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GOE 584 AIRFOIL (goe584-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 584 AIRFOIL (goe584-il)
Reynolds number: 200,000
Max Cl/Cd: 77.92 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe584-il-200000-n5.txt
Download as CSV file: xf-goe584-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 584 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
  ------ -------- --------- --------- -------- -------- --------
 -11.500  -0.3009   0.10994   0.10618  -0.0466   1.0000   0.0296
 -11.250  -0.3111   0.10443   0.10071  -0.0488   1.0000   0.0312
 -11.000  -0.3198   0.09945   0.09578  -0.0504   1.0000   0.0320
 -10.750  -0.3155   0.09768   0.09405  -0.0502   1.0000   0.0324
 -10.500  -0.3052   0.09513   0.09154  -0.0517   0.9916   0.0331
 -10.250  -0.2916   0.09112   0.08751  -0.0560   0.9796   0.0345
 -10.000  -0.3120   0.07814   0.07453  -0.0682   0.9627   0.0376
  -9.750  -0.2867   0.07620   0.07256  -0.0721   0.9501   0.0383
  -9.500  -0.2602   0.07398   0.07029  -0.0765   0.9367   0.0394
  -9.000  -0.3723   0.03524   0.03036  -0.1104   0.8725   0.0453
  -8.750  -0.3483   0.03522   0.03032  -0.1101   0.8618   0.0461
  -8.500  -0.3284   0.03439   0.02937  -0.1098   0.8518   0.0471
  -8.250  -0.3123   0.03284   0.02758  -0.1093   0.8420   0.0485
  -8.000  -0.3010   0.03029   0.02462  -0.1086   0.8322   0.0505
  -7.750  -0.2879   0.02785   0.02157  -0.1076   0.8237   0.0525
  -7.500  -0.2707   0.02614   0.01954  -0.1067   0.8152   0.0538
  -7.250  -0.2483   0.02529   0.01860  -0.1062   0.8077   0.0549
  -7.000  -0.2255   0.02463   0.01784  -0.1056   0.8001   0.0560
  -6.750  -0.2029   0.02380   0.01681  -0.1050   0.7925   0.0572
  -6.500  -0.1798   0.02293   0.01574  -0.1043   0.7858   0.0585
  -6.250  -0.1566   0.02209   0.01469  -0.1037   0.7782   0.0599
  -6.000  -0.1326   0.02126   0.01360  -0.1031   0.7719   0.0611
  -5.750  -0.1087   0.02046   0.01259  -0.1024   0.7645   0.0620
  -5.500  -0.0838   0.01980   0.01171  -0.1019   0.7578   0.0629
  -5.250  -0.0583   0.01931   0.01102  -0.1014   0.7516   0.0637
  -5.000  -0.0340   0.01830   0.00992  -0.1009   0.7446   0.0650
  -4.750  -0.0083   0.01770   0.00920  -0.1005   0.7386   0.0659
  -4.500   0.0173   0.01719   0.00864  -0.1000   0.7317   0.0668
  -4.250   0.0432   0.01674   0.00811  -0.0996   0.7254   0.0678
  -4.000   0.0695   0.01633   0.00761  -0.0992   0.7198   0.0688
  -3.750   0.0953   0.01596   0.00719  -0.0987   0.7128   0.0700
  -3.500   0.1216   0.01564   0.00680  -0.0983   0.7067   0.0715
  -3.250   0.1479   0.01534   0.00643  -0.0979   0.7011   0.0730
  -3.000   0.1739   0.01504   0.00609  -0.0974   0.6946   0.0741
  -2.750   0.2003   0.01478   0.00574  -0.0970   0.6890   0.0751
  -2.500   0.2264   0.01455   0.00547  -0.0965   0.6830   0.0760
  -2.250   0.2520   0.01423   0.00515  -0.0960   0.6769   0.0776
  -2.000   0.2780   0.01399   0.00488  -0.0956   0.6717   0.0795
  -1.750   0.3040   0.01382   0.00471  -0.0952   0.6657   0.0818
  -1.500   0.3301   0.01368   0.00455  -0.0947   0.6596   0.0848
  -1.250   0.3568   0.01358   0.00438  -0.0944   0.6546   0.0884
  -1.000   0.3827   0.01344   0.00427  -0.0939   0.6485   0.0928
  -0.750   0.4088   0.01332   0.00416  -0.0935   0.6425   0.0996
  -0.500   0.4352   0.01320   0.00404  -0.0931   0.6374   0.1122
  -0.250   0.4605   0.01303   0.00404  -0.0926   0.6309   0.1478
   0.000   0.4860   0.01288   0.00402  -0.0921   0.6247   0.1972
   0.250   0.5115   0.01274   0.00400  -0.0916   0.6189   0.2457
