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GOE 290 (MVA 290) AIRFOIL (goe290-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 290 (MVA 290) AIRFOIL (goe290-il)
Reynolds number: 500,000
Max Cl/Cd: 96.53 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe290-il-500000.txt
Download as CSV file: xf-goe290-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.9048   0.06138   0.05767  -0.0729   1.0000   0.0385
 -15.250  -0.9247   0.05500   0.05111  -0.0778   1.0000   0.0386
 -15.000  -0.9357   0.05020   0.04617  -0.0814   1.0000   0.0388
 -14.750  -0.9421   0.04630   0.04214  -0.0842   1.0000   0.0390
 -14.500  -0.9453   0.04314   0.03888  -0.0860   1.0000   0.0392
 -14.250  -0.9468   0.04054   0.03616  -0.0870   1.0000   0.0394
 -14.000  -0.9472   0.03842   0.03394  -0.0872   1.0000   0.0397
 -13.750  -0.9472   0.03665   0.03209  -0.0864   1.0000   0.0400
 -13.500  -0.9490   0.03519   0.03053  -0.0844   1.0000   0.0403
 -13.250  -0.9568   0.03404   0.02929  -0.0805   1.0000   0.0406
 -13.000  -0.9612   0.03289   0.02804  -0.0767   1.0000   0.0408
 -12.750  -0.9632   0.03176   0.02678  -0.0731   1.0000   0.0411
 -12.500  -0.9628   0.03066   0.02557  -0.0696   1.0000   0.0415
 -12.250  -0.9600   0.02961   0.02439  -0.0663   1.0000   0.0418
 -12.000  -0.9325   0.02821   0.02280  -0.0678   0.9971   0.0423
 -11.750  -0.9013   0.02690   0.02130  -0.0698   0.9942   0.0427
 -11.500  -0.8708   0.02520   0.01958  -0.0716   0.9913   0.0434
 -11.250  -0.8375   0.02435   0.01874  -0.0734   0.9875   0.0440
 -11.000  -0.8013   0.02359   0.01795  -0.0757   0.9842   0.0448
 -10.750  -0.7644   0.02273   0.01702  -0.0782   0.9812   0.0456
 -10.500  -0.7352   0.02190   0.01611  -0.0789   0.9734   0.0463
 -10.250  -0.7048   0.02109   0.01520  -0.0798   0.9662   0.0470
 -10.000  -0.6794   0.02044   0.01444  -0.0795   0.9553   0.0476
  -9.750  -0.6577   0.01954   0.01347  -0.0786   0.9416   0.0483
  -9.500  -0.6362   0.01880   0.01272  -0.0775   0.9248   0.0491
  -9.250  -0.6139   0.01830   0.01219  -0.0764   0.9016   0.0498
  -9.000  -0.5916   0.01789   0.01167  -0.0752   0.8700   0.0507
  -8.750  -0.5688   0.01755   0.01115  -0.0740   0.8379   0.0517
  -8.500  -0.5449   0.01724   0.01065  -0.0732   0.8118   0.0527
  -8.250  -0.5199   0.01696   0.01018  -0.0726   0.7885   0.0536
  -8.000  -0.4966   0.01629   0.00944  -0.0719   0.7659   0.0548
  -7.750  -0.4715   0.01597   0.00904  -0.0714   0.7416   0.0559
  -7.500  -0.4458   0.01572   0.00867  -0.0710   0.7148   0.0572
  -7.250  -0.4199   0.01550   0.00829  -0.0706   0.6854   0.0587
  -7.000  -0.3935   0.01536   0.00796  -0.0702   0.6590   0.0600
  -6.750  -0.3688   0.01489   0.00741  -0.0698   0.6376   0.0619
  -6.500  -0.3421   0.01471   0.00715  -0.0696   0.6210   0.0637
  -6.250  -0.3150   0.01454   0.00688  -0.0695   0.6079   0.0658
  -6.000  -0.2873   0.01437   0.00661  -0.0693   0.5979   0.0676
