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GOE 655 AIRFOIL (goe655-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 655 AIRFOIL (goe655-il)
Reynolds number: 1,000,000
Max Cl/Cd: 115.68 at α=7.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe655-il-1000000.txt
Download as CSV file: xf-goe655-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 655 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
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.7321   0.08339   0.08114  -0.0623   1.0000   0.0185
 -15.500  -0.8316   0.06418   0.06166  -0.0749   1.0000   0.0183
 -15.250  -0.8821   0.05329   0.05060  -0.0823   1.0000   0.0182
 -15.000  -0.9161   0.04470   0.04183  -0.0885   1.0000   0.0182
 -14.750  -0.9390   0.03766   0.03462  -0.0945   1.0000   0.0183
 -14.500  -0.9555   0.03339   0.03020  -0.0971   1.0000   0.0183
 -14.250  -0.9833   0.03083   0.02752  -0.0944   1.0000   0.0183
 -14.000  -1.0133   0.02996   0.02660  -0.0871   1.0000   0.0184
 -13.750  -0.9969   0.02909   0.02563  -0.0869   0.9988   0.0186
 -13.500  -0.9794   0.02647   0.02282  -0.0892   0.9957   0.0191
 -13.250  -0.9519   0.02543   0.02174  -0.0908   0.9940   0.0195
 -13.000  -0.9252   0.02476   0.02104  -0.0916   0.9917   0.0199
 -12.750  -0.8975   0.02415   0.02040  -0.0924   0.9893   0.0202
 -12.500  -0.8692   0.02344   0.01962  -0.0935   0.9871   0.0206
 -12.250  -0.8403   0.02259   0.01868  -0.0947   0.9853   0.0211
 -12.000  -0.8097   0.02183   0.01782  -0.0961   0.9839   0.0216
 -11.750  -0.7775   0.02119   0.01707  -0.0976   0.9828   0.0220
 -11.500  -0.7521   0.02065   0.01645  -0.0976   0.9792   0.0222
 -11.250  -0.7296   0.01906   0.01475  -0.0980   0.9756   0.0230
 -11.000  -0.6978   0.01857   0.01426  -0.0992   0.9738   0.0235
 -10.750  -0.6643   0.01815   0.01381  -0.1006   0.9724   0.0240
 -10.500  -0.6298   0.01760   0.01321  -0.1023   0.9711   0.0246
 -10.250  -0.5955   0.01702   0.01255  -0.1039   0.9695   0.0252
 -10.000  -0.5711   0.01653   0.01199  -0.1034   0.9632   0.0257
  -9.750  -0.5395   0.01623   0.01161  -0.1042   0.9592   0.0261
  -9.500  -0.5104   0.01503   0.01030  -0.1051   0.9555   0.0269
  -9.250  -0.4876   0.01454   0.00980  -0.1042   0.9478   0.0274
  -9.000  -0.4585   0.01413   0.00935  -0.1045   0.9420   0.0280
  -8.750  -0.4330   0.01377   0.00894  -0.1040   0.9340   0.0285
  -8.500  -0.4056   0.01343   0.00854  -0.1039   0.9254   0.0292
  -8.250  -0.3809   0.01313   0.00818  -0.1032   0.9147   0.0298
  -8.000  -0.3549   0.01282   0.00778  -0.1026   0.9042   0.0304
  -7.750  -0.3292   0.01257   0.00743  -0.1020   0.8917   0.0307
  -7.500  -0.3083   0.01181   0.00658  -0.1007   0.8772   0.0315
  -7.250  -0.2846   0.01144   0.00616  -0.0998   0.8612   0.0323
  -7.000  -0.2601   0.01122   0.00586  -0.0990   0.8434   0.0330
  -6.750  -0.2357   0.01100   0.00555  -0.0981   0.8255   0.0337
  -6.500  -0.2113   0.01078   0.00524  -0.0972   0.8083   0.0344
  -6.250  -0.1867   0.01059   0.00495  -0.0964   0.7917   0.0350
