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GOE 321 (HANSA-BRANDENBURG III.1) AIRFOIL (goe321-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 321 (HANSA-BRANDENBURG III.1) AIRFOIL (goe321-il)
Reynolds number: 500,000
Max Cl/Cd: 105.27 at α=4.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe321-il-500000.txt
Download as CSV file: xf-goe321-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 321 (HANSA-BRANDENBURG III.1) 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
  ------ -------- --------- --------- -------- -------- --------
  -8.000  -0.2977   0.08873   0.08580  -0.0203   0.7530   0.0278
  -7.750  -0.2910   0.08562   0.08265  -0.0225   0.7456   0.0284
  -7.500  -0.2855   0.08235   0.07936  -0.0252   0.7388   0.0291
  -7.250  -0.2714   0.07408   0.07098  -0.0442   0.7328   0.0306
  -7.000  -0.2613   0.06951   0.06634  -0.0464   0.7267   0.0308
  -6.750  -0.2482   0.06682   0.06364  -0.0467   0.7202   0.0310
  -6.500  -0.2329   0.06426   0.06103  -0.0475   0.7134   0.0313
  -6.250  -0.2159   0.06156   0.05826  -0.0492   0.7072   0.0317
  -6.000  -0.1969   0.05860   0.05526  -0.0516   0.7002   0.0322
  -5.750  -0.1763   0.05549   0.05203  -0.0542   0.6938   0.0330
  -5.500  -0.1407   0.04755   0.04364  -0.0627   0.6884   0.0359
  -5.250  -0.1230   0.04491   0.04099  -0.0632   0.6810   0.0363
  -5.000  -0.1023   0.04292   0.03892  -0.0637   0.6742   0.0366
  -4.750  -0.0797   0.04093   0.03687  -0.0644   0.6663   0.0371
  -4.250  -0.0201   0.03574   0.03102  -0.0666   0.6520   0.0417
  -4.000   0.0013   0.03168   0.02679  -0.0675   0.6453   0.0424
  -3.750   0.0255   0.03015   0.02523  -0.0679   0.6383   0.0429
  -3.500   0.0508   0.02884   0.02386  -0.0682   0.6312   0.0437
  -3.250   0.0773   0.02742   0.02227  -0.0685   0.6253   0.0450
  -3.000   0.1085   0.02490   0.01917  -0.0684   0.6193   0.0495
  -2.750   0.1344   0.02329   0.01754  -0.0688   0.6130   0.0503
  -2.500   0.1613   0.02221   0.01639  -0.0690   0.6061   0.0512
  -2.250   0.1890   0.02122   0.01528  -0.0691   0.5985   0.0529
  -2.000   0.2205   0.02200   0.01567  -0.0685   0.5918   0.0573
  -1.750   0.2465   0.01887   0.01245  -0.0691   0.5859   0.0594
  -1.500   0.2743   0.01811   0.01161  -0.0693   0.5800   0.0613
  -1.250   0.3066   0.01399   0.00663  -0.0681   0.5750   0.0426
  -1.000   0.3353   0.01332   0.00585  -0.0681   0.5683   0.0425
  -0.750   0.3635   0.01276   0.00519  -0.0680   0.5624   0.0428
  -0.500   0.3921   0.01236   0.00481  -0.0681   0.5574   0.0438
  -0.250   0.4207   0.01208   0.00452  -0.0681   0.5529   0.0451
   0.000   0.4491   0.01177   0.00416  -0.0681   0.5485   0.0459
   0.250   0.4776   0.01151   0.00386  -0.0681   0.5438   0.0469
   0.500   0.5063   0.01128   0.00363  -0.0681   0.5385   0.0480
   0.750   0.5348   0.01107   0.00339  -0.0681   0.5340   0.0493
   1.000   0.5630   0.01089   0.00319  -0.0682   0.5296   0.0518
   1.250   0.5919   0.01078   0.00313  -0.0683   0.5247   0.0554
   1.500   0.6206   0.01063   0.00299  -0.0684   0.5189   0.0597
   1.750   0.6490   0.01061   0.00293  -0.0684   0.5136   0.0668
   2.000   0.6779   0.01044   0.00287  -0.0686   0.5083   0.0891
   2.250   0.7041   0.00830   0.00296  -0.0686   0.5027   1.0000
   2.500   0.7321   0.00844   0.00297  -0.0685   0.4968   1.0000
   2.750   0.7606   0.00849   0.00300  -0.0686   0.4909   1.0000
   3.000   0.7888   0.00857   0.00303  -0.0686   0.4843   1.0000
   3.250   0.8170   0.00868   0.00308  -0.0686   0.4779   1.0000
   3.500   0.8453   0.00874   0.00314  -0.0687   0.4701   1.0000
   3.750   0.8733   0.00885   0.00319  -0.0687   0.4621   1.0000
   4.000   0.9015   0.00893   0.00325  -0.0688   0.4520   1.0000
