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GOE 290 (MVA 290) AIRFOIL (goe290-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 290 (MVA 290) AIRFOIL (goe290-il)
Reynolds number: 200,000
Max Cl/Cd: 67.02 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe290-il-200000-n5.txt
Download as CSV file: xf-goe290-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.7326   0.06396   0.05909  -0.0709   1.0000   0.0428
 -13.500  -0.7752   0.05417   0.04896  -0.0790   1.0000   0.0429
 -13.250  -0.7982   0.04846   0.04299  -0.0831   1.0000   0.0431
 -13.000  -0.8152   0.04453   0.03883  -0.0845   1.0000   0.0434
 -12.750  -0.8304   0.04170   0.03580  -0.0835   1.0000   0.0437
 -12.500  -0.8470   0.03972   0.03364  -0.0801   1.0000   0.0440
 -12.250  -0.8601   0.03804   0.03177  -0.0760   1.0000   0.0443
 -12.000  -0.8673   0.03641   0.02993  -0.0724   1.0000   0.0447
 -11.750  -0.8542   0.03488   0.02828  -0.0718   0.9967   0.0451
 -11.500  -0.8260   0.03358   0.02693  -0.0736   0.9914   0.0455
 -11.250  -0.7978   0.03234   0.02563  -0.0752   0.9847   0.0461
 -11.000  -0.7702   0.03113   0.02433  -0.0765   0.9770   0.0467
 -10.750  -0.7418   0.02991   0.02298  -0.0779   0.9688   0.0474
 -10.500  -0.7167   0.02877   0.02169  -0.0784   0.9574   0.0483
 -10.250  -0.6924   0.02763   0.02037  -0.0787   0.9448   0.0493
 -10.000  -0.6691   0.02652   0.01903  -0.0785   0.9300   0.0502
  -9.750  -0.6449   0.02569   0.01820  -0.0783   0.9114   0.0509
  -9.500  -0.6197   0.02495   0.01741  -0.0782   0.8883   0.0516
  -9.250  -0.5940   0.02420   0.01655  -0.0780   0.8623   0.0525
  -9.000  -0.5697   0.02350   0.01568  -0.0774   0.8368   0.0535
  -8.750  -0.5466   0.02284   0.01483  -0.0766   0.8128   0.0545
  -8.500  -0.5235   0.02224   0.01400  -0.0757   0.7908   0.0558
  -8.250  -0.5002   0.02169   0.01333  -0.0750   0.7699   0.0569
  -8.000  -0.4764   0.02124   0.01281  -0.0744   0.7494   0.0581
  -7.750  -0.4521   0.02082   0.01227  -0.0739   0.7287   0.0595
  -7.500  -0.4277   0.02038   0.01168  -0.0733   0.7079   0.0611
  -7.250  -0.4030   0.01996   0.01106  -0.0727   0.6874   0.0627
  -7.000  -0.3788   0.01950   0.01051  -0.0722   0.6681   0.0641
  -6.750  -0.3539   0.01913   0.01005  -0.0718   0.6506   0.0657
  -6.500  -0.3284   0.01880   0.00961  -0.0714   0.6357   0.0679
  -6.250  -0.3025   0.01852   0.00916  -0.0710   0.6234   0.0702
  -6.000  -0.2773   0.01811   0.00871  -0.0707   0.6128   0.0724
  -5.750  -0.2513   0.01779   0.00832  -0.0704   0.6040   0.0748
  -5.500  -0.2249   0.01751   0.00794  -0.0702   0.5955   0.0775
  -5.250  -0.1988   0.01720   0.00756  -0.0699   0.5884   0.0803
  -5.000  -0.1723   0.01688   0.00721  -0.0698   0.5813   0.0836
  -4.750  -0.1454   0.01666   0.00690  -0.0696   0.5750   0.0872
  -4.500  -0.1188   0.01639   0.00659  -0.0695   0.5699   0.0911
