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GOE 534 AIRFOIL (goe534-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 534 AIRFOIL (goe534-il)
Reynolds number: 1,000,000
Max Cl/Cd: 114.93 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe534-il-1000000.txt
Download as CSV file: xf-goe534-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 534 AIRFOIL                                 
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.7681   0.09112   0.08854  -0.0462   1.0000   0.0269
 -15.750  -0.7973   0.08248   0.07978  -0.0520   1.0000   0.0271
 -15.500  -0.8187   0.07549   0.07268  -0.0567   1.0000   0.0271
 -15.250  -0.8382   0.06898   0.06609  -0.0612   1.0000   0.0273
 -15.000  -0.8550   0.06318   0.06020  -0.0652   1.0000   0.0274
 -14.750  -0.8738   0.05759   0.05453  -0.0691   1.0000   0.0274
 -14.500  -0.8933   0.05213   0.04898  -0.0729   1.0000   0.0275
 -14.250  -0.9146   0.04698   0.04375  -0.0762   1.0000   0.0275
 -14.000  -0.9528   0.04142   0.03812  -0.0785   1.0000   0.0275
 -13.750  -0.9679   0.03581   0.03240  -0.0837   1.0000   0.0276
 -13.500  -0.9667   0.03122   0.02766  -0.0884   1.0000   0.0277
 -13.250  -0.9539   0.02767   0.02397  -0.0922   1.0000   0.0279
 -13.000  -0.9369   0.02559   0.02176  -0.0937   1.0000   0.0280
 -12.750  -0.9234   0.02388   0.01993  -0.0936   1.0000   0.0282
 -12.500  -0.9114   0.02211   0.01808  -0.0930   1.0000   0.0286
 -12.250  -0.8959   0.02087   0.01678  -0.0921   1.0000   0.0289
 -12.000  -0.8646   0.01976   0.01562  -0.0938   0.9986   0.0293
 -11.750  -0.8278   0.01879   0.01459  -0.0963   0.9961   0.0296
 -11.500  -0.7904   0.01794   0.01368  -0.0987   0.9935   0.0301
 -11.250  -0.7560   0.01717   0.01285  -0.1003   0.9900   0.0306
 -11.000  -0.7220   0.01648   0.01210  -0.1018   0.9858   0.0310
 -10.750  -0.6862   0.01582   0.01138  -0.1035   0.9822   0.0314
 -10.500  -0.6534   0.01524   0.01074  -0.1044   0.9768   0.0317
 -10.250  -0.6200   0.01454   0.00997  -0.1056   0.9693   0.0321
 -10.000  -0.5849   0.01366   0.00904  -0.1073   0.9603   0.0328
  -9.750  -0.5459   0.01300   0.00833  -0.1096   0.9480   0.0334
  -9.500  -0.5071   0.01248   0.00772  -0.1116   0.9233   0.0341
  -9.250  -0.4765   0.01214   0.00722  -0.1118   0.8862   0.0347
  -9.000  -0.4510   0.01190   0.00681  -0.1110   0.8532   0.0353
  -8.750  -0.4257   0.01168   0.00644  -0.1101   0.8283   0.0358
  -8.500  -0.4005   0.01135   0.00599  -0.1092   0.8088   0.0365
  -8.250  -0.3749   0.01101   0.00557  -0.1085   0.7935   0.0376
  -8.000  -0.3488   0.01074   0.00522  -0.1078   0.7804   0.0386
  -7.750  -0.3219   0.01049   0.00490  -0.1072   0.7687   0.0397
  -7.500  -0.2952   0.01024   0.00459  -0.1066   0.7577   0.0413
  -7.250  -0.2683   0.00996   0.00428  -0.1060   0.7471   0.0443
  -7.000  -0.2414   0.00972   0.00406  -0.1055   0.7377   0.0514
  -6.750  -0.2131   0.00967   0.00405  -0.1050   0.7279   0.0612
  -6.500  -0.1848   0.00971   0.00408  -0.1045   0.7180   0.0659
  -6.250  -0.1559   0.00978   0.00409  -0.1041   0.7077   0.0685
  -6.000  -0.1281   0.00971   0.00400  -0.1037   0.6978   0.0712
  -5.750  -0.0996   0.00971   0.00398  -0.1032   0.6864   0.0732
