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GOE 290 (MVA 290) AIRFOIL (goe290-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 290 (MVA 290) AIRFOIL (goe290-il)
Reynolds number: 1,000,000
Max Cl/Cd: 92.44 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe290-il-1000000-n5.txt
Download as CSV file: xf-goe290-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 290 (MVA 290) 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.0257   0.10916   0.10624  -0.0362   1.0000   0.0257
 -19.500  -1.0527   0.10093   0.09789  -0.0409   1.0000   0.0258
 -19.250  -1.0770   0.09331   0.09016  -0.0453   1.0000   0.0259
 -19.000  -1.0998   0.08614   0.08287  -0.0494   1.0000   0.0260
 -18.750  -1.1200   0.07956   0.07618  -0.0532   1.0000   0.0261
 -18.500  -1.1397   0.07335   0.06986  -0.0568   1.0000   0.0262
 -18.250  -1.1592   0.06742   0.06382  -0.0601   1.0000   0.0263
 -18.000  -1.1776   0.06169   0.05799  -0.0634   1.0000   0.0264
 -17.750  -1.1936   0.05624   0.05242  -0.0666   1.0000   0.0265
 -17.500  -1.2059   0.05119   0.04727  -0.0696   1.0000   0.0266
 -17.250  -1.2147   0.04644   0.04240  -0.0726   1.0000   0.0267
 -17.000  -1.2194   0.04208   0.03794  -0.0756   1.0000   0.0269
 -16.750  -1.2203   0.03819   0.03393  -0.0785   1.0000   0.0270
 -16.500  -1.2187   0.03476   0.03040  -0.0811   1.0000   0.0271
 -16.250  -1.2148   0.03190   0.02743  -0.0830   1.0000   0.0272
 -16.000  -1.2094   0.02959   0.02503  -0.0842   1.0000   0.0273
 -15.750  -1.2027   0.02775   0.02309  -0.0845   1.0000   0.0274
 -15.500  -1.1963   0.02619   0.02145  -0.0841   1.0000   0.0275
 -15.250  -1.1924   0.02475   0.01995  -0.0829   1.0000   0.0277
 -15.000  -1.1885   0.02368   0.01882  -0.0807   1.0000   0.0279
 -14.750  -1.1734   0.02275   0.01784  -0.0800   0.9934   0.0282
 -14.500  -1.1521   0.02192   0.01697  -0.0800   0.9849   0.0285
 -14.250  -1.1307   0.02120   0.01620  -0.0798   0.9763   0.0288
 -14.000  -1.1105   0.02055   0.01550  -0.0792   0.9688   0.0290
 -13.750  -1.0914   0.01996   0.01486  -0.0782   0.9608   0.0292
 -13.500  -1.0720   0.01942   0.01425  -0.0771   0.9520   0.0295
 -13.250  -1.0518   0.01890   0.01368  -0.0761   0.9423   0.0297
 -13.000  -1.0307   0.01840   0.01312  -0.0752   0.9324   0.0300
 -12.750  -1.0096   0.01793   0.01259  -0.0743   0.9168   0.0302
 -12.500  -0.9901   0.01754   0.01204  -0.0728   0.8748   0.0305
 -12.250  -0.9691   0.01724   0.01153  -0.0716   0.8316   0.0307
 -12.000  -0.9456   0.01691   0.01106  -0.0710   0.8083   0.0310
 -11.750  -0.9212   0.01660   0.01064  -0.0705   0.7908   0.0312
 -11.500  -0.8974   0.01617   0.01013  -0.0700   0.7746   0.0317
 -11.250  -0.8729   0.01579   0.00966  -0.0696   0.7577   0.0321
 -11.000  -0.8478   0.01545   0.00924  -0.0692   0.7394   0.0325
 -10.750  -0.8223   0.01515   0.00886  -0.0689   0.7195   0.0329
 -10.500  -0.7966   0.01488   0.00848  -0.0686   0.6954   0.0333
 -10.250  -0.7707   0.01465   0.00813  -0.0683   0.6680   0.0337
 -10.000  -0.7445   0.01443   0.00779  -0.0681   0.6416   0.0342
  -9.750  -0.7180   0.01422   0.00747  -0.0679   0.6182   0.0346
  -9.500  -0.6912   0.01402   0.00716  -0.0677   0.5983   0.0350
  -9.250  -0.6642   0.01382   0.00687  -0.0676   0.5819   0.0354
  -9.000  -0.6374   0.01356   0.00654  -0.0674   0.5683   0.0361
  -8.750  -0.6101   0.01333   0.00626  -0.0673   0.5578   0.0368
  -8.500  -0.5826   0.01312   0.00601  -0.0673   0.5493   0.0376