  -5.750  -0.2615   0.01394   0.00616  -0.0691   0.5892   0.0701
  -5.500  -0.2338   0.01375   0.00592  -0.0691   0.5821   0.0727
  -5.250  -0.2055   0.01363   0.00573  -0.0691   0.5753   0.0752
  -5.000  -0.1790   0.01326   0.00533  -0.0689   0.5691   0.0785
  -4.750  -0.1511   0.01307   0.00511  -0.0689   0.5638   0.0818
  -4.500  -0.1225   0.01293   0.00492  -0.0690   0.5589   0.0846
  -4.250  -0.0952   0.01260   0.00460  -0.0689   0.5544   0.0890
  -4.000  -0.0670   0.01248   0.00441  -0.0689   0.5500   0.0932
  -3.750  -0.0389   0.01229   0.00422  -0.0690   0.5461   0.0985
  -3.500  -0.0102   0.01210   0.00405  -0.0691   0.5424   0.1050
  -3.250   0.0181   0.01188   0.00388  -0.0692   0.5379   0.1164
  -3.000   0.0459   0.01160   0.00370  -0.0692   0.5332   0.1457
  -2.750   0.0715   0.01101   0.00354  -0.0692   0.5284   0.2597
  -2.500   0.1002   0.01084   0.00354  -0.0693   0.5253   0.3080
  -2.250   0.1293   0.01080   0.00354  -0.0695   0.5221   0.3308
  -2.000   0.1585   0.01078   0.00354  -0.0697   0.5190   0.3468
  -1.750   0.1876   0.01078   0.00354  -0.0698   0.5158   0.3605
  -1.500   0.2167   0.01085   0.00355  -0.0700   0.5121   0.3726
  -1.250   0.2455   0.01087   0.00358  -0.0701   0.5084   0.3840
  -1.000   0.2749   0.01084   0.00358  -0.0703   0.5057   0.3954
  -0.750   0.3040   0.01081   0.00359  -0.0705   0.5028   0.4070
  -0.500   0.3331   0.01079   0.00359  -0.0707   0.4998   0.4180
  -0.250   0.3621   0.01079   0.00359  -0.0709   0.4967   0.4305
   0.000   0.3908   0.01080   0.00361  -0.0710   0.4931   0.4439
   0.250   0.4196   0.01082   0.00366  -0.0711   0.4895   0.4594
   0.500   0.4484   0.01073   0.00367  -0.0713   0.4866   0.4802
   0.750   0.4770   0.01064   0.00370  -0.0714   0.4837   0.5105
   1.000   0.5050   0.01050   0.00374  -0.0715   0.4806   0.5574
   1.250   0.5319   0.01027   0.00379  -0.0713   0.4774   0.6390
   1.500   0.5567   0.01002   0.00389  -0.0705   0.4742   0.7521
   1.750   0.5795   0.00986   0.00405  -0.0690   0.4709   0.8536
   2.000   0.6047   0.00977   0.00413  -0.0679   0.4675   0.9217
   2.250   0.6396   0.00979   0.00418  -0.0691   0.4633   0.9604
   2.500   0.6786   0.00986   0.00421  -0.0713   0.4592   0.9813
   2.750   0.7203   0.01001   0.00428  -0.0743   0.4550   0.9930
   3.000   0.7648   0.01010   0.00436  -0.0778   0.4515   0.9995
   3.250   0.7911   0.01014   0.00441  -0.0776   0.4480   1.0000
   3.500   0.8160   0.01019   0.00445  -0.0770   0.4443   1.0000
   3.750   0.8409   0.01026   0.00448  -0.0764   0.4404   1.0000
   4.000   0.8657   0.01040   0.00455  -0.0758   0.4360   1.0000
   4.250   0.8915   0.01041   0.00461  -0.0754   0.4309   1.0000
   4.500   0.9172   0.01046   0.00464  -0.0750   0.4243   1.0000
   4.750   0.9426   0.01056   0.00469  -0.0746   0.4175   1.0000
   5.000   0.9691   0.01062   0.00476  -0.0743   0.4101   1.0000
