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GOE 623 AIRFOIL (goe623-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 623 AIRFOIL (goe623-il)
Reynolds number: 1,000,000
Max Cl/Cd: 104.37 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe623-il-1000000-n5.txt
Download as CSV file: xf-goe623-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 623 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -1.1036   0.03693   0.03401  -0.0843   1.0000   0.0076
 -15.000  -1.1192   0.03323   0.03013  -0.0847   1.0000   0.0076
 -14.750  -1.1193   0.03096   0.02770  -0.0838   1.0000   0.0077
 -14.500  -1.1125   0.02914   0.02574  -0.0829   1.0000   0.0078
 -14.250  -1.1037   0.02750   0.02396  -0.0818   1.0000   0.0079
 -14.000  -1.0937   0.02597   0.02232  -0.0805   1.0000   0.0081
 -13.750  -1.0819   0.02471   0.02095  -0.0791   1.0000   0.0084
 -13.500  -1.0688   0.02362   0.01978  -0.0775   1.0000   0.0086
 -13.250  -1.0501   0.02260   0.01866  -0.0769   0.9991   0.0089
 -13.000  -1.0232   0.02156   0.01753  -0.0779   0.9965   0.0092
 -12.500  -0.9683   0.01976   0.01552  -0.0796   0.9903   0.0099
 -12.250  -0.9398   0.01897   0.01463  -0.0805   0.9859   0.0102
 -12.000  -0.9117   0.01818   0.01376  -0.0812   0.9789   0.0107
 -11.750  -0.8821   0.01752   0.01304  -0.0821   0.9693   0.0113
 -11.500  -0.8536   0.01694   0.01240  -0.0826   0.9559   0.0119
 -11.250  -0.8275   0.01642   0.01178  -0.0826   0.9406   0.0124
 -11.000  -0.8030   0.01594   0.01117  -0.0821   0.9248   0.0129
 -10.750  -0.7787   0.01549   0.01062  -0.0816   0.9102   0.0134
 -10.500  -0.7535   0.01515   0.01021  -0.0812   0.8984   0.0140
 -10.250  -0.7276   0.01485   0.00985  -0.0809   0.8889   0.0146
 -10.000  -0.7015   0.01454   0.00948  -0.0807   0.8809   0.0153
  -9.750  -0.6752   0.01423   0.00909  -0.0805   0.8731   0.0159
  -9.500  -0.6488   0.01393   0.00869  -0.0803   0.8664   0.0164
  -9.250  -0.6224   0.01359   0.00831  -0.0801   0.8592   0.0171
  -9.000  -0.5954   0.01337   0.00805  -0.0799   0.8525   0.0177
  -8.750  -0.5681   0.01314   0.00778  -0.0799   0.8460   0.0182
  -8.500  -0.5410   0.01292   0.00750  -0.0797   0.8398   0.0188
  -8.250  -0.5136   0.01270   0.00722  -0.0797   0.8341   0.0194
  -8.000  -0.4862   0.01248   0.00694  -0.0796   0.8274   0.0200
  -7.750  -0.4587   0.01228   0.00667  -0.0795   0.8210   0.0205
  -7.500  -0.4310   0.01207   0.00640  -0.0794   0.8147   0.0207
  -7.250  -0.4046   0.01160   0.00588  -0.0793   0.8083   0.0215
  -7.000  -0.3771   0.01135   0.00559  -0.0792   0.8024   0.0221
  -6.750  -0.3493   0.01113   0.00533  -0.0792   0.7954   0.0227
  -6.500  -0.3217   0.01092   0.00507  -0.0791   0.7883   0.0233
  -6.250  -0.2939   0.01071   0.00481  -0.0791   0.7802   0.0239
  -6.000  -0.2662   0.01050   0.00454  -0.0790   0.7721   0.0245
  -5.750  -0.2383   0.01029   0.00427  -0.0790   0.7634   0.0250
  -5.500  -0.2103   0.01013   0.00405  -0.0790   0.7545   0.0254
  -5.250  -0.1824   0.00996   0.00382  -0.0789   0.7438   0.0257
  -5.000  -0.1545   0.00980   0.00360  -0.0789   0.7317   0.0259
  -4.750  -0.1272   0.00951   0.00322  -0.0787   0.7174   0.0267
