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GOE 604 AIRFOIL (goe604-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 604 AIRFOIL (goe604-il)
Reynolds number: 1,000,000
Max Cl/Cd: 108.81 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe604-il-1000000-n5.txt
Download as CSV file: xf-goe604-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 604 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
  ------ -------- --------- --------- -------- -------- --------
 -18.000  -0.8181   0.08397   0.08102  -0.0709   1.0000   0.0171
 -17.750  -0.8637   0.07426   0.07117  -0.0769   1.0000   0.0169
 -17.500  -0.9248   0.06279   0.05951  -0.0841   1.0000   0.0167
 -17.250  -0.9865   0.05126   0.04778  -0.0916   1.0000   0.0166
 -17.000  -1.0310   0.04127   0.03756  -0.0990   1.0000   0.0165
 -16.750  -1.0528   0.03465   0.03076  -0.1043   1.0000   0.0166
 -16.500  -1.0647   0.03078   0.02676  -0.1064   1.0000   0.0168
 -16.250  -1.0718   0.02841   0.02431  -0.1061   1.0000   0.0170
 -15.750  -1.0530   0.02509   0.02081  -0.1070   0.9859   0.0176
 -15.500  -1.0318   0.02394   0.01958  -0.1081   0.9781   0.0180
 -15.250  -1.0065   0.02277   0.01835  -0.1099   0.9708   0.0184
 -15.000  -0.9747   0.02175   0.01728  -0.1123   0.9645   0.0189
 -14.750  -0.9394   0.02083   0.01631  -0.1151   0.9570   0.0194
 -14.500  -0.9045   0.02001   0.01541  -0.1176   0.9454   0.0199
 -14.250  -0.8758   0.01933   0.01465  -0.1187   0.9290   0.0204
 -14.000  -0.8573   0.01882   0.01400  -0.1175   0.9080   0.0208
 -13.750  -0.8442   0.01841   0.01348  -0.1152   0.8869   0.0210
 -13.500  -0.8307   0.01796   0.01293  -0.1130   0.8647   0.0215
 -13.250  -0.8161   0.01759   0.01244  -0.1107   0.8382   0.0219
 -13.000  -0.8010   0.01728   0.01199  -0.1085   0.8078   0.0223
 -12.750  -0.7853   0.01703   0.01157  -0.1064   0.7733   0.0227
 -12.500  -0.7685   0.01677   0.01116  -0.1044   0.7409   0.0232
 -12.250  -0.7500   0.01652   0.01077  -0.1027   0.7148   0.0236
 -12.000  -0.7305   0.01626   0.01039  -0.1012   0.6921   0.0240
 -11.750  -0.7100   0.01601   0.01002  -0.0998   0.6727   0.0244
 -11.500  -0.6901   0.01568   0.00959  -0.0984   0.6556   0.0248
 -11.250  -0.6691   0.01537   0.00921  -0.0971   0.6406   0.0253
 -10.750  -0.6239   0.01485   0.00856  -0.0951   0.6185   0.0264
 -10.500  -0.6008   0.01462   0.00825  -0.0941   0.6087   0.0269
 -10.250  -0.5772   0.01436   0.00793  -0.0932   0.5999   0.0273
  -9.750  -0.5291   0.01390   0.00734  -0.0915   0.5841   0.0282
  -9.500  -0.5056   0.01361   0.00700  -0.0906   0.5766   0.0289
  -9.250  -0.4813   0.01337   0.00672  -0.0898   0.5698   0.0295
  -9.000  -0.4564   0.01315   0.00646  -0.0891   0.5633   0.0302
  -8.750  -0.4314   0.01296   0.00621  -0.0884   0.5563   0.0308
  -8.500  -0.4062   0.01276   0.00597  -0.0877   0.5504   0.0314
  -8.250  -0.3806   0.01258   0.00573  -0.0871   0.5434   0.0319
  -8.000  -0.3557   0.01240   0.00549  -0.0864   0.5353   0.0325
  -7.750  -0.3303   0.01217   0.00524  -0.0857   0.5290   0.0333
  -7.500  -0.3046   0.01199   0.00502  -0.0851   0.5229   0.0341
  -7.250  -0.2790   0.01183   0.00482  -0.0845   0.5175   0.0349
  -7.000  -0.2527   0.01168   0.00463  -0.0840   0.5125   0.0357
  -6.750  -0.2262   0.01154   0.00445  -0.0835   0.5076   0.0365
