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GOE 600 AIRFOIL (goe600-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 600 AIRFOIL (goe600-il)
Reynolds number: 500,000
Max Cl/Cd: 76.78 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe600-il-500000-n5.txt
Download as CSV file: xf-goe600-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 600 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -0.8212   0.13945   0.13678   0.0013   1.0000   0.0082
 -17.000  -0.8526   0.12801   0.12521  -0.0046   1.0000   0.0082
 -16.750  -0.8815   0.11763   0.11472  -0.0100   1.0000   0.0081
 -16.500  -0.9123   0.10725   0.10421  -0.0154   1.0000   0.0081
 -16.250  -0.9433   0.09707   0.09388  -0.0207   1.0000   0.0080
 -16.000  -0.9741   0.08723   0.08390  -0.0260   1.0000   0.0080
 -15.750  -1.0029   0.07805   0.07457  -0.0312   1.0000   0.0079
 -15.500  -1.0278   0.06969   0.06605  -0.0361   1.0000   0.0079
 -15.250  -1.0487   0.06218   0.05837  -0.0407   1.0000   0.0079
 -15.000  -1.0653   0.05556   0.05160  -0.0449   1.0000   0.0079
 -14.750  -1.0779   0.04978   0.04566  -0.0487   1.0000   0.0080
 -14.500  -1.0865   0.04486   0.04060  -0.0519   1.0000   0.0080
 -14.250  -1.0911   0.04072   0.03632  -0.0545   1.0000   0.0081
 -14.000  -1.0929   0.03729   0.03273  -0.0564   1.0000   0.0082
 -13.750  -1.0926   0.03451   0.02982  -0.0574   1.0000   0.0083
 -13.500  -1.0907   0.03225   0.02744  -0.0575   1.0000   0.0085
 -13.250  -1.0876   0.03041   0.02549  -0.0568   1.0000   0.0086
 -13.000  -1.0833   0.02892   0.02389  -0.0553   1.0000   0.0088
 -12.750  -1.0779   0.02766   0.02252  -0.0533   1.0000   0.0089
 -12.500  -1.0673   0.02650   0.02125  -0.0519   1.0000   0.0092
 -12.250  -1.0539   0.02544   0.02008  -0.0507   1.0000   0.0095
 -12.000  -1.0388   0.02448   0.01901  -0.0496   1.0000   0.0098
 -11.750  -1.0223   0.02360   0.01801  -0.0485   1.0000   0.0100
 -11.500  -1.0072   0.02256   0.01688  -0.0473   1.0000   0.0104
 -11.250  -0.9913   0.02161   0.01586  -0.0461   1.0000   0.0108
 -11.000  -0.9742   0.02083   0.01503  -0.0449   1.0000   0.0112
 -10.750  -0.9489   0.02004   0.01415  -0.0453   0.9948   0.0117
 -10.500  -0.9214   0.01927   0.01329  -0.0460   0.9878   0.0123
 -10.250  -0.8934   0.01856   0.01247  -0.0468   0.9806   0.0128
  -9.750  -0.8390   0.01714   0.01091  -0.0478   0.9641   0.0145
  -9.500  -0.8126   0.01656   0.01027  -0.0480   0.9556   0.0156
  -9.250  -0.7867   0.01605   0.00968  -0.0480   0.9470   0.0168
  -9.000  -0.7623   0.01554   0.00911  -0.0476   0.9378   0.0182
  -8.750  -0.7379   0.01507   0.00859  -0.0472   0.9292   0.0201
  -8.500  -0.7132   0.01467   0.00813  -0.0468   0.9201   0.0221
  -8.250  -0.6886   0.01428   0.00771  -0.0463   0.9118   0.0253
  -8.000  -0.6633   0.01395   0.00733  -0.0460   0.9035   0.0285
  -7.750  -0.6379   0.01361   0.00697  -0.0457   0.8959   0.0320
  -7.500  -0.6117   0.01336   0.00664  -0.0454   0.8876   0.0347
  -7.250  -0.5860   0.01301   0.00628  -0.0452   0.8795   0.0381
  -7.000  -0.5598   0.01276   0.00597  -0.0450   0.8708   0.0413
  -6.750  -0.5329   0.01253   0.00568  -0.0448   0.8621   0.0435