  -4.500  -0.0996   0.00932   0.00295  -0.0786   0.7014   0.0276
  -4.250  -0.0719   0.00919   0.00274  -0.0786   0.6856   0.0283
  -4.000  -0.0441   0.00908   0.00256  -0.0785   0.6706   0.0288
  -3.750  -0.0161   0.00898   0.00239  -0.0785   0.6568   0.0294
  -3.500   0.0119   0.00890   0.00225  -0.0784   0.6440   0.0301
  -3.250   0.0399   0.00883   0.00211  -0.0784   0.6323   0.0308
  -3.000   0.0681   0.00876   0.00199  -0.0784   0.6217   0.0315
  -2.750   0.0964   0.00870   0.00189  -0.0785   0.6135   0.0321
  -2.500   0.1247   0.00863   0.00178  -0.0785   0.6049   0.0339
  -2.250   0.1531   0.00855   0.00169  -0.0786   0.5974   0.0369
  -2.000   0.1814   0.00848   0.00161  -0.0786   0.5897   0.0420
  -1.750   0.2093   0.00832   0.00152  -0.0787   0.5816   0.0701
  -1.500   0.2372   0.00825   0.00146  -0.0787   0.5707   0.0882
  -1.250   0.2652   0.00814   0.00144  -0.0787   0.5599   0.1232
  -1.000   0.2935   0.00813   0.00143  -0.0788   0.5509   0.1361
  -0.750   0.3217   0.00813   0.00141  -0.0788   0.5403   0.1447
  -0.500   0.3499   0.00815   0.00140  -0.0789   0.5281   0.1506
  -0.250   0.3781   0.00816   0.00139  -0.0790   0.5168   0.1593
   0.000   0.4062   0.00818   0.00139  -0.0790   0.5078   0.1685
   0.250   0.4347   0.00815   0.00139  -0.0791   0.5016   0.1804
   0.500   0.4629   0.00808   0.00140  -0.0792   0.4950   0.2107
   0.750   0.4908   0.00798   0.00143  -0.0793   0.4888   0.2636
   1.000   0.5188   0.00788   0.00146  -0.0794   0.4804   0.3195
   1.250   0.5463   0.00773   0.00150  -0.0795   0.4714   0.4004
   1.500   0.5733   0.00751   0.00156  -0.0795   0.4614   0.5144
   1.750   0.5999   0.00722   0.00163  -0.0795   0.4521   0.6514
   2.000   0.6258   0.00703   0.00172  -0.0791   0.4414   0.7559
   2.250   0.6508   0.00694   0.00181  -0.0785   0.4284   0.8363
   2.500   0.6736   0.00691   0.00192  -0.0772   0.4124   0.9106
   2.750   0.7009   0.00705   0.00203  -0.0770   0.3885   0.9622
   3.000   0.7347   0.00734   0.00217  -0.0784   0.3577   0.9877
   3.250   0.7673   0.00762   0.00232  -0.0797   0.3326   1.0000
   3.500   0.7928   0.00786   0.00246  -0.0793   0.3140   1.0000
   3.750   0.8185   0.00809   0.00261  -0.0790   0.2977   1.0000
   4.000   0.8443   0.00831   0.00276  -0.0787   0.2831   1.0000
   4.250   0.8703   0.00853   0.00291  -0.0784   0.2696   1.0000
   4.500   0.8962   0.00876   0.00307  -0.0782   0.2573   1.0000
   4.750   0.9221   0.00899   0.00325  -0.0779   0.2455   1.0000
   5.000   0.9479   0.00922   0.00342  -0.0776   0.2340   1.0000
   5.250   0.9739   0.00943   0.00360  -0.0774   0.2241   1.0000
   5.500   0.9996   0.00967   0.00379  -0.0771   0.2153   1.0000
   5.750   1.0257   0.00987   0.00397  -0.0769   0.2084   1.0000
   6.000   1.0513   0.01010   0.00417  -0.0766   0.2015   1.0000
   6.250   1.0771   0.01032   0.00438  -0.0764   0.1942   1.0000
   6.500   1.1022   0.01058   0.00460  -0.0760   0.1870   1.0000
   6.750   1.1276   0.01082   0.00482  -0.0758   0.1798   1.0000
   7.000   1.1523   0.01111   0.00507  -0.0754   0.1716   1.0000
   7.250   1.1773   0.01136   0.00531  -0.0750   0.1651   1.0000