   5.250   0.9947   0.01075   0.00484  -0.0739   0.4029   1.0000
   5.500   1.0214   0.01085   0.00496  -0.0738   0.3955   1.0000
   5.750   1.0468   0.01100   0.00507  -0.0734   0.3866   1.0000
   6.000   1.0728   0.01115   0.00520  -0.0731   0.3754   1.0000
   6.250   1.0975   0.01137   0.00536  -0.0726   0.3605   1.0000
   6.500   1.1211   0.01165   0.00556  -0.0720   0.3427   1.0000
   6.750   1.1432   0.01205   0.00584  -0.0712   0.3221   1.0000
   7.000   1.1646   0.01250   0.00617  -0.0703   0.3007   1.0000
   7.250   1.1851   0.01300   0.00656  -0.0692   0.2820   1.0000
   7.500   1.2056   0.01348   0.00697  -0.0682   0.2682   1.0000
   7.750   1.2258   0.01396   0.00739  -0.0671   0.2577   1.0000
   8.000   1.2465   0.01439   0.00778  -0.0662   0.2488   1.0000
   8.250   1.2662   0.01485   0.00821  -0.0650   0.2413   1.0000
   8.500   1.2863   0.01527   0.00861  -0.0639   0.2344   1.0000
   8.750   1.3034   0.01579   0.00910  -0.0624   0.2275   1.0000
   9.000   1.3224   0.01615   0.00948  -0.0611   0.2223   1.0000
   9.250   1.3374   0.01666   0.00998  -0.0592   0.2166   1.0000
   9.500   1.3527   0.01719   0.01051  -0.0575   0.2112   1.0000
   9.750   1.3694   0.01769   0.01102  -0.0560   0.2043   1.0000
  10.000   1.3821   0.01841   0.01173  -0.0541   0.1975   1.0000
  10.250   1.3989   0.01896   0.01229  -0.0529   0.1890   1.0000
  10.500   1.4119   0.01974   0.01305  -0.0512   0.1785   1.0000
  10.750   1.4105   0.02142   0.01450  -0.0483   0.1370   1.0000
  11.000   1.3971   0.02411   0.01701  -0.0447   0.1097   1.0000
  11.250   1.3960   0.02625   0.01914  -0.0429   0.0995   1.0000
  11.500   1.3966   0.02845   0.02135  -0.0416   0.0910   1.0000
  11.750   1.3987   0.03065   0.02356  -0.0406   0.0791   1.0000
  12.500   1.3711   0.04133   0.03418  -0.0382   0.0405   1.0000
  12.750   1.3711   0.04418   0.03710  -0.0380   0.0393   1.0000
  13.000   1.3700   0.04718   0.04017  -0.0378   0.0384   1.0000
  13.250   1.3676   0.05034   0.04341  -0.0376   0.0376   1.0000
  13.500   1.3643   0.05366   0.04681  -0.0376   0.0370   1.0000
  13.750   1.3614   0.05697   0.05020  -0.0376   0.0364   1.0000
  14.000   1.3598   0.06016   0.05348  -0.0376   0.0361   1.0000
  14.250   1.3570   0.06355   0.05695  -0.0378   0.0357   1.0000
  14.500   1.3536   0.06707   0.06055  -0.0380   0.0353   1.0000
  14.750   1.3495   0.07067   0.06424  -0.0382   0.0349   1.0000
  15.000   1.3445   0.07445   0.06811  -0.0386   0.0345   1.0000
  15.250   1.3388   0.07842   0.07216  -0.0391   0.0342   1.0000
  15.500   1.3332   0.08239   0.07621  -0.0396   0.0338   1.0000
  15.750   1.3262   0.08659   0.08049  -0.0402   0.0335   1.0000
  16.000   1.3188   0.09093   0.08491  -0.0409   0.0333   1.0000
  16.250   1.3116   0.09529   0.08934  -0.0417   0.0330   1.0000
  16.500   1.3033   0.09983   0.09397  -0.0426   0.0328   1.0000
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