   4.250   0.9295   0.00903   0.00333  -0.0688   0.4403   1.0000
   4.500   0.9572   0.00916   0.00341  -0.0689   0.4250   1.0000
   4.750   0.9843   0.00935   0.00350  -0.0688   0.4030   1.0000
   5.000   1.0105   0.00967   0.00367  -0.0687   0.3735   1.0000
   5.250   1.0357   0.01010   0.00393  -0.0685   0.3448   1.0000
   5.500   1.0607   0.01056   0.00425  -0.0682   0.3215   1.0000
   5.750   1.0859   0.01099   0.00458  -0.0680   0.3009   1.0000
   6.000   1.1107   0.01145   0.00492  -0.0678   0.2805   1.0000
   6.250   1.1353   0.01192   0.00528  -0.0675   0.2602   1.0000
   6.500   1.1597   0.01237   0.00564  -0.0672   0.2415   1.0000
   6.750   1.1840   0.01283   0.00602  -0.0669   0.2275   1.0000
   7.000   1.2079   0.01330   0.00641  -0.0665   0.2175   1.0000
   7.250   1.2326   0.01366   0.00677  -0.0662   0.2110   1.0000
   7.500   1.2564   0.01409   0.00717  -0.0658   0.2056   1.0000
   7.750   1.2795   0.01456   0.00762  -0.0653   0.2013   1.0000
   8.000   1.3040   0.01489   0.00799  -0.0650   0.1988   1.0000
   8.250   1.3277   0.01527   0.00841  -0.0646   0.1963   1.0000
   8.500   1.3506   0.01569   0.00884  -0.0640   0.1933   1.0000
   8.750   1.3721   0.01620   0.00933  -0.0634   0.1899   1.0000
   9.000   1.3927   0.01676   0.00990  -0.0626   0.1867   1.0000
   9.250   1.4159   0.01709   0.01031  -0.0621   0.1846   1.0000
   9.500   1.4379   0.01748   0.01076  -0.0615   0.1824   1.0000
   9.750   1.4589   0.01793   0.01125  -0.0608   0.1803   1.0000
  10.000   1.4784   0.01845   0.01180  -0.0599   0.1778   1.0000
  10.250   1.4955   0.01910   0.01245  -0.0586   0.1749   1.0000
  10.500   1.5105   0.01981   0.01319  -0.0571   0.1723   1.0000
  10.750   1.5286   0.02019   0.01367  -0.0559   0.1704   1.0000
  11.000   1.5458   0.02066   0.01422  -0.0548   0.1675   1.0000
  11.250   1.5611   0.02127   0.01488  -0.0535   0.1642   1.0000
  11.500   1.5723   0.02219   0.01581  -0.0519   0.1604   1.0000
  11.750   1.5860   0.02302   0.01670  -0.0508   0.1568   1.0000
  12.000   1.6048   0.02353   0.01732  -0.0503   0.1524   1.0000
  12.250   1.6180   0.02450   0.01831  -0.0495   0.1477   1.0000
  12.500   1.6291   0.02570   0.01956  -0.0486   0.1434   1.0000
  12.750   1.6480   0.02635   0.02030  -0.0484   0.1365   1.0000
  13.000   1.6612   0.02752   0.02149  -0.0480   0.1256   1.0000
  13.250   1.6572   0.03036   0.02405  -0.0472   0.0883   1.0000
  13.500   1.6361   0.03493   0.02844  -0.0459   0.0618   1.0000
  13.750   1.6159   0.03952   0.03293  -0.0448   0.0425   1.0000
  14.000   1.6018   0.04363   0.03702  -0.0441   0.0324   1.0000
  14.250   1.5931   0.04727   0.04071  -0.0436   0.0280   1.0000
  14.500   1.5852   0.05093   0.04444  -0.0434   0.0257   1.0000
  14.750   1.5793   0.05446   0.04806  -0.0433   0.0243   1.0000
  15.000   1.5739   0.05805   0.05176  -0.0434   0.0232   1.0000
  15.250   1.5668   0.06200   0.05581  -0.0437   0.0224   1.0000
  15.500   1.5570   0.06642   0.06033  -0.0442   0.0216   1.0000
  15.750   1.5449   0.07126   0.06529  -0.0450   0.0210   1.0000
  16.000   1.5350   0.07591   0.07006  -0.0458   0.0206   1.0000
  16.250   1.5261   0.08049   0.07476  -0.0467   0.0202   1.0000
  16.500   1.5157   0.08538   0.07978  -0.0477   0.0198   1.0000
  16.750   1.5039   0.09058   0.08509  -0.0490   0.0194   1.0000
  17.000   1.4912   0.09605   0.09069  -0.0505   0.0191   1.0000
  17.250   1.4769   0.10185   0.09661  -0.0522   0.0188   1.0000
  17.500   1.4618   0.10794   0.10282  -0.0541   0.0186   1.0000
  17.750   1.4466   0.11417   0.10916  -0.0563   0.0184   1.0000
  18.000   1.4309   0.12054   0.11565  -0.0586   0.0182   1.0000
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