   7.500   1.2016   0.01166   0.00558  -0.0746   0.1583   1.0000
   7.750   1.2265   0.01189   0.00582  -0.0742   0.1531   1.0000
   8.000   1.2501   0.01223   0.00612  -0.0737   0.1453   1.0000
   8.250   1.2743   0.01250   0.00639  -0.0732   0.1389   1.0000
   8.500   1.2968   0.01288   0.00672  -0.0726   0.1289   1.0000
   8.750   1.3181   0.01334   0.00710  -0.0717   0.1146   1.0000
   9.000   1.3271   0.01464   0.00807  -0.0690   0.0652   1.0000
   9.250   1.3427   0.01542   0.00877  -0.0673   0.0488   1.0000
   9.500   1.3602   0.01602   0.00934  -0.0658   0.0405   1.0000
   9.750   1.3761   0.01664   0.00993  -0.0641   0.0322   1.0000
  10.000   1.3884   0.01737   0.01060  -0.0618   0.0227   1.0000
  10.250   1.4015   0.01808   0.01129  -0.0597   0.0171   1.0000
  10.500   1.4162   0.01872   0.01195  -0.0580   0.0149   1.0000
  10.750   1.4310   0.01938   0.01263  -0.0564   0.0133   1.0000
  11.000   1.4460   0.02004   0.01333  -0.0549   0.0124   1.0000
  11.250   1.4597   0.02080   0.01412  -0.0533   0.0114   1.0000
  11.500   1.4725   0.02165   0.01501  -0.0517   0.0105   1.0000
  11.750   1.4865   0.02244   0.01586  -0.0503   0.0101   1.0000
  12.000   1.4995   0.02333   0.01679  -0.0489   0.0095   1.0000
  12.250   1.5114   0.02433   0.01784  -0.0476   0.0090   1.0000
  12.500   1.5221   0.02544   0.01899  -0.0462   0.0085   1.0000
  12.750   1.5315   0.02671   0.02031  -0.0448   0.0080   1.0000
  13.000   1.5420   0.02791   0.02158  -0.0436   0.0078   1.0000
  13.250   1.5518   0.02921   0.02295  -0.0425   0.0076   1.0000
  13.500   1.5607   0.03063   0.02443  -0.0414   0.0073   1.0000
  13.750   1.5684   0.03218   0.02604  -0.0404   0.0070   1.0000
  14.000   1.5751   0.03387   0.02780  -0.0394   0.0068   1.0000
  14.250   1.5806   0.03572   0.02972  -0.0386   0.0066   1.0000
  14.500   1.5846   0.03777   0.03184  -0.0377   0.0064   1.0000
  14.750   1.5868   0.04007   0.03421  -0.0370   0.0062   1.0000
  15.000   1.5869   0.04266   0.03690  -0.0364   0.0060   1.0000
  15.250   1.5891   0.04513   0.03945  -0.0360   0.0059   1.0000
  15.500   1.5906   0.04774   0.04214  -0.0358   0.0057   1.0000
  15.750   1.5908   0.05059   0.04508  -0.0357   0.0056   1.0000
  16.000   1.5899   0.05366   0.04825  -0.0357   0.0055   1.0000
  16.250   1.5883   0.05689   0.05156  -0.0359   0.0054   1.0000
  16.500   1.5851   0.06034   0.05511  -0.0362   0.0053   1.0000
  16.750   1.5804   0.06409   0.05896  -0.0366   0.0052   1.0000
  17.000   1.5744   0.06810   0.06307  -0.0373   0.0051   1.0000
  17.250   1.5671   0.07234   0.06740  -0.0380   0.0050   1.0000
  17.500   1.5583   0.07683   0.07200  -0.0389   0.0049   1.0000
  17.750   1.5481   0.08165   0.07692  -0.0400   0.0049   1.0000
  18.000   1.5365   0.08681   0.08219  -0.0413   0.0048   1.0000
  18.250   1.5239   0.09217   0.08767  -0.0428   0.0047   1.0000
  18.500   1.5098   0.09788   0.09349  -0.0446   0.0047   1.0000
  18.750   1.4946   0.10390   0.09963  -0.0466   0.0047   1.0000
  19.000   1.4792   0.11007   0.10591  -0.0487   0.0046   1.0000
  19.250   1.4627   0.11647   0.11243  -0.0511   0.0046   1.0000
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