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GOE 614 AIRFOIL (goe614-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 614 AIRFOIL (goe614-il)
Reynolds number: 1,000,000
Max Cl/Cd: 105.35 at α=5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe614-il-1000000.txt
Download as CSV file: xf-goe614-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 614 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
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.3638   0.08799   0.08576  -0.1051   0.9866   0.0268
 -14.750  -0.3152   0.09230   0.09019  -0.1017   0.9855   0.0263
 -14.500  -0.4299   0.06680   0.06428  -0.1219   0.9834   0.0256
 -14.250  -0.4590   0.05659   0.05384  -0.1332   0.9818   0.0254
 -14.000  -0.4775   0.05002   0.04711  -0.1395   0.9755   0.0254
 -13.750  -0.4819   0.04405   0.04096  -0.1475   0.9718   0.0254
 -13.500  -0.4777   0.03895   0.03569  -0.1556   0.9690   0.0256
 -13.250  -0.4779   0.03514   0.03172  -0.1602   0.9592   0.0256
 -13.000  -0.4595   0.03148   0.02788  -0.1678   0.9547   0.0256
 -12.750  -0.4434   0.02893   0.02516  -0.1724   0.9439   0.0257
 -12.500  -0.4164   0.02682   0.02288  -0.1772   0.9353   0.0258
 -12.250  -0.3917   0.02525   0.02114  -0.1800   0.9240   0.0259
 -12.000  -0.3773   0.02412   0.01985  -0.1798   0.9078   0.0260
 -11.750  -0.3668   0.02319   0.01877  -0.1782   0.8915   0.0261
 -11.500  -0.3555   0.02243   0.01786  -0.1765   0.8756   0.0262
 -11.250  -0.3438   0.02171   0.01701  -0.1745   0.8619   0.0263
 -11.000  -0.3303   0.02101   0.01618  -0.1727   0.8499   0.0263
 -10.750  -0.3164   0.02038   0.01542  -0.1709   0.8381   0.0264
 -10.500  -0.3014   0.01981   0.01476  -0.1691   0.8275   0.0265
 -10.250  -0.2849   0.01930   0.01413  -0.1674   0.8174   0.0265
 -10.000  -0.2681   0.01896   0.01368  -0.1658   0.8079   0.0267
  -9.750  -0.2510   0.01818   0.01280  -0.1643   0.7988   0.0268
  -9.500  -0.2340   0.01716   0.01175  -0.1628   0.7901   0.0269
  -9.250  -0.2176   0.01635   0.01088  -0.1611   0.7809   0.0272
  -9.000  -0.1995   0.01573   0.01025  -0.1596   0.7724   0.0275
  -8.500  -0.1608   0.01484   0.00926  -0.1568   0.7552   0.0280
  -8.250  -0.1414   0.01446   0.00880  -0.1553   0.7458   0.0281
  -8.000  -0.1208   0.01407   0.00837  -0.1541   0.7366   0.0283
  -7.500  -0.0798   0.01337   0.00756  -0.1514   0.7169   0.0287
  -7.250  -0.0593   0.01308   0.00719  -0.1500   0.7070   0.0289
  -7.000  -0.0377   0.01276   0.00682  -0.1488   0.6970   0.0291
  -6.750  -0.0166   0.01250   0.00649  -0.1475   0.6867   0.0293
  -6.500   0.0048   0.01223   0.00616  -0.1462   0.6756   0.0295
  -6.250   0.0265   0.01199   0.00586  -0.1450   0.6647   0.0298
  -5.750   0.0704   0.01157   0.00530  -0.1426   0.6430   0.0302
  -5.500   0.0924   0.01141   0.00506  -0.1413   0.6328   0.0304
  -5.250   0.1153   0.01124   0.00484  -0.1403   0.6225   0.0306
  -5.000   0.1379   0.01110   0.00463  -0.1392   0.6128   0.0308
