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GOE 290 (MVA 290) AIRFOIL (goe290-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 290 (MVA 290) AIRFOIL (goe290-il)
Reynolds number: 1,000,000
Max Cl/Cd: 112.33 at α=4.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe290-il-1000000.txt
Download as CSV file: xf-goe290-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.000  -1.0092   0.09819   0.09531  -0.0437   1.0000   0.0292
 -18.750  -1.0340   0.09024   0.08722  -0.0487   1.0000   0.0293
 -18.500  -1.0525   0.08353   0.08039  -0.0529   1.0000   0.0294
 -18.250  -1.0686   0.07744   0.07418  -0.0567   1.0000   0.0294
 -18.000  -1.0913   0.07086   0.06746  -0.0605   1.0000   0.0296
 -17.750  -1.1116   0.06500   0.06148  -0.0638   1.0000   0.0298
 -17.500  -1.1258   0.05991   0.05629  -0.0667   1.0000   0.0300
 -17.250  -1.1353   0.05537   0.05167  -0.0693   1.0000   0.0301
 -17.000  -1.1415   0.05115   0.04738  -0.0719   1.0000   0.0303
 -16.750  -1.1448   0.04724   0.04340  -0.0744   1.0000   0.0305
 -16.500  -1.1455   0.04359   0.03967  -0.0769   1.0000   0.0307
 -16.250  -1.1443   0.04020   0.03620  -0.0793   1.0000   0.0308
 -16.000  -1.1413   0.03711   0.03304  -0.0815   1.0000   0.0310
 -15.750  -1.1369   0.03438   0.03021  -0.0833   1.0000   0.0312
 -15.500  -1.1314   0.03201   0.02777  -0.0846   1.0000   0.0314
 -15.250  -1.1252   0.03000   0.02568  -0.0853   1.0000   0.0316
 -15.000  -1.1184   0.02833   0.02393  -0.0853   1.0000   0.0318
 -14.750  -1.1112   0.02693   0.02246  -0.0846   1.0000   0.0321
 -14.500  -1.1044   0.02578   0.02123  -0.0832   1.0000   0.0323
 -14.250  -1.1007   0.02487   0.02025  -0.0807   1.0000   0.0325
 -14.000  -1.1030   0.02422   0.01955  -0.0764   1.0000   0.0327
 -13.750  -1.1003   0.02364   0.01891  -0.0728   1.0000   0.0329
 -13.500  -1.0774   0.02294   0.01814  -0.0728   0.9984   0.0332
 -13.250  -1.0479   0.02225   0.01739  -0.0740   0.9962   0.0334
 -13.000  -1.0230   0.02090   0.01596  -0.0750   0.9941   0.0339
 -12.750  -0.9950   0.01990   0.01493  -0.0762   0.9921   0.0344
 -12.500  -0.9674   0.01920   0.01420  -0.0769   0.9882   0.0348
 -12.250  -0.9383   0.01859   0.01357  -0.0777   0.9841   0.0352
 -12.000  -0.9101   0.01804   0.01299  -0.0782   0.9791   0.0356
 -11.750  -0.8863   0.01755   0.01246  -0.0777   0.9713   0.0361
 -11.500  -0.8636   0.01709   0.01196  -0.0769   0.9630   0.0365
 -11.250  -0.8416   0.01669   0.01150  -0.0758   0.9539   0.0370
 -11.000  -0.8190   0.01632   0.01107  -0.0749   0.9429   0.0374
 -10.750  -0.7959   0.01597   0.01065  -0.0740   0.9299   0.0377
 -10.500  -0.7752   0.01537   0.00997  -0.0728   0.9097   0.0382
 -10.250  -0.7552   0.01484   0.00932  -0.0713   0.8710   0.0389
  -9.750  -0.7072   0.01431   0.00850  -0.0698   0.8104   0.0401
  -9.500  -0.6814   0.01406   0.00816  -0.0694   0.7907   0.0407
  -9.250  -0.6552   0.01382   0.00782  -0.0691   0.7720   0.0414
  -9.000  -0.6286   0.01360   0.00750  -0.0689   0.7527   0.0420
  -8.750  -0.6016   0.01341   0.00720  -0.0687   0.7310   0.0426
  -8.500  -0.5763   0.01302   0.00671  -0.0683   0.7046   0.0437
  -8.250  -0.5497   0.01283   0.00641  -0.0681   0.6744   0.0448