  -5.750  -0.1371   0.01022   0.00440  -0.0948   0.7622   0.0363
  -5.500  -0.1134   0.00985   0.00397  -0.0939   0.7494   0.0375
  -5.250  -0.0882   0.00969   0.00374  -0.0932   0.7375   0.0386
  -4.750  -0.0365   0.00941   0.00335  -0.0920   0.7165   0.0407
  -4.500  -0.0104   0.00931   0.00319  -0.0914   0.7071   0.0416
  -4.250   0.0154   0.00909   0.00292  -0.0909   0.6976   0.0434
  -4.000   0.0414   0.00894   0.00275  -0.0903   0.6886   0.0455
  -3.750   0.0678   0.00884   0.00261  -0.0898   0.6787   0.0476
  -3.500   0.0943   0.00873   0.00245  -0.0893   0.6689   0.0499
  -3.250   0.1199   0.00859   0.00229  -0.0887   0.6580   0.0542
  -3.000   0.1463   0.00848   0.00216  -0.0882   0.6458   0.0595
  -2.750   0.1723   0.00836   0.00203  -0.0877   0.6338   0.0689
  -2.500   0.1975   0.00818   0.00190  -0.0870   0.6207   0.0915
  -2.250   0.2218   0.00794   0.00181  -0.0863   0.6066   0.1435
  -2.000   0.2468   0.00782   0.00175  -0.0856   0.5913   0.1797
  -1.750   0.2720   0.00775   0.00171  -0.0850   0.5752   0.2111
  -1.500   0.2971   0.00770   0.00169  -0.0843   0.5587   0.2417
  -1.250   0.3223   0.00767   0.00168  -0.0837   0.5420   0.2719
  -1.000   0.3474   0.00766   0.00168  -0.0830   0.5244   0.3013
  -0.750   0.3724   0.00769   0.00170  -0.0823   0.5051   0.3298
  -0.500   0.3972   0.00770   0.00172  -0.0816   0.4856   0.3617
  -0.250   0.4217   0.00771   0.00176  -0.0809   0.4667   0.4006
   0.000   0.4457   0.00771   0.00181  -0.0801   0.4479   0.4493
   0.250   0.4695   0.00770   0.00186  -0.0792   0.4303   0.5021
   0.500   0.4922   0.00761   0.00192  -0.0781   0.4142   0.5763
   0.750   0.5127   0.00742   0.00201  -0.0765   0.4006   0.6883
   1.000   0.5324   0.00727   0.00209  -0.0747   0.3891   0.7875
   1.250   0.5545   0.00713   0.00222  -0.0731   0.3786   0.8985
   1.500   0.6256   0.00732   0.00240  -0.0825   0.3659   0.9663
   2.000   0.7080   0.00768   0.00261  -0.0882   0.3495   0.9923
   2.250   0.7501   0.00783   0.00270  -0.0912   0.3430   0.9983
   2.500   0.7836   0.00795   0.00277  -0.0925   0.3375   1.0000
   2.750   0.8053   0.00810   0.00286  -0.0912   0.3320   1.0000
   3.000   0.8279   0.00821   0.00295  -0.0900   0.3282   1.0000
   3.250   0.8511   0.00830   0.00302  -0.0890   0.3246   1.0000
   3.500   0.8739   0.00842   0.00312  -0.0879   0.3205   1.0000
   3.750   0.8963   0.00857   0.00322  -0.0868   0.3167   1.0000
   4.000   0.9188   0.00871   0.00334  -0.0856   0.3128   1.0000
   4.250   0.9426   0.00880   0.00343  -0.0848   0.3102   1.0000
   4.500   0.9660   0.00891   0.00354  -0.0838   0.3070   1.0000
   4.750   0.9891   0.00905   0.00365  -0.0828   0.3035   1.0000
   5.000   1.0114   0.00922   0.00379  -0.0817   0.2995   1.0000
   5.250   1.0346   0.00935   0.00392  -0.0808   0.2960   1.0000
   5.500   1.0585   0.00945   0.00403  -0.0800   0.2927   1.0000
   5.750   1.0817   0.00958   0.00415  -0.0790   0.2889   1.0000
   6.000   1.1040   0.00975   0.00430  -0.0779   0.2847   1.0000