  -4.750   0.1591   0.01081   0.00426  -0.1378   0.6027   0.0313
  -4.500   0.1814   0.01061   0.00400  -0.1367   0.5934   0.0319
  -4.250   0.2038   0.01047   0.00380  -0.1355   0.5836   0.0325
  -4.000   0.2271   0.01035   0.00363  -0.1345   0.5752   0.0332
  -3.750   0.2502   0.01026   0.00349  -0.1334   0.5664   0.0338
  -3.500   0.2736   0.01018   0.00335  -0.1324   0.5588   0.0344
  -3.250   0.2974   0.01010   0.00324  -0.1315   0.5512   0.0350
  -3.000   0.3196   0.01005   0.00312  -0.1303   0.5435   0.0358
  -2.750   0.3440   0.00994   0.00300  -0.1294   0.5372   0.0373
  -2.500   0.3663   0.00990   0.00290  -0.1282   0.5299   0.0392
  -2.250   0.3877   0.00981   0.00280  -0.1268   0.5226   0.0448
  -2.000   0.4074   0.00950   0.00268  -0.1252   0.5160   0.1005
  -1.750   0.4273   0.00947   0.00264  -0.1235   0.5083   0.1139
  -1.500   0.4498   0.00932   0.00257  -0.1224   0.5030   0.1367
  -1.250   0.4714   0.00917   0.00257  -0.1212   0.4975   0.1855
  -1.000   0.4927   0.00919   0.00260  -0.1198   0.4912   0.2032
  -0.750   0.5161   0.00918   0.00262  -0.1189   0.4865   0.2176
  -0.500   0.5392   0.00919   0.00264  -0.1178   0.4804   0.2277
  -0.250   0.5611   0.00926   0.00269  -0.1166   0.4747   0.2368
   0.000   0.5838   0.00930   0.00274  -0.1155   0.4690   0.2474
   0.250   0.6076   0.00934   0.00278  -0.1146   0.4636   0.2570
   0.500   0.6292   0.00940   0.00285  -0.1134   0.4573   0.2699
   0.750   0.6514   0.00947   0.00293  -0.1122   0.4525   0.2841
   1.000   0.6751   0.00948   0.00299  -0.1114   0.4482   0.3007
   1.250   0.6972   0.00952   0.00307  -0.1103   0.4431   0.3222
   1.500   0.7177   0.00961   0.00318  -0.1088   0.4376   0.3454
   1.750   0.7406   0.00964   0.00327  -0.1079   0.4336   0.3713
   2.000   0.7637   0.00967   0.00337  -0.1069   0.4299   0.3964
   2.250   0.7858   0.00974   0.00347  -0.1058   0.4258   0.4185
   2.500   0.8064   0.00983   0.00360  -0.1045   0.4216   0.4416
   2.750   0.8274   0.00992   0.00373  -0.1032   0.4174   0.4659
   3.000   0.8503   0.00995   0.00384  -0.1023   0.4141   0.4933
   3.250   0.8719   0.01000   0.00397  -0.1011   0.4102   0.5260
   3.500   0.8915   0.01009   0.00412  -0.0996   0.4054   0.5611
   3.750   0.9099   0.01020   0.00430  -0.0979   0.4009   0.5976
   4.000   0.9300   0.01017   0.00444  -0.0964   0.3978   0.6554
   4.250   0.9437   0.01002   0.00463  -0.0936   0.3940   0.7788
   4.500   1.0560   0.01011   0.00504  -0.1121   0.3855   1.0000
   4.750   1.0780   0.01027   0.00518  -0.1111   0.3817   1.0000
   5.000   1.0999   0.01044   0.00533  -0.1101   0.3774   1.0000
   5.250   1.1207   0.01064   0.00551  -0.1090   0.3728   1.0000
   5.500   1.1401   0.01091   0.00573  -0.1076   0.3676   1.0000
   5.750   1.1627   0.01108   0.00590  -0.1068   0.3640   1.0000
   6.000   1.1838   0.01130   0.00610  -0.1058   0.3587   1.0000
   6.250   1.2023   0.01162   0.00637  -0.1043   0.3520   1.0000
