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GOE 504 AIRFOIL (goe504-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 504 AIRFOIL (goe504-il)
Reynolds number: 500,000
Max Cl/Cd: 91.73 at α=4°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe504-il-500000.txt
Download as CSV file: xf-goe504-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 504 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.2935   0.08050   0.07811  -0.1005   0.9829   0.0234
 -12.750  -0.3312   0.06819   0.06567  -0.1104   0.9775   0.0229
 -12.500  -0.3668   0.05512   0.05233  -0.1250   0.9726   0.0225
 -12.250  -0.3849   0.04629   0.04320  -0.1369   0.9665   0.0225
 -12.000  -0.3931   0.04024   0.03685  -0.1449   0.9589   0.0224
 -11.750  -0.3918   0.03616   0.03242  -0.1500   0.9504   0.0227
 -11.500  -0.3895   0.03306   0.02894  -0.1517   0.9397   0.0231
 -11.250  -0.3910   0.03153   0.02713  -0.1493   0.9248   0.0234
 -11.000  -0.3908   0.03055   0.02587  -0.1462   0.9096   0.0236
 -10.750  -0.3920   0.02794   0.02297  -0.1433   0.8951   0.0242
 -10.500  -0.3781   0.02636   0.02131  -0.1421   0.8830   0.0247
 -10.250  -0.3581   0.02558   0.02052  -0.1414   0.8721   0.0253
 -10.000  -0.3425   0.02460   0.01940  -0.1400   0.8609   0.0258
  -9.750  -0.3282   0.02390   0.01855  -0.1381   0.8489   0.0267
  -9.500  -0.3143   0.02306   0.01752  -0.1361   0.8375   0.0274
  -9.250  -0.2988   0.02231   0.01654  -0.1342   0.8273   0.0280
  -9.000  -0.2826   0.02192   0.01592  -0.1323   0.8172   0.0285
  -8.750  -0.2659   0.02063   0.01444  -0.1307   0.8076   0.0290
  -8.250  -0.2249   0.01842   0.01215  -0.1289   0.7906   0.0306
  -8.000  -0.2037   0.01785   0.01150  -0.1279   0.7828   0.0317
  -7.750  -0.1836   0.01728   0.01086  -0.1266   0.7744   0.0324
  -7.500  -0.1619   0.01677   0.01022  -0.1256   0.7671   0.0331
  -7.250  -0.1412   0.01629   0.00968  -0.1243   0.7593   0.0337
  -7.000  -0.1185   0.01601   0.00926  -0.1233   0.7522   0.0343
  -6.750  -0.1015   0.01506   0.00828  -0.1216   0.7449   0.0353
  -6.500  -0.0825   0.01446   0.00762  -0.1201   0.7379   0.0362
  -6.250  -0.0624   0.01401   0.00713  -0.1187   0.7311   0.0370
  -6.000  -0.0417   0.01364   0.00670  -0.1174   0.7241   0.0378
  -5.750  -0.0199   0.01331   0.00629  -0.1163   0.7177   0.0386
  -5.500   0.0017   0.01301   0.00594  -0.1151   0.7106   0.0397
  -5.250   0.0247   0.01276   0.00560  -0.1142   0.7045   0.0406
  -5.000   0.0469   0.01250   0.00529  -0.1131   0.6977   0.0412
  -4.750   0.0688   0.01217   0.00489  -0.1119   0.6912   0.0426
  -4.500   0.0921   0.01194   0.00459  -0.1110   0.6850   0.0442
  -4.250   0.1152   0.01173   0.00434  -0.1101   0.6783   0.0463
  -4.000   0.1397   0.01160   0.00411  -0.1094   0.6721   0.0487
  -3.750   0.1627   0.01138   0.00394  -0.1084   0.6655   0.0557
  -3.500   0.1844   0.01104   0.00373  -0.1073   0.6591   0.0958
  -3.250   0.2029   0.01046   0.00352  -0.1058   0.6531   0.1975
  -3.000   0.2261   0.01032   0.00350  -0.1049   0.6463   0.2364
  -2.750   0.2511   0.01030   0.00345  -0.1044   0.6403   0.2581
  -2.500   0.2752   0.01026   0.00344  -0.1036   0.6337   0.2752
  -2.250   0.2998   0.01026   0.00341  -0.1030   0.6273   0.2897
  -2.000   0.3241   0.01023   0.00338  -0.1023   0.6211   0.3007
  -1.750   0.3482   0.01021   0.00335  -0.1015   0.6144   0.3103
  -1.500   0.3727   0.01023   0.00331  -0.1009   0.6085   0.3208
  -1.250   0.3962   0.01018   0.00330  -0.1001   0.6021   0.3315
  -1.000   0.4198   0.01017   0.00328  -0.0992   0.5958   0.3455
  -0.750   0.4437   0.01017   0.00326  -0.0985   0.5899   0.3585
  -0.500   0.4666   0.01012   0.00326  -0.0976   0.5837   0.3721
  -0.250   0.4896   0.01011   0.00325  -0.0967   0.5778   0.3922
   0.250   0.5308   0.00984   0.00329  -0.0940   0.5660   0.4822
   0.500   0.5486   0.00964   0.00333  -0.0920   0.5606   0.5690
   0.750   0.5624   0.00933   0.00340  -0.0892   0.5551   0.6763
   1.000   0.5763   0.00907   0.00350  -0.0861   0.5493   0.7907