  -5.500  -0.0714   0.00972   0.00393  -0.1028   0.6746   0.0748
  -5.250  -0.0431   0.00978   0.00390  -0.1023   0.6608   0.0758
  -5.000  -0.0161   0.00954   0.00363  -0.1018   0.6453   0.0777
  -4.750   0.0114   0.00947   0.00351  -0.1013   0.6271   0.0793
  -4.500   0.0389   0.00947   0.00343  -0.1007   0.6060   0.0809
  -4.250   0.0660   0.00948   0.00333  -0.1001   0.5824   0.0822
  -4.000   0.0933   0.00950   0.00324  -0.0995   0.5592   0.0832
  -3.750   0.1207   0.00954   0.00318  -0.0990   0.5395   0.0840
  -3.500   0.1479   0.00951   0.00305  -0.0984   0.5234   0.0848
  -3.250   0.1752   0.00935   0.00284  -0.0979   0.5112   0.0864
  -3.000   0.2028   0.00927   0.00273  -0.0975   0.5009   0.0876
  -2.750   0.2306   0.00923   0.00264  -0.0970   0.4911   0.0888
  -2.500   0.2585   0.00920   0.00257  -0.0966   0.4820   0.0902
  -2.250   0.2865   0.00916   0.00250  -0.0962   0.4729   0.0913
  -2.000   0.3143   0.00915   0.00244  -0.0958   0.4647   0.0923
  -1.750   0.3426   0.00912   0.00239  -0.0954   0.4575   0.0934
  -1.500   0.3703   0.00911   0.00232  -0.0949   0.4491   0.0946
  -1.250   0.3984   0.00903   0.00223  -0.0945   0.4421   0.0964
  -1.000   0.4263   0.00900   0.00217  -0.0941   0.4342   0.0981
  -0.750   0.4541   0.00900   0.00214  -0.0937   0.4269   0.0999
  -0.500   0.4823   0.00897   0.00211  -0.0933   0.4204   0.1018
  -0.250   0.5101   0.00900   0.00209  -0.0929   0.4130   0.1039
   0.000   0.5379   0.00897   0.00207  -0.0925   0.4062   0.1098
   0.250   0.5656   0.00892   0.00205  -0.0921   0.3986   0.1244
   0.500   0.5921   0.00874   0.00206  -0.0916   0.3906   0.1971
   0.750   0.6198   0.00864   0.00209  -0.0913   0.3845   0.2408
   1.000   0.6471   0.00865   0.00215  -0.0908   0.3768   0.2694
   1.250   0.6746   0.00868   0.00221  -0.0904   0.3694   0.2918
   1.500   0.7021   0.00872   0.00227  -0.0900   0.3611   0.3127
   1.750   0.7292   0.00879   0.00235  -0.0895   0.3530   0.3303
   2.000   0.7568   0.00884   0.00243  -0.0891   0.3453   0.3477
   2.250   0.7836   0.00896   0.00252  -0.0886   0.3360   0.3629
   2.500   0.8110   0.00903   0.00260  -0.0882   0.3276   0.3772
   2.750   0.8376   0.00916   0.00271  -0.0877   0.3181   0.3916
   3.000   0.8647   0.00925   0.00281  -0.0872   0.3091   0.4060
   3.500   0.9177   0.00953   0.00306  -0.0862   0.2899   0.4326
   3.750   0.9440   0.00968   0.00319  -0.0856   0.2811   0.4451
   4.000   0.9702   0.00985   0.00333  -0.0850   0.2721   0.4574
   4.250   0.9963   0.00999   0.00348  -0.0845   0.2642   0.4698
   4.500   1.0223   0.01015   0.00363  -0.0839   0.2567   0.4839
   4.750   1.0479   0.01032   0.00380  -0.0833   0.2498   0.5003
   5.000   1.0739   0.01045   0.00395  -0.0827   0.2440   0.5170
   5.250   1.0989   0.01063   0.00415  -0.0820   0.2371   0.5382
   5.500   1.1242   0.01073   0.00432  -0.0813   0.2325   0.5700
   5.750   1.1479   0.01069   0.00452  -0.0804   0.2280   0.6652
   6.000   1.1960   0.01048   0.00483  -0.0848   0.2207   1.0000
   6.250   1.2215   0.01066   0.00500  -0.0842   0.2170   1.0000
   6.500   1.2470   0.01085   0.00518  -0.0835   0.2133   1.0000
   6.750   1.2716   0.01109   0.00538  -0.0828   0.2090   1.0000
   7.000   1.2952   0.01139   0.00564  -0.0819   0.2037   1.0000