  -8.250  -0.5547   0.01292   0.00577  -0.0673   0.5427   0.0384
  -8.000  -0.5267   0.01274   0.00554  -0.0672   0.5361   0.0393
  -7.750  -0.4986   0.01257   0.00532  -0.0672   0.5301   0.0400
  -7.500  -0.4706   0.01235   0.00509  -0.0672   0.5254   0.0411
  -7.250  -0.4423   0.01217   0.00488  -0.0673   0.5203   0.0423
  -7.000  -0.4139   0.01201   0.00469  -0.0673   0.5154   0.0435
  -6.500  -0.3568   0.01170   0.00434  -0.0675   0.5083   0.0462
  -6.250  -0.3280   0.01154   0.00417  -0.0676   0.5053   0.0479
  -6.000  -0.2991   0.01141   0.00402  -0.0677   0.5020   0.0495
  -5.750  -0.2703   0.01128   0.00388  -0.0678   0.4985   0.0513
  -5.500  -0.2415   0.01116   0.00375  -0.0679   0.4949   0.0535
  -5.250  -0.2125   0.01106   0.00363  -0.0680   0.4909   0.0554
  -5.000  -0.1834   0.01094   0.00350  -0.0682   0.4881   0.0573
  -4.750  -0.1542   0.01082   0.00339  -0.0683   0.4848   0.0594
  -4.500  -0.1250   0.01073   0.00328  -0.0685   0.4817   0.0615
  -4.250  -0.0958   0.01065   0.00318  -0.0687   0.4790   0.0632
  -4.000  -0.0667   0.01055   0.00308  -0.0688   0.4757   0.0657
  -3.750  -0.0376   0.01048   0.00300  -0.0690   0.4720   0.0682
  -3.500  -0.0081   0.01040   0.00291  -0.0692   0.4698   0.0702
  -3.250   0.0212   0.01030   0.00281  -0.0694   0.4669   0.0727
  -3.000   0.0505   0.01021   0.00273  -0.0696   0.4636   0.0754
  -2.750   0.0799   0.01015   0.00265  -0.0698   0.4604   0.0781
  -2.500   0.1091   0.01008   0.00258  -0.0700   0.4577   0.0817
  -2.250   0.1383   0.01000   0.00251  -0.0702   0.4549   0.0866
  -2.000   0.1675   0.00991   0.00245  -0.0704   0.4525   0.0946
  -1.750   0.1966   0.00973   0.00238  -0.0706   0.4503   0.1192
  -1.500   0.2256   0.00954   0.00230  -0.0708   0.4479   0.1517
  -1.250   0.2539   0.00924   0.00220  -0.0710   0.4453   0.2065
  -1.000   0.2824   0.00901   0.00217  -0.0712   0.4421   0.2694
  -0.750   0.3115   0.00896   0.00217  -0.0714   0.4385   0.2917
  -0.500   0.3408   0.00897   0.00218  -0.0717   0.4353   0.3032
  -0.250   0.3704   0.00893   0.00219  -0.0719   0.4332   0.3153
   0.000   0.4000   0.00892   0.00219  -0.0722   0.4302   0.3260
   0.250   0.4294   0.00891   0.00221  -0.0724   0.4257   0.3363
   0.500   0.4585   0.00895   0.00222  -0.0726   0.4197   0.3451
   0.750   0.4877   0.00895   0.00225  -0.0729   0.4145   0.3561
   1.000   0.5171   0.00897   0.00227  -0.0731   0.4097   0.3641
   1.250   0.5462   0.00900   0.00230  -0.0733   0.4040   0.3738
   1.500   0.5752   0.00904   0.00234  -0.0735   0.3974   0.3843
   1.750   0.6040   0.00908   0.00239  -0.0737   0.3882   0.3972
   2.000   0.6327   0.00913   0.00244  -0.0739   0.3804   0.4103
   2.250   0.6613   0.00916   0.00250  -0.0740   0.3725   0.4293
   2.500   0.6895   0.00923   0.00258  -0.0742   0.3623   0.4476
   2.750   0.7171   0.00936   0.00268  -0.0742   0.3460   0.4661
   3.000   0.7439   0.00954   0.00283  -0.0741   0.3248   0.4914
   3.250   0.7697   0.00977   0.00303  -0.0739   0.2991   0.5275
   3.500   0.7937   0.01012   0.00333  -0.0735   0.2642   0.5780
   3.750   0.8179   0.01038   0.00362  -0.0730   0.2394   0.6385
   4.000   0.8438   0.01045   0.00382  -0.0728   0.2290   0.7043
   4.250   0.8694   0.01050   0.00403  -0.0724   0.2214   0.7698
   4.500   0.8944   0.01052   0.00421  -0.0719   0.2164   0.8331
   4.750   0.9177   0.01059   0.00441  -0.0709   0.2114   0.8907
   5.000   0.9410   0.01071   0.00461  -0.0698   0.2067   0.9380