  -7.750  -0.4954   0.01258   0.00592  -0.0678   0.6189   0.0468
  -7.500  -0.4676   0.01248   0.00570  -0.0677   0.5992   0.0477
  -7.250  -0.4407   0.01221   0.00536  -0.0676   0.5841   0.0493
  -7.000  -0.4127   0.01203   0.00515  -0.0676   0.5729   0.0507
  -6.750  -0.3844   0.01191   0.00497  -0.0676   0.5637   0.0522
  -6.500  -0.3557   0.01181   0.00481  -0.0677   0.5563   0.0536
  -6.250  -0.3280   0.01159   0.00456  -0.0676   0.5489   0.0558
  -6.000  -0.2992   0.01146   0.00442  -0.0677   0.5437   0.0578
  -5.750  -0.2702   0.01137   0.00430  -0.0678   0.5384   0.0597
  -5.500  -0.2419   0.01119   0.00409  -0.0679   0.5332   0.0621
  -5.250  -0.2133   0.01109   0.00397  -0.0680   0.5281   0.0644
  -5.000  -0.1840   0.01098   0.00385  -0.0681   0.5252   0.0665
  -4.750  -0.1551   0.01083   0.00368  -0.0683   0.5217   0.0689
  -4.500  -0.1263   0.01068   0.00354  -0.0684   0.5177   0.0717
  -4.250  -0.0973   0.01063   0.00344  -0.0685   0.5128   0.0743
  -4.000  -0.0684   0.01054   0.00331  -0.0687   0.5083   0.0769
  -3.750  -0.0393   0.01036   0.00316  -0.0688   0.5053   0.0804
  -3.500  -0.0100   0.01025   0.00305  -0.0690   0.5024   0.0834
  -3.250   0.0191   0.01014   0.00293  -0.0692   0.4994   0.0874
  -3.000   0.0481   0.01003   0.00282  -0.0693   0.4964   0.0929
  -2.750   0.0769   0.00992   0.00273  -0.0695   0.4931   0.1023
  -2.500   0.1053   0.00969   0.00263  -0.0696   0.4900   0.1360
  -2.250   0.1329   0.00918   0.00245  -0.0698   0.4878   0.2154
  -2.000   0.1615   0.00890   0.00240  -0.0700   0.4847   0.2818
  -1.750   0.1908   0.00881   0.00239  -0.0702   0.4816   0.3064
  -1.500   0.2201   0.00878   0.00238  -0.0704   0.4786   0.3224
  -1.250   0.2495   0.00880   0.00238  -0.0706   0.4756   0.3342
  -1.000   0.2785   0.00882   0.00241  -0.0708   0.4720   0.3467
  -0.750   0.3084   0.00879   0.00241  -0.0711   0.4704   0.3556
  -0.500   0.3380   0.00875   0.00241  -0.0713   0.4680   0.3675
  -0.250   0.3677   0.00872   0.00240  -0.0716   0.4651   0.3776
   0.000   0.3972   0.00871   0.00241  -0.0719   0.4622   0.3869
   0.250   0.4265   0.00872   0.00242  -0.0721   0.4594   0.3964
   0.500   0.4556   0.00874   0.00244  -0.0723   0.4561   0.4080
   0.750   0.4849   0.00874   0.00247  -0.0725   0.4528   0.4203
   1.000   0.5145   0.00868   0.00248  -0.0728   0.4498   0.4367
   1.250   0.5438   0.00862   0.00248  -0.0731   0.4460   0.4580
   1.500   0.5728   0.00858   0.00250  -0.0733   0.4420   0.4851
   1.750   0.6012   0.00851   0.00255  -0.0734   0.4380   0.5305
   2.000   0.6292   0.00832   0.00262  -0.0735   0.4350   0.6136
   2.250   0.6569   0.00807   0.00268  -0.0735   0.4322   0.7104
   2.500   0.6836   0.00788   0.00276  -0.0731   0.4284   0.7977
   2.750   0.7085   0.00776   0.00285  -0.0723   0.4242   0.8734
   3.000   0.7324   0.00776   0.00295  -0.0711   0.4198   0.9282
   3.250   0.7617   0.00778   0.00301  -0.0712   0.4161   0.9620
   3.500   0.7963   0.00784   0.00306  -0.0726   0.4099   0.9811
   3.750   0.8327   0.00798   0.00313  -0.0744   0.4018   0.9922
   4.250   0.9046   0.00822   0.00328  -0.0780   0.3833   1.0000