  -6.500  -0.2003   0.01136   0.00425  -0.0829   0.5029   0.0376
  -6.000  -0.1476   0.01108   0.00392  -0.0819   0.4941   0.0399
  -5.750  -0.1209   0.01095   0.00377  -0.0815   0.4891   0.0411
  -5.500  -0.0946   0.01083   0.00362  -0.0810   0.4840   0.0427
  -5.250  -0.0682   0.01071   0.00348  -0.0805   0.4797   0.0449
  -5.000  -0.0412   0.01060   0.00335  -0.0801   0.4761   0.0470
  -4.750  -0.0146   0.01047   0.00322  -0.0797   0.4718   0.0498
  -4.500   0.0121   0.01038   0.00311  -0.0793   0.4670   0.0528
  -4.250   0.0384   0.01028   0.00300  -0.0788   0.4621   0.0569
  -4.000   0.0653   0.01016   0.00289  -0.0784   0.4579   0.0618
  -3.750   0.0917   0.01005   0.00278  -0.0779   0.4527   0.0692
  -3.500   0.1175   0.00991   0.00266  -0.0774   0.4477   0.0820
  -3.250   0.1429   0.00971   0.00257  -0.0768   0.4436   0.1086
  -3.000   0.1695   0.00960   0.00252  -0.0764   0.4392   0.1272
  -2.750   0.1965   0.00957   0.00248  -0.0761   0.4342   0.1356
  -2.500   0.2230   0.00954   0.00245  -0.0756   0.4290   0.1432
  -2.250   0.2503   0.00953   0.00242  -0.0753   0.4247   0.1484
  -2.000   0.2772   0.00950   0.00239  -0.0750   0.4191   0.1552
  -1.750   0.3036   0.00950   0.00238  -0.0746   0.4129   0.1610
  -1.500   0.3307   0.00951   0.00236  -0.0742   0.4079   0.1652
  -1.250   0.3571   0.00948   0.00235  -0.0738   0.4019   0.1750
  -1.000   0.3832   0.00948   0.00235  -0.0734   0.3961   0.1857
  -0.750   0.4096   0.00945   0.00235  -0.0730   0.3915   0.1992
  -0.250   0.4613   0.00941   0.00238  -0.0720   0.3804   0.2376
   0.000   0.4874   0.00941   0.00240  -0.0715   0.3758   0.2556
   0.250   0.5135   0.00941   0.00243  -0.0711   0.3709   0.2732
   0.500   0.5390   0.00945   0.00247  -0.0706   0.3647   0.2902
   0.750   0.5645   0.00948   0.00252  -0.0701   0.3586   0.3069
   1.000   0.5899   0.00952   0.00258  -0.0695   0.3514   0.3242
   1.250   0.6146   0.00959   0.00265  -0.0689   0.3447   0.3420
   1.500   0.6402   0.00960   0.00270  -0.0684   0.3408   0.3620
   2.000   0.6895   0.00962   0.00285  -0.0671   0.3324   0.4222
   2.250   0.7131   0.00963   0.00294  -0.0663   0.3283   0.4615
   2.500   0.7371   0.00958   0.00301  -0.0655   0.3257   0.5102
   2.750   0.7600   0.00952   0.00310  -0.0646   0.3226   0.5692
   3.000   0.7812   0.00943   0.00321  -0.0633   0.3191   0.6439
   3.250   0.8001   0.00934   0.00333  -0.0615   0.3152   0.7240
   3.500   0.8165   0.00921   0.00346  -0.0590   0.3123   0.8169
   3.750   0.8502   0.00912   0.00367  -0.0602   0.3100   0.9240
   4.000   0.9273   0.00939   0.00393  -0.0709   0.3056   0.9626
   4.250   0.9708   0.00959   0.00410  -0.0743   0.3022   0.9739
   4.500   1.0037   0.00978   0.00426  -0.0755   0.2993   0.9825
   4.750   1.0374   0.00998   0.00443  -0.0770   0.2962   0.9902
   5.000   1.0763   0.01016   0.00460  -0.0795   0.2943   0.9978
   5.250   1.1144   0.01033   0.00476  -0.0818   0.2920   1.0000
   5.500   1.1338   0.01045   0.00488  -0.0802   0.2898   1.0000
   5.750   1.1529   0.01060   0.00502  -0.0786   0.2872   1.0000
   6.000   1.1710   0.01078   0.00517  -0.0768   0.2840   1.0000
   6.250   1.1888   0.01097   0.00535  -0.0750   0.2810   1.0000
   6.500   1.2069   0.01112   0.00550  -0.0732   0.2790   1.0000
