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FX 74-130 WP1 (fx74130wp1-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: FX 74-130 WP1 (fx74130wp1-il)
Reynolds number: 1,000,000
Max Cl/Cd: 152.61 at α=4.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx74130wp1-il-1000000.txt
Download as CSV file: xf-fx74130wp1-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.0841   0.08328   0.08076  -0.1097   0.8182   0.0097
 -11.000  -0.0811   0.07981   0.07728  -0.1109   0.8170   0.0099
 -10.750  -0.0789   0.07606   0.07354  -0.1123   0.8163   0.0099
 -10.500  -0.0758   0.07277   0.07026  -0.1133   0.8155   0.0101
 -10.250  -0.0743   0.06909   0.06658  -0.1146   0.8147   0.0102
 -10.000  -0.0740   0.06514   0.06264  -0.1161   0.8138   0.0102
  -9.750  -0.0738   0.06137   0.05889  -0.1175   0.8128   0.0103
  -9.500  -0.0743   0.05755   0.05508  -0.1189   0.8118   0.0104
  -9.250  -0.0772   0.05334   0.05089  -0.1207   0.8107   0.0106
  -9.000  -0.0827   0.04874   0.04631  -0.1230   0.8094   0.0106
  -8.750  -0.0995   0.04221   0.03979  -0.1286   0.8079   0.0104
  -8.500  -0.1228   0.03683   0.03435  -0.1314   0.8062   0.0103
  -8.250  -0.1442   0.03350   0.03097  -0.1303   0.8044   0.0103
  -8.000  -0.1542   0.03048   0.02785  -0.1290   0.8025   0.0104
  -7.750  -0.1572   0.02736   0.02465  -0.1279   0.8015   0.0105
  -7.500  -0.1563   0.02437   0.02155  -0.1268   0.8002   0.0107
  -7.250  -0.1527   0.02131   0.01835  -0.1255   0.7987   0.0109
  -7.000  -0.1456   0.01847   0.01536  -0.1244   0.7972   0.0112
  -6.750  -0.1364   0.01566   0.01235  -0.1231   0.7957   0.0115
  -6.500  -0.1242   0.01295   0.00941  -0.1218   0.7943   0.0123
  -6.250  -0.1017   0.01190   0.00810  -0.1207   0.7931   0.0135
  -6.000  -0.1045   0.01699   0.01187  -0.1231   0.7944   0.0099
  -5.750  -0.0813   0.01539   0.01006  -0.1225   0.7932   0.0100
  -5.500  -0.0560   0.01472   0.00932  -0.1226   0.7921   0.0107
  -5.250  -0.0307   0.01365   0.00811  -0.1223   0.7911   0.0107
  -5.000  -0.0050   0.01283   0.00718  -0.1221   0.7899   0.0108
  -4.750   0.0203   0.01218   0.00644  -0.1218   0.7885   0.0109
  -4.500   0.0460   0.01166   0.00590  -0.1217   0.7875   0.0114
  -4.250   0.0718   0.01121   0.00543  -0.1216   0.7864   0.0119
  -4.000   0.0971   0.01066   0.00482  -0.1213   0.7850   0.0122
  -3.750   0.1230   0.01020   0.00432  -0.1211   0.7836   0.0125
  -3.500   0.1496   0.00986   0.00395  -0.1212   0.7822   0.0133
  -3.250   0.1761   0.00941   0.00343  -0.1211   0.7809   0.0151
  -3.000   0.2037   0.00920   0.00320  -0.1213   0.7796   0.0175
  -2.750   0.2315   0.00897   0.00295  -0.1216   0.7784   0.0219
  -2.500   0.2593   0.00870   0.00276  -0.1219   0.7772   0.0457
  -2.250   0.2861   0.00821   0.00263  -0.1223   0.7758   0.1586
