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FX 74-130 WP1 (fx74130wp1-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: FX 74-130 WP1 (fx74130wp1-il)
Reynolds number: 500,000
Max Cl/Cd: 115.85 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx74130wp1-il-500000-n5.txt
Download as CSV file: xf-fx74130wp1-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 74-130 WP1                                   
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.250  -0.1271   0.08430   0.08083  -0.1184   0.8158   0.0107
 -10.000  -0.1291   0.07931   0.07587  -0.1206   0.8145   0.0090
  -9.750  -0.1279   0.07587   0.07244  -0.1222   0.8130   0.0088
  -9.500  -0.1300   0.07175   0.06837  -0.1241   0.8114   0.0084
  -9.250  -0.1340   0.06728   0.06392  -0.1266   0.8097   0.0082
  -9.000  -0.1415   0.06220   0.05889  -0.1304   0.8077   0.0080
  -8.750  -0.1563   0.05690   0.05356  -0.1340   0.8056   0.0077
  -8.500  -0.1760   0.05282   0.04942  -0.1338   0.8036   0.0075
  -8.000  -0.2246   0.03816   0.03425  -0.1300   0.7993   0.0067
  -7.750  -0.2312   0.03230   0.02802  -0.1273   0.7975   0.0066
  -7.500  -0.2263   0.02864   0.02404  -0.1254   0.7960   0.0068
  -7.250  -0.2160   0.02553   0.02058  -0.1238   0.7945   0.0069
  -7.000  -0.1983   0.02389   0.01870  -0.1230   0.7931   0.0072
  -6.750  -0.1806   0.02171   0.01619  -0.1220   0.7918   0.0073
  -6.500  -0.1599   0.02002   0.01422  -0.1213   0.7906   0.0076
  -6.250  -0.1374   0.01855   0.01245  -0.1207   0.7896   0.0079
  -6.000  -0.1137   0.01727   0.01093  -0.1203   0.7886   0.0081
  -5.750  -0.0895   0.01632   0.00982  -0.1199   0.7875   0.0085
  -5.500  -0.0642   0.01576   0.00914  -0.1197   0.7863   0.0091
  -5.250  -0.0392   0.01505   0.00831  -0.1194   0.7849   0.0093
  -5.000  -0.0145   0.01431   0.00746  -0.1191   0.7835   0.0094
  -4.750   0.0097   0.01352   0.00659  -0.1187   0.7820   0.0096
  -4.500   0.0337   0.01278   0.00580  -0.1183   0.7806   0.0101
  -4.250   0.0591   0.01233   0.00531  -0.1182   0.7793   0.0106
  -4.000   0.0851   0.01197   0.00491  -0.1181   0.7781   0.0114
  -3.750   0.1115   0.01164   0.00453  -0.1181   0.7770   0.0124
  -3.500   0.1384   0.01137   0.00421  -0.1182   0.7759   0.0134
  -3.250   0.1652   0.01107   0.00387  -0.1183   0.7748   0.0153
  -3.000   0.1921   0.01090   0.00370  -0.1184   0.7735   0.0185
  -2.750   0.2185   0.01068   0.00349  -0.1184   0.7719   0.0241
  -2.500   0.2451   0.01046   0.00333  -0.1185   0.7702   0.0396
  -2.250   0.2716   0.01016   0.00320  -0.1187   0.7687   0.0881
  -2.000   0.2979   0.00975   0.00308  -0.1190   0.7672   0.1790
  -1.750   0.3232   0.00882   0.00293  -0.1196   0.7657   0.4213
  -1.500   0.3461   0.00795   0.00316  -0.1192   0.7642   0.7329
  -1.250   0.3743   0.00813   0.00331  -0.1192   0.7629   0.7766
  -1.000   0.4014   0.00834   0.00350  -0.1189   0.7616   0.7968
  -0.750   0.4283   0.00853   0.00366  -0.1186   0.7604   0.8098
  -0.500   0.4547   0.00868   0.00380  -0.1183   0.7588   0.8184
  -0.250   0.4809   0.00876   0.00389  -0.1181   0.7569   0.8234
   0.000   0.5075   0.00882   0.00396  -0.1179   0.7550   0.8272
   0.250   0.5355   0.00885   0.00397  -0.1182   0.7531   0.8300
   0.500   0.5643   0.00886   0.00395  -0.1186   0.7513   0.8320
   0.750   0.5936   0.00887   0.00393  -0.1192   0.7498   0.8336
   1.000   0.6229   0.00887   0.00391  -0.1198   0.7484   0.8347
   1.250   0.6516   0.00886   0.00389  -0.1202   0.7470   0.8356
   1.500   0.6791   0.00889   0.00395  -0.1204   0.7451   0.8366
   1.750   0.7060   0.00891   0.00401  -0.1205   0.7425   0.8375
   2.000   0.7335   0.00891   0.00403  -0.1207   0.7393   0.8385
   2.250   0.7617   0.00887   0.00400  -0.1210   0.7362   0.8394
   2.500   0.7906   0.00883   0.00397  -0.1215   0.7337   0.8401
   2.750   0.8178   0.00884   0.00402  -0.1216   0.7301   0.8410
   3.000   0.8446   0.00883   0.00405  -0.1216   0.7252   0.8420
   3.250   0.8728   0.00876   0.00400  -0.1219   0.7204   0.8428