   6.750   1.2238   0.01125   0.00565  -0.0711   0.2770   1.0000
   7.000   1.2404   0.01140   0.00580  -0.0690   0.2743   1.0000
   7.250   1.2570   0.01158   0.00597  -0.0670   0.2714   1.0000
   7.500   1.2740   0.01179   0.00618  -0.0652   0.2687   1.0000
   7.750   1.2908   0.01202   0.00640  -0.0633   0.2659   1.0000
   8.000   1.3092   0.01224   0.00663  -0.0618   0.2636   1.0000
   8.250   1.3285   0.01244   0.00685  -0.0605   0.2612   1.0000
   8.500   1.3474   0.01268   0.00709  -0.0592   0.2582   1.0000
   8.750   1.3648   0.01298   0.00739  -0.0576   0.2540   1.0000
   9.000   1.3813   0.01334   0.00773  -0.0561   0.2491   1.0000
   9.250   1.3994   0.01365   0.00805  -0.0548   0.2442   1.0000
   9.500   1.4158   0.01405   0.00844  -0.0533   0.2387   1.0000
   9.750   1.4316   0.01450   0.00888  -0.0518   0.2329   1.0000
  10.000   1.4455   0.01505   0.00940  -0.0502   0.2243   1.0000
  10.250   1.4575   0.01572   0.01003  -0.0483   0.2133   1.0000
  10.500   1.4617   0.01681   0.01103  -0.0457   0.1960   1.0000
  10.750   1.4655   0.01801   0.01216  -0.0433   0.1821   1.0000
  11.000   1.4709   0.01920   0.01332  -0.0413   0.1725   1.0000
  11.250   1.4788   0.02034   0.01445  -0.0397   0.1664   1.0000
  11.500   1.4862   0.02157   0.01568  -0.0382   0.1613   1.0000
  11.750   1.4927   0.02293   0.01705  -0.0369   0.1566   1.0000
  12.000   1.5036   0.02406   0.01822  -0.0360   0.1543   1.0000
  12.250   1.5135   0.02531   0.01950  -0.0352   0.1522   1.0000
  12.500   1.5231   0.02663   0.02086  -0.0344   0.1507   1.0000
  12.750   1.5291   0.02829   0.02255  -0.0336   0.1482   1.0000
  13.000   1.5341   0.03010   0.02440  -0.0329   0.1458   1.0000
  13.250   1.5388   0.03200   0.02635  -0.0323   0.1437   1.0000
  13.500   1.5453   0.03378   0.02818  -0.0318   0.1421   1.0000
  13.750   1.5528   0.03549   0.02996  -0.0315   0.1410   1.0000
  14.000   1.5589   0.03737   0.03190  -0.0312   0.1398   1.0000
  14.250   1.5634   0.03943   0.03400  -0.0308   0.1384   1.0000
  14.500   1.5640   0.04187   0.03649  -0.0305   0.1358   1.0000
  14.750   1.5634   0.04447   0.03914  -0.0302   0.1339   1.0000
  15.000   1.5612   0.04728   0.04200  -0.0299   0.1320   1.0000
  15.250   1.5591   0.05010   0.04489  -0.0297   0.1305   1.0000
  15.500   1.5594   0.05272   0.04756  -0.0296   0.1293   1.0000
  15.750   1.5625   0.05505   0.04996  -0.0296   0.1280   1.0000
  16.000   1.5618   0.05784   0.05282  -0.0296   0.1262   1.0000
  16.250   1.5610   0.06065   0.05569  -0.0296   0.1247   1.0000
  16.500   1.5567   0.06386   0.05894  -0.0297   0.1220   1.0000
  16.750   1.5510   0.06732   0.06245  -0.0299   0.1202   1.0000
  17.000   1.5432   0.07104   0.06622  -0.0301   0.1175   1.0000
  17.250   1.5428   0.07390   0.06914  -0.0304   0.1156   1.0000
  17.500   1.5371   0.07745   0.07275  -0.0307   0.1126   1.0000
  17.750   1.5275   0.08151   0.07685  -0.0312   0.1090   1.0000
  18.000   1.5184   0.08553   0.08089  -0.0317   0.1047   1.0000
  18.250   1.4978   0.09103   0.08639  -0.0325   0.0958   1.0000
  18.500   1.4741   0.09707   0.09243  -0.0335   0.0858   1.0000
  18.750   1.4372   0.10492   0.10023  -0.0350   0.0703   1.0000
  19.000   1.4148   0.11101   0.10632  -0.0364   0.0616   1.0000
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