  -4.250  -0.0914   0.01614   0.00633  -0.0694   0.5649   0.0958
  -4.000  -0.0640   0.01591   0.00609  -0.0694   0.5601   0.1014
  -3.750  -0.0365   0.01571   0.00586  -0.0694   0.5556   0.1090
  -3.500  -0.0092   0.01551   0.00566  -0.0693   0.5515   0.1206
  -3.250   0.0184   0.01525   0.00546  -0.0693   0.5474   0.1410
  -3.000   0.0454   0.01487   0.00524  -0.0694   0.5433   0.1779
  -2.750   0.0718   0.01445   0.00520  -0.0694   0.5396   0.2662
  -2.500   0.0999   0.01440   0.00518  -0.0694   0.5362   0.3037
  -2.250   0.1282   0.01440   0.00517  -0.0694   0.5330   0.3267
  -2.000   0.1566   0.01442   0.00516  -0.0695   0.5295   0.3449
  -1.750   0.1852   0.01440   0.00516  -0.0696   0.5254   0.3617
  -1.500   0.2135   0.01437   0.00517  -0.0696   0.5211   0.3772
  -1.250   0.2417   0.01436   0.00516  -0.0696   0.5170   0.3914
  -1.000   0.2701   0.01439   0.00514  -0.0697   0.5132   0.4045
  -0.750   0.2984   0.01440   0.00515  -0.0697   0.5099   0.4176
  -0.500   0.3266   0.01436   0.00518  -0.0698   0.5064   0.4323
  -0.250   0.3548   0.01433   0.00521  -0.0698   0.5028   0.4488
   0.000   0.3829   0.01430   0.00524  -0.0698   0.4993   0.4663
   0.250   0.4108   0.01427   0.00526  -0.0698   0.4958   0.4864
   0.500   0.4384   0.01426   0.00529  -0.0697   0.4923   0.5102
   0.750   0.4659   0.01419   0.00536  -0.0696   0.4887   0.5397
   1.000   0.4931   0.01411   0.00544  -0.0694   0.4850   0.5771
   1.250   0.5195   0.01399   0.00554  -0.0691   0.4813   0.6301
   1.500   0.5445   0.01384   0.00564  -0.0683   0.4776   0.6998
   1.750   0.5687   0.01373   0.00575  -0.0671   0.4742   0.7795
   2.000   0.5955   0.01373   0.00589  -0.0664   0.4709   0.8557
   2.250   0.6293   0.01376   0.00603  -0.0672   0.4667   0.9151
   2.500   0.6674   0.01383   0.00612  -0.0693   0.4615   0.9549
   2.750   0.7062   0.01394   0.00618  -0.0715   0.4570   0.9821
   3.000   0.7464   0.01409   0.00625  -0.0742   0.4535   1.0000
   3.250   0.7710   0.01420   0.00638  -0.0736   0.4497   1.0000
   3.500   0.7958   0.01432   0.00651  -0.0731   0.4456   1.0000
   3.750   0.8209   0.01445   0.00663  -0.0726   0.4416   1.0000
   4.000   0.8461   0.01458   0.00670  -0.0722   0.4374   1.0000
   4.250   0.8713   0.01472   0.00683  -0.0717   0.4324   1.0000
   4.500   0.8964   0.01484   0.00698  -0.0713   0.4261   1.0000
   4.750   0.9214   0.01496   0.00706  -0.0708   0.4200   1.0000
   5.000   0.9465   0.01511   0.00722  -0.0703   0.4138   1.0000
   5.250   0.9715   0.01526   0.00738  -0.0699   0.4068   1.0000
   5.500   0.9959   0.01542   0.00750  -0.0693   0.3997   1.0000
   5.750   1.0204   0.01558   0.00769  -0.0688   0.3899   1.0000
   6.000   1.0440   0.01577   0.00785  -0.0682   0.3793   1.0000
   6.250   1.0667   0.01600   0.00803  -0.0674   0.3670   1.0000