   7.250   1.3207   0.01155   0.00581  -0.0813   0.2011   1.0000
   7.500   1.3454   0.01175   0.00601  -0.0806   0.1974   1.0000
   7.750   1.3690   0.01202   0.00624  -0.0798   0.1928   1.0000
   8.000   1.3920   0.01233   0.00652  -0.0788   0.1881   1.0000
   8.250   1.4166   0.01251   0.00672  -0.0782   0.1852   1.0000
   8.500   1.4402   0.01274   0.00695  -0.0773   0.1816   1.0000
   8.750   1.4625   0.01305   0.00723  -0.0763   0.1772   1.0000
   9.000   1.4847   0.01335   0.00752  -0.0753   0.1733   1.0000
   9.250   1.5080   0.01358   0.00776  -0.0744   0.1705   1.0000
   9.500   1.5300   0.01386   0.00803  -0.0734   0.1668   1.0000
   9.750   1.5504   0.01422   0.00837  -0.0721   0.1625   1.0000
  10.000   1.5712   0.01453   0.00869  -0.0709   0.1591   1.0000
  10.250   1.5922   0.01481   0.00898  -0.0698   0.1557   1.0000
  10.500   1.6111   0.01518   0.00933  -0.0683   0.1516   1.0000
  10.750   1.6263   0.01561   0.00975  -0.0662   0.1472   1.0000
  11.000   1.6439   0.01591   0.01008  -0.0645   0.1447   1.0000
  11.250   1.6596   0.01629   0.01047  -0.0625   0.1414   1.0000
  11.500   1.6734   0.01678   0.01095  -0.0604   0.1376   1.0000
  11.750   1.6873   0.01728   0.01146  -0.0583   0.1342   1.0000
  12.000   1.7031   0.01772   0.01193  -0.0566   0.1316   1.0000
  12.250   1.7167   0.01828   0.01250  -0.0548   0.1284   1.0000
  12.500   1.7280   0.01900   0.01322  -0.0527   0.1249   1.0000
  12.750   1.7407   0.01968   0.01393  -0.0510   0.1223   1.0000
  13.000   1.7542   0.02035   0.01464  -0.0495   0.1198   1.0000
  13.250   1.7655   0.02120   0.01550  -0.0479   0.1170   1.0000
  13.500   1.7737   0.02232   0.01663  -0.0463   0.1136   1.0000
  13.750   1.7846   0.02332   0.01768  -0.0450   0.1111   1.0000
  14.000   1.7957   0.02439   0.01878  -0.0439   0.1085   1.0000
  14.250   1.8037   0.02574   0.02016  -0.0428   0.1056   1.0000
  14.500   1.8084   0.02747   0.02191  -0.0418   0.1026   1.0000
  14.750   1.8177   0.02886   0.02336  -0.0411   0.1006   1.0000
  15.000   1.8254   0.03044   0.02499  -0.0404   0.0987   1.0000
  15.250   1.8301   0.03234   0.02693  -0.0398   0.0965   1.0000
  15.500   1.8312   0.03463   0.02926  -0.0392   0.0942   1.0000
  15.750   1.8312   0.03708   0.03177  -0.0388   0.0921   1.0000
  16.000   1.8355   0.03914   0.03390  -0.0384   0.0905   1.0000
  16.250   1.8362   0.04162   0.03644  -0.0382   0.0888   1.0000
  16.500   1.8327   0.04459   0.03947  -0.0380   0.0868   1.0000
  16.750   1.8267   0.04796   0.04290  -0.0381   0.0852   1.0000
  17.000   1.8168   0.05189   0.04690  -0.0384   0.0834   1.0000
  17.250   1.8146   0.05498   0.05009  -0.0387   0.0824   1.0000
  17.500   1.8097   0.05846   0.05365  -0.0391   0.0813   1.0000
  17.750   1.8015   0.06237   0.05764  -0.0397   0.0798   1.0000
  18.000   1.7906   0.06666   0.06200  -0.0404   0.0787   1.0000
  18.250   1.7763   0.07144   0.06686  -0.0413   0.0774   1.0000
  18.500   1.7599   0.07653   0.07203  -0.0424   0.0763   1.0000
  18.750   1.7430   0.08177   0.07735  -0.0436   0.0752   1.0000
  19.000   1.7343   0.08597   0.08164  -0.0446   0.0744   1.0000
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