  -2.000   0.3120   0.00744   0.00254  -0.1229   0.7742   0.3829
  -1.750   0.3390   0.00636   0.00240  -0.1239   0.7730   0.6754
  -1.500   0.3663   0.00638   0.00264  -0.1238   0.7716   0.7667
  -1.250   0.3946   0.00650   0.00275  -0.1240   0.7701   0.7841
  -1.000   0.4222   0.00668   0.00293  -0.1238   0.7685   0.7990
  -0.750   0.4498   0.00683   0.00308  -0.1237   0.7669   0.8096
  -0.500   0.4772   0.00698   0.00323  -0.1236   0.7653   0.8184
  -0.250   0.5046   0.00705   0.00329  -0.1235   0.7639   0.8241
   0.000   0.5322   0.00715   0.00338  -0.1234   0.7626   0.8292
   0.250   0.5612   0.00726   0.00346  -0.1238   0.7611   0.8337
   0.500   0.5884   0.00729   0.00351  -0.1238   0.7595   0.8369
   0.750   0.6153   0.00730   0.00355  -0.1238   0.7577   0.8395
   1.000   0.6431   0.00730   0.00356  -0.1239   0.7555   0.8416
   1.250   0.6717   0.00726   0.00352  -0.1243   0.7531   0.8432
   1.500   0.7010   0.00721   0.00346  -0.1248   0.7506   0.8445
   1.750   0.7305   0.00717   0.00339  -0.1254   0.7484   0.8455
   2.000   0.7597   0.00717   0.00338  -0.1260   0.7458   0.8465
   2.250   0.7876   0.00711   0.00336  -0.1263   0.7423   0.8474
   2.500   0.8163   0.00704   0.00330  -0.1267   0.7384   0.8482
   2.750   0.8451   0.00695   0.00321  -0.1271   0.7347   0.8489
   3.000   0.8728   0.00688   0.00316  -0.1273   0.7303   0.8499
   3.250   0.9001   0.00680   0.00313  -0.1274   0.7247   0.8506
   3.500   0.9281   0.00675   0.00305  -0.1276   0.7191   0.8511
   3.750   0.9546   0.00669   0.00305  -0.1276   0.7104   0.8518
   4.000   0.9813   0.00667   0.00303  -0.1275   0.7009   0.8525
   4.250   1.0068   0.00667   0.00303  -0.1272   0.6857   0.8533
   4.500   1.0310   0.00676   0.00307  -0.1267   0.6670   0.8540
   4.750   1.0545   0.00691   0.00316  -0.1260   0.6464   0.8546
   5.000   1.0753   0.00715   0.00331  -0.1249   0.6158   0.8554
   5.250   1.0893   0.00764   0.00359  -0.1224   0.5626   0.8563
   5.500   1.0920   0.00853   0.00411  -0.1177   0.4866   0.8577
   5.750   1.0936   0.00942   0.00468  -0.1130   0.4193   0.8590
   6.000   1.0903   0.01024   0.00520  -0.1073   0.3605   0.8602
   6.250   1.0872   0.01118   0.00586  -0.1019   0.3035   0.8614
   6.500   1.0843   0.01223   0.00664  -0.0969   0.2466   0.8624
   6.750   1.0853   0.01325   0.00741  -0.0929   0.1980   0.8635
   7.000   1.0887   0.01427   0.00823  -0.0894   0.1546   0.8647
   7.250   1.0948   0.01525   0.00903  -0.0864   0.1172   0.8660
   7.500   1.1024   0.01623   0.00985  -0.0838   0.0849   0.8671
   7.750   1.1118   0.01717   0.01066  -0.0816   0.0583   0.8681
   8.000   1.1223   0.01810   0.01148  -0.0795   0.0393   0.8690
   8.250   1.1361   0.01886   0.01221  -0.0779   0.0309   0.8699
   8.500   1.1518   0.01953   0.01291  -0.0766   0.0268   0.8707
   8.750   1.1668   0.02026   0.01364  -0.0753   0.0237   0.8716
