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GOE 398 AIRFOIL (goe398-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 398 AIRFOIL (goe398-il)
Reynolds number: 1,000,000
Max Cl/Cd: 120.85 at α=5.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe398-il-1000000.txt
Download as CSV file: xf-goe398-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 398 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
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.8136   0.06152   0.05904  -0.0816   1.0000   0.0193
 -15.000  -0.8891   0.04580   0.04304  -0.0931   1.0000   0.0190
 -14.750  -0.9276   0.03669   0.03370  -0.1014   1.0000   0.0190
 -14.500  -0.9606   0.03297   0.02983  -0.1005   1.0000   0.0189
 -14.250  -0.9870   0.03129   0.02804  -0.0953   0.9997   0.0190
 -14.000  -0.9659   0.02977   0.02638  -0.0971   0.9970   0.0193
 -13.750  -0.9414   0.02812   0.02458  -0.0991   0.9943   0.0196
 -13.500  -0.9169   0.02687   0.02320  -0.1003   0.9913   0.0198
 -13.250  -0.8994   0.02467   0.02082  -0.1013   0.9870   0.0203
 -13.000  -0.8727   0.02344   0.01951  -0.1027   0.9846   0.0206
 -12.750  -0.8409   0.02281   0.01886  -0.1042   0.9832   0.0210
 -12.500  -0.8171   0.02207   0.01807  -0.1042   0.9784   0.0214
 -12.250  -0.7890   0.02134   0.01727  -0.1049   0.9749   0.0217
 -12.000  -0.7593   0.02055   0.01639  -0.1060   0.9725   0.0222
 -11.750  -0.7280   0.01982   0.01557  -0.1073   0.9706   0.0227
 -11.500  -0.7036   0.01933   0.01499  -0.1068   0.9636   0.0231
 -11.250  -0.6738   0.01832   0.01384  -0.1080   0.9596   0.0236
 -11.000  -0.6398   0.01730   0.01277  -0.1100   0.9567   0.0242
 -10.750  -0.6112   0.01680   0.01224  -0.1105   0.9481   0.0246
 -10.500  -0.5754   0.01627   0.01166  -0.1124   0.9426   0.0251
 -10.250  -0.5454   0.01575   0.01106  -0.1130   0.9327   0.0257
 -10.000  -0.5138   0.01529   0.01049  -0.1140   0.9232   0.0262
  -9.750  -0.4857   0.01489   0.00998  -0.1141   0.9114   0.0267
  -9.500  -0.4593   0.01467   0.00965  -0.1137   0.8993   0.0270
  -9.250  -0.4397   0.01377   0.00865  -0.1124   0.8865   0.0279
  -9.000  -0.4159   0.01343   0.00824  -0.1116   0.8749   0.0284
  -8.750  -0.3929   0.01314   0.00790  -0.1106   0.8632   0.0290
  -8.500  -0.3695   0.01285   0.00753  -0.1096   0.8526   0.0295
  -8.250  -0.3459   0.01259   0.00717  -0.1086   0.8419   0.0301
  -8.000  -0.3218   0.01237   0.00688  -0.1077   0.8323   0.0307
  -7.500  -0.2768   0.01157   0.00593  -0.1054   0.8138   0.0320
  -7.000  -0.2293   0.01103   0.00529  -0.1035   0.7964   0.0333
  -6.750  -0.2051   0.01082   0.00502  -0.1026   0.7878   0.0341
  -6.500  -0.1801   0.01061   0.00476  -0.1018   0.7798   0.0348
  -6.250  -0.1552   0.01046   0.00454  -0.1010   0.7713   0.0355
  -6.000  -0.1316   0.01014   0.00417  -0.1000   0.7631   0.0364
  -5.750  -0.1077   0.00987   0.00386  -0.0990   0.7544   0.0374
  -5.500  -0.0827   0.00969   0.00365  -0.0982   0.7464   0.0384
  -5.250  -0.0573   0.00954   0.00346  -0.0975   0.7386   0.0396