   6.250   1.1265   0.00991   0.00445  -0.0769   0.2807   1.0000
   6.500   1.1501   0.01002   0.00458  -0.0761   0.2770   1.0000
   6.750   1.1727   0.01018   0.00473  -0.0751   0.2721   1.0000
   7.000   1.1938   0.01039   0.00491  -0.0738   0.2662   1.0000
   7.250   1.2170   0.01052   0.00506  -0.0729   0.2608   1.0000
   7.500   1.2375   0.01075   0.00524  -0.0716   0.2520   1.0000
   7.750   1.2578   0.01100   0.00544  -0.0703   0.2392   1.0000
   8.000   1.2742   0.01135   0.00570  -0.0682   0.2222   1.0000
   8.250   1.2885   0.01175   0.00600  -0.0658   0.2044   1.0000
   8.500   1.3017   0.01221   0.00637  -0.0632   0.1893   1.0000
   8.750   1.3161   0.01265   0.00674  -0.0609   0.1796   1.0000
   9.000   1.3328   0.01300   0.00708  -0.0591   0.1737   1.0000
   9.250   1.3487   0.01340   0.00747  -0.0572   0.1686   1.0000
   9.500   1.3661   0.01375   0.00783  -0.0555   0.1648   1.0000
   9.750   1.3846   0.01406   0.00816  -0.0541   0.1622   1.0000
  10.000   1.4015   0.01446   0.00856  -0.0525   0.1585   1.0000
  10.250   1.4175   0.01490   0.00901  -0.0508   0.1551   1.0000
  10.500   1.4332   0.01537   0.00949  -0.0491   0.1516   1.0000
  10.750   1.4527   0.01567   0.00983  -0.0480   0.1494   1.0000
  11.000   1.4705   0.01606   0.01025  -0.0467   0.1466   1.0000
  11.250   1.4860   0.01658   0.01076  -0.0452   0.1427   1.0000
  11.500   1.4998   0.01720   0.01139  -0.0435   0.1381   1.0000
  11.750   1.5187   0.01757   0.01180  -0.0425   0.1358   1.0000
  12.000   1.5350   0.01809   0.01234  -0.0412   0.1312   1.0000
  12.250   1.5478   0.01882   0.01305  -0.0396   0.1246   1.0000
  12.500   1.5597   0.01963   0.01382  -0.0380   0.1146   1.0000
  12.750   1.5632   0.02100   0.01506  -0.0357   0.0948   1.0000
  13.000   1.5387   0.02434   0.01811  -0.0312   0.0568   1.0000
  13.250   1.5131   0.02821   0.02185  -0.0276   0.0287   1.0000
  13.500   1.5049   0.03103   0.02466  -0.0259   0.0197   1.0000
  13.750   1.5074   0.03308   0.02677  -0.0249   0.0181   1.0000
  14.000   1.5096   0.03522   0.02898  -0.0241   0.0167   1.0000
  14.250   1.5120   0.03742   0.03125  -0.0234   0.0160   1.0000
  14.500   1.5140   0.03974   0.03364  -0.0229   0.0155   1.0000
  14.750   1.5105   0.04271   0.03669  -0.0225   0.0148   1.0000
  15.250   1.5064   0.04861   0.04277  -0.0222   0.0139   1.0000
  15.500   1.5041   0.05174   0.04599  -0.0223   0.0137   1.0000
  15.750   1.5005   0.05509   0.04943  -0.0226   0.0134   1.0000
  16.000   1.4943   0.05883   0.05327  -0.0230   0.0131   1.0000
  16.250   1.4869   0.06285   0.05739  -0.0235   0.0129   1.0000
  16.500   1.4768   0.06730   0.06194  -0.0243   0.0126   1.0000
  16.750   1.4650   0.07202   0.06676  -0.0252   0.0124   1.0000
  17.000   1.4534   0.07682   0.07167  -0.0263   0.0122   1.0000
  17.250   1.4397   0.08198   0.07693  -0.0275   0.0121   1.0000
  17.500   1.4199   0.08808   0.08316  -0.0291   0.0119   1.0000
  17.750   1.4042   0.09366   0.08884  -0.0305   0.0118   1.0000
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