   9.000   1.1802   0.02112   0.01453  -0.0737   0.0208   0.8725
   9.250   1.1976   0.02171   0.01517  -0.0728   0.0197   0.8734
   9.500   1.2137   0.02240   0.01589  -0.0717   0.0184   0.8742
   9.750   1.2284   0.02321   0.01672  -0.0705   0.0169   0.8750
  10.000   1.2384   0.02437   0.01795  -0.0687   0.0150   0.8759
  10.250   1.2546   0.02509   0.01872  -0.0677   0.0143   0.8766
  10.500   1.2717   0.02573   0.01939  -0.0669   0.0133   0.8778
  10.750   1.2872   0.02649   0.02019  -0.0659   0.0123   0.8791
  11.000   1.3004   0.02743   0.02116  -0.0647   0.0112   0.8804
  11.250   1.3082   0.02883   0.02264  -0.0629   0.0100   0.8816
  11.500   1.3242   0.02960   0.02347  -0.0620   0.0095   0.8828
  11.750   1.3386   0.03050   0.02442  -0.0611   0.0086   0.8840
  12.000   1.3524   0.03147   0.02544  -0.0601   0.0081   0.8853
  12.250   1.3575   0.03322   0.02725  -0.0583   0.0070   0.8866
  12.500   1.3684   0.03450   0.02862  -0.0571   0.0066   0.8879
  12.750   1.3811   0.03565   0.02984  -0.0562   0.0063   0.8893
  13.000   1.3918   0.03701   0.03128  -0.0551   0.0060   0.8906
  13.250   1.4017   0.03843   0.03277  -0.0540   0.0057   0.8924
  13.500   1.4124   0.03979   0.03421  -0.0531   0.0054   0.8943
  13.750   1.4211   0.04137   0.03586  -0.0521   0.0051   0.8964
  14.000   1.4262   0.04337   0.03796  -0.0509   0.0049   0.8986
  14.250   1.4178   0.04689   0.04167  -0.0488   0.0045   0.9005
  14.500   1.4282   0.04844   0.04331  -0.0482   0.0044   0.9033
  14.750   1.4340   0.05053   0.04554  -0.0474   0.0043   0.9064
  15.000   1.4403   0.05255   0.04767  -0.0466   0.0042   0.9109
  15.250   1.4444   0.05485   0.05012  -0.0459   0.0041   0.9164
  15.500   1.4457   0.05736   0.05278  -0.0449   0.0040   0.9267
  15.750   1.4431   0.05984   0.05547  -0.0434   0.0039   1.0000
  16.000   1.4448   0.06278   0.05852  -0.0432   0.0038   1.0000
  16.250   1.4438   0.06615   0.06203  -0.0430   0.0037   1.0000
  16.500   1.4427   0.06960   0.06561  -0.0430   0.0037   1.0000
  16.750   1.4403   0.07331   0.06945  -0.0433   0.0036   1.0000
  17.000   1.4362   0.07740   0.07369  -0.0437   0.0036   1.0000
  17.250   1.4306   0.08185   0.07828  -0.0445   0.0035   1.0000
  17.500   1.4245   0.08649   0.08307  -0.0455   0.0035   1.0000
  17.750   1.4164   0.09161   0.08834  -0.0469   0.0035   1.0000
  18.000   1.4072   0.09708   0.09396  -0.0487   0.0034   1.0000
  18.250   1.3969   0.10293   0.09997  -0.0509   0.0034   1.0000
  18.500   1.3850   0.10929   0.10648  -0.0535   0.0034   1.0000
  18.750   1.3717   0.11609   0.11345  -0.0567   0.0034   1.0000
  19.000   1.3568   0.12342   0.12095  -0.0605   0.0034   1.0000
  19.250   1.3408   0.13126   0.12896  -0.0648   0.0034   1.0000
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