   3.500   0.8992   0.00874   0.00404  -0.1219   0.7137   0.8436
   3.750   0.9266   0.00868   0.00398  -0.1220   0.7064   0.8443
   4.000   0.9525   0.00867   0.00401  -0.1218   0.6962   0.8451
   4.250   0.9782   0.00865   0.00400  -0.1215   0.6828   0.8460
   4.500   1.0026   0.00869   0.00398  -0.1210   0.6647   0.8470
   4.750   1.0241   0.00884   0.00404  -0.1199   0.6370   0.8478
   5.000   1.0383   0.00922   0.00420  -0.1173   0.5842   0.8487
   5.250   1.0330   0.01018   0.00471  -0.1110   0.4990   0.8499
   5.500   1.0239   0.01114   0.00534  -0.1042   0.4336   0.8514
   5.750   1.0181   0.01211   0.00606  -0.0983   0.3787   0.8529
   6.000   1.0168   0.01310   0.00683  -0.0936   0.3292   0.8546
   6.250   1.0166   0.01419   0.00769  -0.0894   0.2796   0.8563
   6.500   1.0205   0.01525   0.00854  -0.0861   0.2343   0.8576
   6.750   1.0244   0.01640   0.00945  -0.0830   0.1857   0.8588
   7.000   1.0321   0.01744   0.01030  -0.0805   0.1471   0.8599
   7.250   1.0420   0.01840   0.01111  -0.0784   0.1156   0.8610
   7.500   1.0527   0.01935   0.01195  -0.0765   0.0880   0.8620
   8.000   1.0769   0.02115   0.01357  -0.0731   0.0487   0.8638
   8.250   1.0908   0.02196   0.01435  -0.0716   0.0387   0.8647
   8.500   1.1058   0.02270   0.01511  -0.0704   0.0321   0.8656
   8.750   1.1207   0.02348   0.01591  -0.0691   0.0277   0.8667
   9.000   1.1358   0.02425   0.01673  -0.0679   0.0245   0.8679
   9.250   1.1496   0.02514   0.01764  -0.0666   0.0216   0.8692
   9.500   1.1644   0.02596   0.01853  -0.0654   0.0202   0.8703
   9.750   1.1798   0.02677   0.01940  -0.0644   0.0188   0.8714
  10.000   1.1945   0.02763   0.02031  -0.0633   0.0171   0.8725
  10.250   1.2072   0.02867   0.02137  -0.0620   0.0155   0.8737
  10.500   1.2205   0.02967   0.02246  -0.0609   0.0143   0.8748
  10.750   1.2355   0.03056   0.02342  -0.0599   0.0133   0.8760
  11.250   1.2619   0.03261   0.02562  -0.0578   0.0115   0.8783
  11.500   1.2731   0.03382   0.02688  -0.0565   0.0106   0.8796
  11.750   1.2837   0.03512   0.02826  -0.0553   0.0098   0.8811
  12.000   1.2966   0.03623   0.02947  -0.0544   0.0092   0.8826
  12.250   1.3094   0.03736   0.03068  -0.0535   0.0083   0.8843
  12.500   1.3213   0.03861   0.03200  -0.0525   0.0076   0.8861
  12.750   1.3309   0.04010   0.03356  -0.0515   0.0070   0.8880
  13.000   1.3397   0.04170   0.03527  -0.0504   0.0066   0.8899
  13.250   1.3490   0.04327   0.03695  -0.0494   0.0063   0.8919
  13.500   1.3576   0.04491   0.03872  -0.0485   0.0059   0.8944
  13.750   1.3662   0.04658   0.04049  -0.0476   0.0055   0.8974
  14.000   1.3735   0.04840   0.04242  -0.0466   0.0053   0.9010
  14.500   1.3856   0.05237   0.04662  -0.0449   0.0048   0.9105
  14.750   1.3876   0.05484   0.04922  -0.0439   0.0046   0.9175
  15.000   1.3878   0.05730   0.05186  -0.0427   0.0045   0.9318
  15.250   1.3884   0.05972   0.05445  -0.0417   0.0044   1.0000
  15.500   1.3911   0.06250   0.05738  -0.0414   0.0042   1.0000
  15.750   1.3926   0.06550   0.06053  -0.0412   0.0041   1.0000
  16.000   1.3936   0.06862   0.06380  -0.0411   0.0040   1.0000
  16.250   1.3923   0.07214   0.06747  -0.0412   0.0039   1.0000
  16.500   1.3902   0.07586   0.07135  -0.0415   0.0038   1.0000
  16.750   1.3870   0.07986   0.07551  -0.0421   0.0038   1.0000
  17.000   1.3831   0.08409   0.07990  -0.0429   0.0037   1.0000
  17.250   1.3775   0.08868   0.08465  -0.0439   0.0036   1.0000
  17.500   1.3706   0.09363   0.08977  -0.0453   0.0035   1.0000
  17.750   1.3630   0.09888   0.09518  -0.0471   0.0035   1.0000
  18.000   1.3544   0.10445   0.10092  -0.0493   0.0034   1.0000
  18.250   1.3451   0.11032   0.10696  -0.0518   0.0034   1.0000
  18.500   1.3343   0.11665   0.11345  -0.0548   0.0034   1.0000
  18.750   1.3226   0.12336   0.12033  -0.0583   0.0033   1.0000
  19.000   1.3094   0.13059   0.12773  -0.0623   0.0033   1.0000
  19.250   1.2953   0.13827   0.13558  -0.0668   0.0033   1.0000
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