  -5.000  -0.0317   0.00943   0.00329  -0.0968   0.7316   0.0407
  -4.750  -0.0069   0.00918   0.00302  -0.0960   0.7243   0.0423
  -4.500   0.0181   0.00904   0.00285  -0.0952   0.7169   0.0441
  -4.250   0.0442   0.00891   0.00270  -0.0946   0.7097   0.0459
  -4.000   0.0693   0.00876   0.00252  -0.0939   0.7022   0.0487
  -3.750   0.0951   0.00864   0.00239  -0.0932   0.6954   0.0523
  -3.500   0.1207   0.00850   0.00226  -0.0926   0.6884   0.0584
  -3.250   0.1458   0.00839   0.00215  -0.0918   0.6814   0.0666
  -3.000   0.1719   0.00826   0.00205  -0.0912   0.6746   0.0766
  -2.750   0.1973   0.00817   0.00196  -0.0905   0.6674   0.0865
  -2.500   0.2229   0.00807   0.00188  -0.0899   0.6609   0.0983
  -2.000   0.2730   0.00784   0.00176  -0.0884   0.6466   0.1441
  -1.750   0.2988   0.00772   0.00174  -0.0879   0.6397   0.1726
  -1.500   0.3243   0.00768   0.00171  -0.0872   0.6322   0.1914
  -1.250   0.3502   0.00763   0.00169  -0.0866   0.6249   0.2076
  -1.000   0.3756   0.00758   0.00166  -0.0860   0.6165   0.2240
  -0.750   0.4009   0.00753   0.00164  -0.0853   0.6084   0.2436
  -0.500   0.4249   0.00741   0.00163  -0.0844   0.5988   0.2871
  -0.250   0.4466   0.00714   0.00164  -0.0831   0.5884   0.3932
   0.000   0.4684   0.00700   0.00166  -0.0818   0.5761   0.4669
   0.250   0.4900   0.00687   0.00169  -0.0804   0.5621   0.5419
   0.500   0.5108   0.00675   0.00173  -0.0788   0.5465   0.6139
   0.750   0.5284   0.00660   0.00177  -0.0765   0.5288   0.7022
   1.250   0.6727   0.00677   0.00230  -0.0958   0.4718   0.9827
   1.500   0.7147   0.00701   0.00242  -0.0989   0.4546   0.9897
   1.750   0.7574   0.00724   0.00255  -0.1021   0.4410   0.9951
   2.000   0.8023   0.00738   0.00262  -0.1059   0.4302   0.9988
   2.250   0.8342   0.00751   0.00269  -0.1068   0.4219   1.0000
   2.500   0.8563   0.00763   0.00276  -0.1055   0.4146   1.0000
   2.750   0.8777   0.00777   0.00285  -0.1042   0.4072   1.0000
   3.000   0.9006   0.00787   0.00293  -0.1031   0.4008   1.0000
   3.250   0.9223   0.00801   0.00303  -0.1018   0.3941   1.0000
   3.500   0.9447   0.00813   0.00312  -0.1006   0.3884   1.0000
   3.750   0.9674   0.00824   0.00322  -0.0995   0.3827   1.0000
   4.000   0.9889   0.00839   0.00333  -0.0982   0.3763   1.0000
   4.250   1.0113   0.00851   0.00344  -0.0970   0.3709   1.0000
   4.500   1.0337   0.00864   0.00355  -0.0959   0.3647   1.0000
   4.750   1.0545   0.00882   0.00369  -0.0944   0.3579   1.0000
   5.000   1.0771   0.00893   0.00380  -0.0933   0.3522   1.0000
   5.250   1.0982   0.00909   0.00394  -0.0919   0.3445   1.0000
   5.500   1.1191   0.00926   0.00408  -0.0905   0.3363   1.0000
   5.750   1.1381   0.00950   0.00425  -0.0888   0.3240   1.0000
   6.000   1.1584   0.00969   0.00441  -0.0873   0.3130   1.0000
   6.250   1.1775   0.00991   0.00459  -0.0856   0.3021   1.0000
   6.500   1.1954   0.01018   0.00480  -0.0837   0.2916   1.0000
   6.750   1.2140   0.01041   0.00500  -0.0819   0.2812   1.0000
