700   0.09180  -0.0773   0.0130   0.9999
  16.250   1.3793   0.10086   0.09586  -0.0779   0.0125   0.9999
  16.500   1.3765   0.10493   0.10013  -0.0787   0.0120   0.9999
  16.750   1.3736   0.10909   0.10446  -0.0798   0.0117   0.9999
  17.000   1.3692   0.11356   0.10911  -0.0813   0.0113   0.9999
  17.250   1.3639   0.11828   0.11400  -0.0830   0.0110   0.9999
  17.500   1.3571   0.12332   0.11924  -0.0849   0.0109   0.9999
  17.750   1.3491   0.12871   0.12482  -0.0873   0.0108   0.9999
  18.000   1.3396   0.13459   0.13090  -0.0902   0.0107   0.9999
  18.250   1.3287   0.14097   0.13750  -0.0937   0.0107   0.9999
  18.500   1.3162   0.14800   0.14473  -0.0979   0.0107   0.9999
  18.750   1.2994   0.15644   0.15343  -0.1033   0.0108   0.9999
  19.000   1.2817   0.16563   0.16286  -0.1097   0.0109   0.9999
  19.250   1.2509   0.17960   0.17717  -0.1198   0.0114   0.9999
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