   6.500   1.2237   0.01185   0.00659  -0.1034   0.3472   1.0000
   6.750   1.2440   0.01213   0.00685  -0.1024   0.3410   1.0000
   7.000   1.2616   0.01251   0.00718  -0.1009   0.3344   1.0000
   7.250   1.2827   0.01278   0.00744  -0.1000   0.3288   1.0000
   7.500   1.3005   0.01318   0.00781  -0.0987   0.3207   1.0000
   7.750   1.3187   0.01358   0.00818  -0.0974   0.3131   1.0000
   8.000   1.3348   0.01408   0.00863  -0.0959   0.3036   1.0000
   8.250   1.3517   0.01456   0.00908  -0.0945   0.2943   1.0000
   8.500   1.3665   0.01516   0.00962  -0.0929   0.2852   1.0000
   8.750   1.3807   0.01579   0.01021  -0.0913   0.2744   1.0000
   9.000   1.3954   0.01643   0.01081  -0.0898   0.2661   1.0000
   9.250   1.4073   0.01723   0.01155  -0.0880   0.2562   1.0000
   9.500   1.4218   0.01791   0.01222  -0.0866   0.2482   1.0000
   9.750   1.4338   0.01875   0.01303  -0.0850   0.2410   1.0000
  10.000   1.4467   0.01956   0.01382  -0.0835   0.2328   1.0000
  10.250   1.4570   0.02055   0.01478  -0.0819   0.2254   1.0000
  10.500   1.4706   0.02138   0.01560  -0.0806   0.2192   1.0000
  10.750   1.4782   0.02260   0.01678  -0.0788   0.2105   1.0000
  11.000   1.4900   0.02358   0.01775  -0.0775   0.2040   1.0000
  11.250   1.4979   0.02485   0.01900  -0.0759   0.1966   1.0000
  11.500   1.5074   0.02606   0.02020  -0.0746   0.1886   1.0000
  11.750   1.5110   0.02771   0.02180  -0.0728   0.1764   1.0000
  12.000   1.4923   0.03107   0.02498  -0.0695   0.1423   1.0000
  12.250   1.4790   0.03425   0.02808  -0.0669   0.1248   1.0000
  12.500   1.4804   0.03635   0.03018  -0.0656   0.1198   1.0000
  12.750   1.4839   0.03835   0.03222  -0.0645   0.1175   1.0000
  13.000   1.4911   0.04008   0.03399  -0.0637   0.1167   1.0000
  13.250   1.4935   0.04226   0.03620  -0.0627   0.1145   1.0000
  13.500   1.4979   0.04431   0.03829  -0.0619   0.1130   1.0000
  13.750   1.5010   0.04651   0.04054  -0.0611   0.1117   1.0000
  14.000   1.5034   0.04884   0.04292  -0.0604   0.1100   1.0000
  14.250   1.5095   0.05081   0.04495  -0.0599   0.1095   1.0000
  14.500   1.5136   0.05303   0.04724  -0.0594   0.1090   1.0000
  14.750   1.5177   0.05523   0.04950  -0.0589   0.1083   1.0000
  15.000   1.5200   0.05766   0.05199  -0.0584   0.1075   1.0000
  15.250   1.5218   0.06017   0.05457  -0.0580   0.1069   1.0000
  15.500   1.5235   0.06271   0.05718  -0.0577   0.1062   1.0000
  15.750   1.5234   0.06549   0.06001  -0.0573   0.1054   1.0000
  16.000   1.5217   0.06844   0.06303  -0.0570   0.1046   1.0000
  16.250   1.5202   0.07138   0.06603  -0.0567   0.1036   1.0000
  16.500   1.5179   0.07449   0.06919  -0.0565   0.1028   1.0000
  16.750   1.5132   0.07789   0.07267  -0.0564   0.1016   1.0000
  17.000   1.5097   0.08115   0.07598  -0.0563   0.1004   1.0000
  17.250   1.5024   0.08490   0.07980  -0.0563   0.0990   1.0000
  17.500   1.5024   0.08779   0.08276  -0.0563   0.0985   1.0000
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