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GOE 321 (HANSA-BRANDENBURG III.1) AIRFOIL (goe321-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: GOE 321 (HANSA-BRANDENBURG III.1) AIRFOIL (goe321-il)
Reynolds number: 200,000
Max Cl/Cd: 77.69 at α=6°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe321-il-200000.txt
Download as CSV file: xf-goe321-il-200000.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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -8.000  -0.2609   0.09020   0.08702  -0.0338   0.9012   0.0480
  -7.750  -0.2641   0.08689   0.08356  -0.0459   0.8696   0.0488
  -7.500  -0.2567   0.08245   0.07902  -0.0493   0.8530   0.0491
  -7.250  -0.2484   0.07934   0.07587  -0.0453   0.8399   0.0495
  -7.000  -0.2382   0.07662   0.07308  -0.0438   0.8274   0.0501
  -6.750  -0.2260   0.07384   0.07023  -0.0444   0.8152   0.0510
  -6.500  -0.2124   0.07092   0.06723  -0.0464   0.8043   0.0524
  -6.250  -0.1964   0.06768   0.06385  -0.0499   0.7939   0.0545
  -6.000  -0.1636   0.06287   0.05854  -0.0635   0.7837   0.0576
  -5.750  -0.1520   0.05902   0.05471  -0.0624   0.7751   0.0582
  -5.500  -0.1364   0.05633   0.05202  -0.0620   0.7650   0.0589
  -5.250  -0.1185   0.05391   0.04952  -0.0624   0.7568   0.0601
  -5.000  -0.0972   0.05137   0.04688  -0.0637   0.7477   0.0620
  -4.750  -0.0594   0.04924   0.04398  -0.0689   0.7407   0.0679
  -4.500  -0.0430   0.04506   0.03996  -0.0691   0.7324   0.0689
  -4.250  -0.0232   0.04287   0.03772  -0.0691   0.7259   0.0703
  -4.000   0.0003   0.04086   0.03565  -0.0697   0.7178   0.0725
  -3.500   0.0562   0.03637   0.03051  -0.0718   0.7049   0.0814
  -3.250   0.0797   0.03443   0.02857  -0.0721   0.6984   0.0834
  -3.000   0.1055   0.03294   0.02693  -0.0724   0.6934   0.0874
  -2.750   0.1352   0.03126   0.02488  -0.0731   0.6876   0.0954
  -2.500   0.1602   0.02968   0.02332  -0.0733   0.6818   0.0992
  -2.250   0.1889   0.02853   0.02181  -0.0735   0.6773   0.1103
  -2.000   0.2151   0.02708   0.02038  -0.0738   0.6720   0.1149
  -1.750   0.2433   0.02593   0.01904  -0.0742   0.6666   0.1274
  -1.500   0.2706   0.02496   0.01789  -0.0742   0.6616   0.1427
  -1.250   0.2974   0.02390   0.01676  -0.0744   0.6556   0.1597
  -0.750   0.3669   0.02017   0.01183  -0.0724   0.6442   0.0778
  -0.500   0.3958   0.01896   0.01050  -0.0723   0.6378   0.0743
  -0.250   0.4247   0.01807   0.00944  -0.0720   0.6316   0.0724
   0.000   0.4531   0.01740   0.00860  -0.0716   0.6267   0.0723
   0.250   0.4815   0.01688   0.00809  -0.0715   0.6199   0.0734
   0.500   0.5097   0.01651   0.00767  -0.0713   0.6143   0.0769
   0.750   0.5380   0.01621   0.00727  -0.0710   0.6097   0.0793
   1.000   0.5654   0.01560   0.00680  -0.0709   0.6029   0.0827
   1.250   0.5933   0.01524   0.00643  -0.0706   0.5968   0.0882
   1.500   0.6210   0.01493   0.00616  -0.0705   0.5903   0.0985
   1.750   0.6490   0.01463   0.00589  -0.0704   0.5835   0.1196
   2.000   0.6782   0.01239   0.00564  -0.0702   0.5777   1.0000
   2.250   0.7056   0.01248   0.00564  -0.0700   0.5696   1.0000
   2.500   0.7333   0.01256   0.00556  -0.0698   0.5633   1.0000
   2.750   0.7608   0.01270   0.00566  -0.0697   0.5562   1.0000
   3.000   0.7884   0.01280   0.00567  -0.0695   0.5492   1.0000
   3.250   0.8158   0.01295   0.00575  -0.0694   0.5422   1.0000
   3.500   0.8431   0.01306   0.00582  -0.0692   0.5342   1.0000
   3.750   0.8705   0.01321   0.00589  -0.0691   0.5267   1.0000