   1.250   0.6164   0.00908   0.00373  -0.0885   0.5435   0.8952
   1.500   0.6817   0.00931   0.00397  -0.0967   0.5362   0.9390
   1.750   0.7320   0.00958   0.00414  -0.1016   0.5297   0.9565
   2.000   0.7708   0.00977   0.00432  -0.1040   0.5234   0.9701
   2.250   0.8109   0.01000   0.00447  -0.1068   0.5169   0.9796
   2.500   0.8529   0.01021   0.00462  -0.1101   0.5107   0.9860
   2.750   0.8941   0.01038   0.00476  -0.1132   0.5037   0.9923
   3.000   0.9369   0.01059   0.00488  -0.1167   0.4972   0.9972
   3.250   0.9732   0.01069   0.00498  -0.1189   0.4908   1.0000
   3.500   0.9854   0.01080   0.00505  -0.1160   0.4854   1.0000
   3.750   0.9979   0.01093   0.00514  -0.1131   0.4804   1.0000
   4.000   1.0099   0.01101   0.00523  -0.1101   0.4748   1.0000
   4.250   1.0181   0.01112   0.00530  -0.1063   0.4695   1.0000
   4.500   1.0275   0.01124   0.00539  -0.1027   0.4642   1.0000
   4.750   1.0390   0.01134   0.00550  -0.0996   0.4586   1.0000
   5.000   1.0509   0.01151   0.00563  -0.0966   0.4532   1.0000
   5.250   1.0648   0.01168   0.00579  -0.0941   0.4481   1.0000
   5.500   1.0796   0.01183   0.00595  -0.0918   0.4424   1.0000
   5.750   1.0935   0.01206   0.00613  -0.0893   0.4368   1.0000
   6.000   1.1093   0.01226   0.00634  -0.0873   0.4312   1.0000
   6.250   1.1248   0.01248   0.00656  -0.0852   0.4251   1.0000
   6.500   1.1390   0.01279   0.00681  -0.0829   0.4194   1.0000
   6.750   1.1563   0.01300   0.00707  -0.0813   0.4133   1.0000
   7.000   1.1714   0.01330   0.00736  -0.0793   0.4073   1.0000
   7.250   1.1862   0.01362   0.00767  -0.0773   0.3999   1.0000
   7.500   1.2008   0.01397   0.00801  -0.0754   0.3928   1.0000
   7.750   1.2152   0.01436   0.00839  -0.0734   0.3855   1.0000
   8.000   1.2290   0.01478   0.00880  -0.0715   0.3772   1.0000
   8.250   1.2427   0.01524   0.00924  -0.0696   0.3688   1.0000
   8.500   1.2563   0.01573   0.00973  -0.0677   0.3613   1.0000
   8.750   1.2705   0.01624   0.01024  -0.0660   0.3537   1.0000
   9.000   1.2843   0.01679   0.01079  -0.0644   0.3467   1.0000
   9.250   1.2973   0.01740   0.01140  -0.0627   0.3389   1.0000
   9.500   1.3078   0.01815   0.01212  -0.0607   0.3294   1.0000
   9.750   1.3213   0.01881   0.01280  -0.0592   0.3211   1.0000
  10.000   1.3304   0.01970   0.01366  -0.0573   0.3129   1.0000
  10.250   1.3433   0.02046   0.01444  -0.0559   0.3038   1.0000
  10.500   1.3522   0.02146   0.01542  -0.0541   0.2941   1.0000
  10.750   1.3589   0.02264   0.01657  -0.0523   0.2833   1.0000
  11.000   1.3650   0.02391   0.01782  -0.0505   0.2697   1.0000
  11.250   1.3685   0.02542   0.01928  -0.0486   0.2550   1.0000
  11.500   1.3685   0.02725   0.02103  -0.0465   0.2384   1.0000
  11.750   1.3685   0.02916   0.02288  -0.0446   0.2208   1.0000
  12.000   1.3596   0.03183   0.02542  -0.0423   0.1973   1.0000
  12.250   1.3484   0.03481   0.02826  -0.0400   0.1711   1.0000
  12.500   1.3246   0.03899   0.03222  -0.0373   0.1346   1.0000
  12.750   1.2996   0.04353   0.03658  -0.0350   0.1026   1.0000
  13.000   1.2669   0.04908   0.04195  -0.0328   0.0625   1.0000
  13.250   1.2429   0.05408   0.04688  -0.0314   0.0322   1.0000
  13.500   1.2344   0.05770   0.05051  -0.0307   0.0229   1.0000
  13.750   1.2332   0.06061   0.05349  -0.0302   0.0208   1.0000
  14.000   1.2314   0.06365   0.05660  -0.0299   0.0193   1.0000
  14.250   1.2308   0.06659   0.05964  -0.0297   0.0184   1.0000
  14.500   1.2309   0.06951   0.06264  -0.0295   0.0180   1.0000
  14.750   1.2296   0.07263   0.06586  -0.0294   0.0175   1.0000
  15.000   1.2271   0.07594   0.06926  -0.0294   0.0169   1.0000
  15.250   1.2220   0.07960   0.07302  -0.0295   0.0165   1.0000
  15.500   1.2165   0.08337   0.07688  -0.0297   0.0162   1.0000
  15.750   1.2089   0.08749   0.08111  -0.0299   0.0159   1.0000
  16.000   1.1977   0.09217   0.08589  -0.0304   0.0155   1.0000
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