  -6.500  -0.5069   0.01219   0.00529  -0.0446   0.8536   0.0473
  -6.250  -0.4800   0.01192   0.00498  -0.0445   0.8444   0.0507
  -6.000  -0.4529   0.01171   0.00469  -0.0444   0.8356   0.0535
  -5.750  -0.4262   0.01141   0.00436  -0.0443   0.8259   0.0597
  -5.500  -0.3992   0.01112   0.00407  -0.0443   0.8161   0.0681
  -5.250  -0.3727   0.01078   0.00384  -0.0442   0.8062   0.0928
  -5.000  -0.3450   0.01061   0.00365  -0.0442   0.7962   0.1064
  -4.750  -0.3171   0.01047   0.00347  -0.0443   0.7872   0.1155
  -4.250  -0.2611   0.01020   0.00312  -0.0444   0.7706   0.1283
  -3.750  -0.2048   0.00994   0.00280  -0.0446   0.7558   0.1428
  -3.500  -0.1765   0.00985   0.00266  -0.0447   0.7488   0.1490
  -3.250  -0.1482   0.00971   0.00252  -0.0449   0.7427   0.1577
  -3.000  -0.1200   0.00955   0.00238  -0.0451   0.7368   0.1707
  -2.500  -0.0651   0.00892   0.00210  -0.0454   0.7244   0.2769
  -2.250  -0.0374   0.00871   0.00200  -0.0455   0.7170   0.3231
  -2.000  -0.0097   0.00846   0.00193  -0.0456   0.7099   0.3753
  -1.750   0.0183   0.00829   0.00187  -0.0458   0.7035   0.4168
  -1.500   0.0467   0.00819   0.00183  -0.0459   0.6978   0.4434
  -1.250   0.0752   0.00810   0.00181  -0.0461   0.6913   0.4707
  -0.750   0.1323   0.00798   0.00178  -0.0464   0.6785   0.5182
  -0.500   0.1610   0.00795   0.00177  -0.0466   0.6723   0.5365
  -0.250   0.1897   0.00792   0.00177  -0.0468   0.6671   0.5559
   0.000   0.2185   0.00787   0.00178  -0.0470   0.6613   0.5746
   0.250   0.2471   0.00786   0.00179  -0.0472   0.6556   0.5906
   0.500   0.2759   0.00783   0.00181  -0.0474   0.6497   0.6057
   0.750   0.3045   0.00780   0.00183  -0.0475   0.6431   0.6234
   1.000   0.3329   0.00778   0.00186  -0.0476   0.6366   0.6433
   1.250   0.3612   0.00772   0.00190  -0.0477   0.6287   0.6671
   1.500   0.3890   0.00767   0.00193  -0.0477   0.6190   0.6975
   1.750   0.4161   0.00761   0.00197  -0.0475   0.6028   0.7318
   2.000   0.4430   0.00759   0.00202  -0.0472   0.5837   0.7644
   2.250   0.4697   0.00758   0.00208  -0.0470   0.5662   0.7959
   2.500   0.4956   0.00760   0.00216  -0.0464   0.5465   0.8316
   2.750   0.5202   0.00765   0.00225  -0.0456   0.5194   0.8722
   3.000   0.5439   0.00784   0.00237  -0.0446   0.4797   0.9133
   3.250   0.5710   0.00816   0.00255  -0.0445   0.4384   0.9462
   3.500   0.6029   0.00848   0.00273  -0.0455   0.4079   0.9681
   3.750   0.6362   0.00873   0.00291  -0.0469   0.3863   0.9838
   4.000   0.6702   0.00901   0.00310  -0.0485   0.3643   0.9948
   4.250   0.7009   0.00926   0.00327  -0.0494   0.3452   1.0000
   4.500   0.7255   0.00950   0.00345  -0.0489   0.3269   1.0000
   4.750   0.7501   0.00977   0.00364  -0.0484   0.3059   1.0000
   5.000   0.7743   0.01009   0.00385  -0.0479   0.2817   1.0000
   5.250   0.7980   0.01048   0.00410  -0.0474   0.2525   1.0000
   5.500   0.8221   0.01084   0.00436  -0.0469   0.2295   1.0000
   5.750   0.8465   0.01118   0.00462  -0.0465   0.2112   1.0000
   6.000   0.8709   0.01152   0.00490  -0.0460   0.1939   1.0000
   6.250   0.8951   0.01187   0.00519  -0.0456   0.1778   1.0000