   6.500   1.0890   0.01626   0.00826  -0.0665   0.3533   1.0000
   6.750   1.1106   0.01657   0.00852  -0.0656   0.3393   1.0000
   7.000   1.1306   0.01696   0.00883  -0.0645   0.3235   1.0000
   7.250   1.1489   0.01742   0.00921  -0.0631   0.3069   1.0000
   7.500   1.1661   0.01794   0.00965  -0.0616   0.2919   1.0000
   7.750   1.1832   0.01847   0.01013  -0.0601   0.2800   1.0000
   8.000   1.1992   0.01903   0.01065  -0.0584   0.2705   1.0000
   8.250   1.2139   0.01962   0.01121  -0.0566   0.2619   1.0000
   8.500   1.2261   0.02022   0.01180  -0.0544   0.2550   1.0000
   8.750   1.2388   0.02087   0.01244  -0.0523   0.2479   1.0000
   9.000   1.2490   0.02168   0.01322  -0.0501   0.2415   1.0000
   9.250   1.2632   0.02235   0.01394  -0.0485   0.2361   1.0000
   9.500   1.2756   0.02316   0.01476  -0.0469   0.2306   1.0000
   9.750   1.2858   0.02412   0.01573  -0.0451   0.2257   1.0000
  10.000   1.2979   0.02503   0.01669  -0.0437   0.2215   1.0000
  10.250   1.3109   0.02595   0.01766  -0.0425   0.2170   1.0000
  10.500   1.3204   0.02713   0.01888  -0.0411   0.2116   1.0000
  10.750   1.3271   0.02859   0.02034  -0.0397   0.2069   1.0000
  11.000   1.3400   0.02968   0.02153  -0.0389   0.2026   1.0000
  11.250   1.3498   0.03106   0.02298  -0.0381   0.1973   1.0000
  11.500   1.3554   0.03283   0.02479  -0.0371   0.1921   1.0000
  11.750   1.3653   0.03432   0.02636  -0.0365   0.1859   1.0000
  12.000   1.3696   0.03636   0.02844  -0.0359   0.1760   1.0000
  12.250   1.3690   0.03896   0.03103  -0.0353   0.1491   1.0000
  12.500   1.3481   0.04372   0.03559  -0.0348   0.1228   1.0000
  12.750   1.3362   0.04769   0.03950  -0.0344   0.1122   1.0000
  13.000   1.3298   0.05117   0.04301  -0.0341   0.1057   1.0000
  13.250   1.3258   0.05446   0.04635  -0.0340   0.1005   1.0000
  13.500   1.3223   0.05774   0.04969  -0.0340   0.0961   1.0000
  13.750   1.3221   0.06072   0.05275  -0.0340   0.0906   1.0000
  14.000   1.3194   0.06404   0.05614  -0.0342   0.0821   1.0000
  14.250   1.3059   0.06871   0.06077  -0.0345   0.0588   1.0000
  14.500   1.2879   0.07408   0.06609  -0.0352   0.0484   1.0000
  14.750   1.2770   0.07870   0.07074  -0.0358   0.0448   1.0000
  15.000   1.2689   0.08303   0.07514  -0.0364   0.0430   1.0000
  15.250   1.2621   0.08727   0.07946  -0.0372   0.0416   1.0000
  15.500   1.2559   0.09151   0.08378  -0.0380   0.0406   1.0000
  15.750   1.2507   0.09567   0.08804  -0.0388   0.0398   1.0000
  16.000   1.2454   0.09987   0.09234  -0.0398   0.0391   1.0000
  16.250   1.2396   0.10422   0.09678  -0.0408   0.0385   1.0000
  16.500   1.2333   0.10869   0.10135  -0.0420   0.0379   1.0000
  16.750   1.2271   0.11321   0.10597  -0.0433   0.0374   1.0000
  17.000   1.2207   0.11779   0.11064  -0.0447   0.0369   1.0000
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