   4.000   0.8975   0.01331   0.00598  -0.0689   0.5174   1.0000
   4.250   0.9245   0.01344   0.00608  -0.0687   0.5084   1.0000
   4.500   0.9514   0.01354   0.00613  -0.0684   0.4983   1.0000
   4.750   0.9779   0.01365   0.00625  -0.0682   0.4869   1.0000
   5.000   1.0044   0.01375   0.00634  -0.0680   0.4753   1.0000
   5.250   1.0307   0.01385   0.00641  -0.0677   0.4625   1.0000
   5.500   1.0567   0.01395   0.00651  -0.0674   0.4469   1.0000
   5.750   1.0823   0.01406   0.00665  -0.0670   0.4272   1.0000
   6.000   1.1071   0.01425   0.00677  -0.0666   0.4033   1.0000
   6.250   1.1303   0.01460   0.00698  -0.0659   0.3749   1.0000
   6.500   1.1518   0.01518   0.00735  -0.0651   0.3471   1.0000
   6.750   1.1719   0.01593   0.00790  -0.0642   0.3235   1.0000
   7.000   1.1925   0.01667   0.00852  -0.0633   0.3038   1.0000
   7.250   1.2131   0.01741   0.00915  -0.0625   0.2888   1.0000
   7.750   1.2557   0.01874   0.01039  -0.0610   0.2682   1.0000
   8.000   1.2766   0.01948   0.01102  -0.0602   0.2614   1.0000
   8.250   1.2990   0.02002   0.01162  -0.0596   0.2551   1.0000
   8.500   1.3206   0.02064   0.01224  -0.0589   0.2500   1.0000
   8.750   1.3425   0.02138   0.01291  -0.0583   0.2460   1.0000
   9.000   1.3648   0.02195   0.01358  -0.0578   0.2424   1.0000
   9.250   1.3869   0.02256   0.01427  -0.0572   0.2392   1.0000
   9.500   1.4091   0.02319   0.01494  -0.0566   0.2363   1.0000
   9.750   1.4317   0.02389   0.01563  -0.0561   0.2337   1.0000
  10.000   1.4551   0.02470   0.01642  -0.0559   0.2308   1.0000
  10.250   1.4743   0.02528   0.01719  -0.0549   0.2275   1.0000
  10.500   1.4932   0.02589   0.01790  -0.0540   0.2236   1.0000
  10.750   1.5120   0.02652   0.01855  -0.0531   0.2197   1.0000
  11.000   1.5328   0.02735   0.01935  -0.0526   0.2157   1.0000
  11.250   1.5469   0.02800   0.02021  -0.0511   0.2122   1.0000
  11.500   1.5602   0.02866   0.02098  -0.0495   0.2081   1.0000
  11.750   1.5733   0.02936   0.02167  -0.0479   0.2038   1.0000
  12.000   1.5847   0.03024   0.02263  -0.0462   0.1997   1.0000
  12.250   1.5901   0.03114   0.02372  -0.0440   0.1955   1.0000
  12.500   1.5972   0.03209   0.02473  -0.0423   0.1909   1.0000
  12.750   1.6066   0.03322   0.02585  -0.0410   0.1858   1.0000
  13.000   1.6080   0.03462   0.02748  -0.0395   0.1814   1.0000
  13.250   1.6127   0.03604   0.02899  -0.0384   0.1767   1.0000
  13.500   1.6216   0.03740   0.03034  -0.0375   0.1720   1.0000
  13.750   1.6212   0.03942   0.03263  -0.0368   0.1677   1.0000
  14.000   1.6218   0.04150   0.03484  -0.0364   0.1624   1.0000
  14.250   1.6219   0.04375   0.03714  -0.0359   0.1566   1.0000
  14.500   1.6177   0.04663   0.04027  -0.0361   0.1496   1.0000
  14.750   1.6118   0.04982   0.04357  -0.0363   0.1414   1.0000
  15.000   1.6045   0.05354   0.04750  -0.0372   0.1264   1.0000
  15.250   1.5870   0.05868   0.05255  -0.0382   0.0928   1.0000
  15.500   1.5602   0.06503   0.05873  -0.0392   0.0747   1.0000
  15.750   1.5354   0.07140   0.06507  -0.0402   0.0627   1.0000
  16.000   1.5125   0.07778   0.07148  -0.0415   0.0554   1.0000
  16.250   1.4909   0.08423   0.07801  -0.0430   0.0508   1.0000
  16.500   1.4701   0.09081   0.08470  -0.0448   0.0479   1.0000
  16.750   1.4509   0.09734   0.09136  -0.0468   0.0457   1.0000
  17.000   1.4306   0.10426   0.09841  -0.0491   0.0442   1.0000
  17.250   1.4096   0.11152   0.10579  -0.0518   0.0431   1.0000
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