   6.500   0.9190   0.01225   0.00551  -0.0451   0.1609   1.0000
   6.750   0.9420   0.01270   0.00586  -0.0445   0.1409   1.0000
   7.000   0.9647   0.01317   0.00624  -0.0438   0.1204   1.0000
   7.250   0.9863   0.01372   0.00667  -0.0430   0.0990   1.0000
   7.750   1.0315   0.01461   0.00749  -0.0417   0.0797   1.0000
   8.000   1.0537   0.01507   0.00793  -0.0410   0.0724   1.0000
   8.250   1.0761   0.01549   0.00835  -0.0403   0.0638   1.0000
   8.500   1.0964   0.01605   0.00885  -0.0394   0.0486   1.0000
   8.750   1.1146   0.01677   0.00945  -0.0381   0.0361   1.0000
   9.000   1.1343   0.01734   0.01003  -0.0370   0.0316   1.0000
   9.250   1.1530   0.01794   0.01064  -0.0358   0.0285   1.0000
   9.500   1.1717   0.01851   0.01125  -0.0346   0.0262   1.0000
   9.750   1.1899   0.01905   0.01185  -0.0333   0.0243   1.0000
  10.000   1.2047   0.01968   0.01252  -0.0315   0.0224   1.0000
  10.250   1.2186   0.02039   0.01327  -0.0296   0.0208   1.0000
  10.500   1.2346   0.02100   0.01394  -0.0281   0.0195   1.0000
  10.750   1.2494   0.02171   0.01470  -0.0266   0.0180   1.0000
  11.000   1.2626   0.02256   0.01558  -0.0250   0.0166   1.0000
  11.250   1.2761   0.02342   0.01650  -0.0235   0.0156   1.0000
  11.500   1.2896   0.02430   0.01746  -0.0221   0.0147   1.0000
  11.750   1.3021   0.02528   0.01849  -0.0208   0.0138   1.0000
  12.000   1.3135   0.02637   0.01963  -0.0194   0.0131   1.0000
  12.250   1.3225   0.02769   0.02100  -0.0180   0.0123   1.0000
  12.500   1.3330   0.02892   0.02232  -0.0168   0.0119   1.0000
  12.750   1.3428   0.03025   0.02374  -0.0156   0.0114   1.0000
  13.000   1.3520   0.03167   0.02525  -0.0146   0.0108   1.0000
  13.250   1.3602   0.03321   0.02687  -0.0136   0.0104   1.0000
  13.500   1.3670   0.03492   0.02865  -0.0127   0.0100   1.0000
  13.750   1.3719   0.03688   0.03069  -0.0119   0.0096   1.0000
  14.000   1.3735   0.03921   0.03311  -0.0111   0.0093   1.0000
  14.250   1.3766   0.04146   0.03547  -0.0105   0.0091   1.0000
  14.500   1.3795   0.04380   0.03791  -0.0101   0.0089   1.0000
  14.750   1.3811   0.04633   0.04056  -0.0097   0.0087   1.0000
  15.000   1.3811   0.04908   0.04342  -0.0095   0.0085   1.0000
  15.250   1.3801   0.05205   0.04651  -0.0095   0.0083   1.0000
  15.500   1.3780   0.05527   0.04986  -0.0097   0.0081   1.0000
  15.750   1.3749   0.05872   0.05342  -0.0101   0.0080   1.0000
  16.000   1.3703   0.06251   0.05733  -0.0108   0.0078   1.0000
  16.250   1.3651   0.06654   0.06148  -0.0117   0.0077   1.0000
  16.500   1.3583   0.07093   0.06599  -0.0129   0.0076   1.0000
  16.750   1.3501   0.07569   0.07087  -0.0144   0.0075   1.0000
  17.000   1.3408   0.08080   0.07610  -0.0162   0.0074   1.0000
  17.250   1.3300   0.08628   0.08171  -0.0183   0.0073   1.0000
  17.500   1.3176   0.09213   0.08769  -0.0206   0.0072   1.0000
  17.750   1.3040   0.09829   0.09398  -0.0232   0.0071   1.0000
  18.000   1.2894   0.10472   0.10053  -0.0259   0.0071   1.0000
  18.250   1.2749   0.11122   0.10715  -0.0288   0.0070   1.0000
  18.500   1.2595   0.11795   0.11399  -0.0319   0.0070   1.0000
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