   5.250   0.9712   0.01085   0.00477  -0.0703   0.2033   0.9716
   5.500   1.0039   0.01108   0.00497  -0.0716   0.1981   0.9928
   5.750   1.0325   0.01134   0.00518  -0.0720   0.1926   1.0000
   6.000   1.0585   0.01153   0.00536  -0.0717   0.1896   1.0000
   6.250   1.0843   0.01173   0.00554  -0.0715   0.1855   1.0000
   6.500   1.1086   0.01202   0.00578  -0.0710   0.1785   1.0000
   6.750   1.1326   0.01233   0.00603  -0.0705   0.1680   1.0000
   7.000   1.1417   0.01356   0.00691  -0.0677   0.1109   1.0000
   7.250   1.1617   0.01405   0.00736  -0.0666   0.1016   1.0000
   7.500   1.1825   0.01447   0.00775  -0.0656   0.0950   1.0000
   7.750   1.2018   0.01494   0.00819  -0.0644   0.0880   1.0000
   8.000   1.2196   0.01545   0.00864  -0.0630   0.0777   1.0000
   8.250   1.2153   0.01681   0.00980  -0.0580   0.0340   1.0000
   8.500   1.2301   0.01738   0.01037  -0.0562   0.0306   1.0000
   8.750   1.2459   0.01795   0.01095  -0.0546   0.0291   1.0000
   9.000   1.2617   0.01854   0.01156  -0.0532   0.0281   1.0000
   9.250   1.2779   0.01915   0.01219  -0.0518   0.0275   1.0000
   9.500   1.2932   0.01983   0.01288  -0.0505   0.0269   1.0000
   9.750   1.3078   0.02059   0.01366  -0.0492   0.0265   1.0000
  10.000   1.3217   0.02144   0.01454  -0.0480   0.0260   1.0000
  10.250   1.3347   0.02239   0.01553  -0.0468   0.0256   1.0000
  10.500   1.3468   0.02348   0.01665  -0.0457   0.0252   1.0000
  10.750   1.3579   0.02472   0.01793  -0.0447   0.0248   1.0000
  11.000   1.3688   0.02605   0.01929  -0.0438   0.0245   1.0000
  11.250   1.3801   0.02740   0.02069  -0.0432   0.0243   1.0000
  11.500   1.3907   0.02889   0.02222  -0.0426   0.0241   1.0000
  11.750   1.4000   0.03052   0.02390  -0.0420   0.0238   1.0000
  12.000   1.4083   0.03230   0.02574  -0.0416   0.0236   1.0000
  12.250   1.4155   0.03424   0.02773  -0.0411   0.0234   1.0000
  12.500   1.4217   0.03634   0.02988  -0.0408   0.0232   1.0000
  12.750   1.4267   0.03858   0.03218  -0.0405   0.0230   1.0000
  13.000   1.4306   0.04097   0.03463  -0.0403   0.0228   1.0000
  13.250   1.4335   0.04351   0.03724  -0.0401   0.0226   1.0000
  13.500   1.4353   0.04620   0.03999  -0.0400   0.0225   1.0000
  13.750   1.4361   0.04900   0.04286  -0.0399   0.0223   1.0000
  14.000   1.4361   0.05193   0.04585  -0.0398   0.0221   1.0000
  14.250   1.4352   0.05501   0.04899  -0.0398   0.0220   1.0000
  14.500   1.4332   0.05822   0.05228  -0.0399   0.0218   1.0000
  14.750   1.4304   0.06155   0.05568  -0.0400   0.0217   1.0000
  15.000   1.4273   0.06496   0.05915  -0.0401   0.0215   1.0000
  15.250   1.4222   0.06867   0.06293  -0.0404   0.0213   1.0000
  15.500   1.4174   0.07235   0.06669  -0.0406   0.0212   1.0000
  15.750   1.4175   0.07546   0.06986  -0.0409   0.0211   1.0000
  16.000   1.4154   0.07893   0.07340  -0.0413   0.0210   1.0000
  16.250   1.4145   0.08222   0.07676  -0.0417   0.0209   1.0000
  16.500   1.4108   0.08592   0.08053  -0.0422   0.0208   1.0000
  16.750   1.4095   0.08933   0.08400  -0.0427   0.0207   1.0000
  17.000   1.4054   0.09318   0.08792  -0.0433   0.0206   1.0000
  17.250   1.4030   0.09680   0.09161  -0.0440   0.0205   1.0000
  17.500   1.3988   0.10071   0.09559  -0.0448   0.0204   1.0000
  17.750   1.3950   0.10457   0.09953  -0.0456   0.0203   1.0000
  18.000   1.3912   0.10847   0.10350  -0.0465   0.0202   1.0000
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