   7.000   1.2308   0.01067   0.00522  -0.0798   0.2715   1.0000
   7.250   1.2434   0.01096   0.00546  -0.0768   0.2607   1.0000
   7.500   1.2589   0.01119   0.00566  -0.0744   0.2522   1.0000
   7.750   1.2728   0.01149   0.00593  -0.0718   0.2432   1.0000
   8.000   1.2881   0.01178   0.00619  -0.0695   0.2346   1.0000
   8.250   1.3036   0.01209   0.00648  -0.0673   0.2269   1.0000
   8.500   1.3196   0.01241   0.00678  -0.0653   0.2196   1.0000
   8.750   1.3357   0.01275   0.00711  -0.0633   0.2131   1.0000
   9.000   1.3529   0.01306   0.00741  -0.0615   0.2075   1.0000
   9.250   1.3675   0.01350   0.00782  -0.0594   0.1997   1.0000
   9.500   1.3853   0.01382   0.00815  -0.0579   0.1948   1.0000
   9.750   1.4013   0.01423   0.00855  -0.0561   0.1891   1.0000
  10.000   1.4172   0.01466   0.00898  -0.0544   0.1837   1.0000
  10.250   1.4341   0.01506   0.00939  -0.0529   0.1783   1.0000
  10.500   1.4475   0.01564   0.00994  -0.0509   0.1708   1.0000
  10.750   1.4638   0.01610   0.01041  -0.0494   0.1644   1.0000
  11.000   1.4765   0.01676   0.01104  -0.0475   0.1562   1.0000
  11.250   1.4885   0.01748   0.01172  -0.0457   0.1455   1.0000
  11.500   1.4962   0.01847   0.01263  -0.0434   0.1280   1.0000
  11.750   1.4884   0.02043   0.01433  -0.0395   0.0922   1.0000
  12.000   1.4796   0.02260   0.01636  -0.0359   0.0687   1.0000
  12.250   1.4841   0.02403   0.01777  -0.0339   0.0616   1.0000
  12.500   1.4910   0.02535   0.01910  -0.0322   0.0571   1.0000
  12.750   1.4978   0.02671   0.02049  -0.0307   0.0542   1.0000
  13.000   1.5033   0.02823   0.02203  -0.0292   0.0513   1.0000
  13.250   1.5131   0.02946   0.02331  -0.0281   0.0499   1.0000
  13.500   1.5204   0.03090   0.02480  -0.0269   0.0483   1.0000
  13.750   1.5258   0.03256   0.02649  -0.0258   0.0468   1.0000
  14.000   1.5288   0.03448   0.02846  -0.0246   0.0451   1.0000
  14.250   1.5345   0.03621   0.03026  -0.0237   0.0441   1.0000
  14.500   1.5419   0.03783   0.03194  -0.0229   0.0433   1.0000
  14.750   1.5474   0.03967   0.03384  -0.0222   0.0422   1.0000
  15.000   1.5512   0.04174   0.03597  -0.0216   0.0414   1.0000
  15.250   1.5524   0.04410   0.03838  -0.0210   0.0404   1.0000
  15.500   1.5518   0.04672   0.04106  -0.0204   0.0396   1.0000
  15.750   1.5472   0.04986   0.04428  -0.0200   0.0385   1.0000
  16.000   1.5508   0.05217   0.04667  -0.0198   0.0381   1.0000
  16.250   1.5526   0.05470   0.04928  -0.0196   0.0376   1.0000
  16.500   1.5542   0.05732   0.05197  -0.0196   0.0370   1.0000
  16.750   1.5534   0.06027   0.05500  -0.0196   0.0363   1.0000
  17.000   1.5515   0.06341   0.05820  -0.0198   0.0356   1.0000
  17.250   1.5457   0.06709   0.06196  -0.0201   0.0351   1.0000
  17.500   1.5384   0.07105   0.06600  -0.0206   0.0345   1.0000
  17.750   1.5283   0.07548   0.07052  -0.0213   0.0339   1.0000
  18.000   1.5140   0.08057   0.07570  -0.0223   0.0332   1.0000
  18.250   1.5090   0.08443   0.07966  -0.0231   0.0330   1.0000
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