   4.500   0.9297   0.00834   0.00336  -0.0775   0.3736   1.0000
   4.750   0.9548   0.00850   0.00346  -0.0770   0.3623   1.0000
   5.000   0.9795   0.00872   0.00360  -0.0765   0.3458   1.0000
   5.250   1.0031   0.00907   0.00380  -0.0758   0.3223   1.0000
   5.500   1.0256   0.00952   0.00408  -0.0750   0.2927   1.0000
   5.750   1.0474   0.01003   0.00442  -0.0742   0.2646   1.0000
   6.000   1.0708   0.01043   0.00472  -0.0735   0.2485   1.0000
   6.250   1.0953   0.01075   0.00497  -0.0731   0.2386   1.0000
   6.500   1.1196   0.01106   0.00523  -0.0726   0.2304   1.0000
   6.750   1.1448   0.01131   0.00546  -0.0723   0.2247   1.0000
   7.000   1.1697   0.01157   0.00569  -0.0719   0.2194   1.0000
   7.250   1.1934   0.01190   0.00598  -0.0713   0.2129   1.0000
   7.500   1.2187   0.01212   0.00620  -0.0710   0.2089   1.0000
   7.750   1.2423   0.01243   0.00648  -0.0705   0.2027   1.0000
   8.000   1.2658   0.01274   0.00676  -0.0699   0.1969   1.0000
   8.250   1.2893   0.01303   0.00704  -0.0694   0.1895   1.0000
   8.500   1.3110   0.01341   0.00737  -0.0685   0.1801   1.0000
   8.750   1.3231   0.01429   0.00800  -0.0663   0.1423   1.0000
   9.000   1.3199   0.01569   0.00916  -0.0615   0.1052   1.0000
   9.250   1.3279   0.01651   0.00994  -0.0586   0.0937   1.0000
   9.500   1.3376   0.01734   0.01072  -0.0561   0.0820   1.0000
  10.000   1.3355   0.02042   0.01358  -0.0492   0.0348   1.0000
  10.250   1.3463   0.02146   0.01465  -0.0477   0.0329   1.0000
  10.500   1.3582   0.02249   0.01572  -0.0464   0.0318   1.0000
  10.750   1.3701   0.02360   0.01687  -0.0453   0.0312   1.0000
  11.000   1.3810   0.02487   0.01818  -0.0443   0.0306   1.0000
  11.250   1.3904   0.02632   0.01968  -0.0433   0.0300   1.0000
  11.500   1.3986   0.02796   0.02137  -0.0425   0.0295   1.0000
  11.750   1.4052   0.02982   0.02328  -0.0418   0.0290   1.0000
  12.000   1.4097   0.03193   0.02546  -0.0411   0.0285   1.0000
  12.250   1.4128   0.03428   0.02787  -0.0406   0.0281   1.0000
  12.500   1.4188   0.03640   0.03006  -0.0402   0.0280   1.0000
  12.750   1.4232   0.03871   0.03244  -0.0399   0.0278   1.0000
  13.000   1.4266   0.04117   0.03496  -0.0397   0.0275   1.0000
  13.250   1.4287   0.04380   0.03767  -0.0395   0.0272   1.0000
  13.500   1.4296   0.04661   0.04055  -0.0394   0.0269   1.0000
  13.750   1.4291   0.04957   0.04358  -0.0393   0.0267   1.0000
  14.000   1.4278   0.05268   0.04676  -0.0393   0.0265   1.0000
  14.250   1.4257   0.05590   0.05005  -0.0393   0.0263   1.0000
  14.500   1.4226   0.05925   0.05348  -0.0393   0.0261   1.0000
  14.750   1.4186   0.06277   0.05707  -0.0395   0.0259   1.0000
  15.000   1.4141   0.06640   0.06077  -0.0397   0.0257   1.0000
  15.250   1.4094   0.07004   0.06449  -0.0399   0.0255   1.0000
  15.500   1.4030   0.07398   0.06851  -0.0403   0.0253   1.0000
  15.750   1.3957   0.07812   0.07272  -0.0407   0.0252   1.0000
  16.000   1.3881   0.08231   0.07699  -0.0412   0.0250   1.0000
  16.250   1.3789   0.08676   0.08152  -0.0419   0.0248   1.0000
  16.500   1.3676   0.09160   0.08644  -0.0426   0.0246   1.0000
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