   0.500   0.5356   0.01251   0.00405  -0.0910   0.6120   0.3265
   0.750   0.5581   0.01212   0.00407  -0.0900   0.6063   0.4613
   1.000   0.6305   0.01104   0.00426  -0.0987   0.5992   0.9769
   1.250   0.6721   0.01115   0.00428  -0.1016   0.5925   1.0000
   1.750   0.7199   0.01138   0.00437  -0.0999   0.5804   1.0000
   2.000   0.7438   0.01150   0.00442  -0.0990   0.5741   1.0000
   2.250   0.7678   0.01163   0.00448  -0.0982   0.5683   1.0000
   2.500   0.7914   0.01176   0.00459  -0.0973   0.5614   1.0000
   2.750   0.8154   0.01190   0.00466  -0.0965   0.5553   1.0000
   3.000   0.8390   0.01203   0.00478  -0.0956   0.5485   1.0000
   3.250   0.8626   0.01218   0.00489  -0.0947   0.5415   1.0000
   3.500   0.8864   0.01233   0.00500  -0.0939   0.5349   1.0000
   3.750   0.9098   0.01248   0.00516  -0.0930   0.5274   1.0000
   4.000   0.9335   0.01265   0.00526  -0.0921   0.5207   1.0000
   4.250   0.9566   0.01281   0.00545  -0.0912   0.5126   1.0000
   4.500   0.9799   0.01299   0.00559  -0.0903   0.5051   1.0000
   4.750   1.0027   0.01316   0.00579  -0.0893   0.4966   1.0000
   5.000   1.0255   0.01336   0.00594  -0.0884   0.4886   1.0000
   5.250   1.0479   0.01355   0.00617  -0.0873   0.4793   1.0000
   5.500   1.0696   0.01376   0.00635  -0.0862   0.4691   1.0000
   5.750   1.0900   0.01399   0.00653  -0.0848   0.4560   1.0000
   6.000   1.1096   0.01424   0.00676  -0.0833   0.4410   1.0000
   6.250   1.1288   0.01451   0.00700  -0.0818   0.4261   1.0000
   6.500   1.1482   0.01481   0.00727  -0.0803   0.4128   1.0000
   6.750   1.1672   0.01512   0.00758  -0.0788   0.4006   1.0000
   7.000   1.1851   0.01547   0.00790  -0.0771   0.3880   1.0000
   7.500   1.2190   0.01623   0.00862  -0.0735   0.3636   1.0000
   7.750   1.2347   0.01664   0.00903  -0.0715   0.3519   1.0000
   8.000   1.2477   0.01709   0.00945  -0.0690   0.3405   1.0000
   8.250   1.2593   0.01758   0.00992  -0.0664   0.3288   1.0000
   8.500   1.2720   0.01807   0.01043  -0.0640   0.3178   1.0000
   8.750   1.2833   0.01864   0.01098  -0.0615   0.3076   1.0000
   9.000   1.2948   0.01924   0.01158  -0.0592   0.2972   1.0000
   9.250   1.3068   0.01985   0.01222  -0.0570   0.2872   1.0000
   9.500   1.3166   0.02058   0.01296  -0.0547   0.2772   1.0000
   9.750   1.3258   0.02139   0.01377  -0.0524   0.2654   1.0000
  10.000   1.3336   0.02230   0.01467  -0.0502   0.2520   1.0000
  10.250   1.3397   0.02336   0.01571  -0.0479   0.2375   1.0000
  10.500   1.3450   0.02455   0.01687  -0.0457   0.2230   1.0000
  10.750   1.3505   0.02580   0.01811  -0.0437   0.2097   1.0000
  11.000   1.3559   0.02714   0.01944  -0.0418   0.1974   1.0000
  11.250   1.3598   0.02864   0.02092  -0.0400   0.1851   1.0000
  11.500   1.3634   0.03024   0.02250  -0.0384   0.1742   1.0000
  11.750   1.3688   0.03176   0.02404  -0.0370   0.1636   1.0000
  12.000   1.3722   0.03350   0.02578  -0.0356   0.1555   1.0000
  12.250   1.3780   0.03512   0.02745  -0.0344   0.1474   1.0000
  12.500   1.3795   0.03711   0.02945  -0.0331   0.1403   1.0000
  12.750   1.3857   0.03878   0.03118  -0.0322   0.1335   1.0000
  13.000   1.3878   0.04085   0.03328  -0.0312   0.1268   1.0000
  13.250   1.3907   0.04291   0.03539  -0.0303   0.1200   1.0000
  13.500   1.3923   0.04516   0.03767  -0.0296   0.1125   1.0000
  13.750   1.3937   0.04751   0.04005  -0.0289   0.1060   1.0000
  14.000   1.3962   0.04982   0.04243  -0.0284   0.0992   1.0000
  14.250   1.3966   0.05240   0.04506  -0.0280   0.0917   1.0000
  14.500   1.3949   0.05530   0.04797  -0.0277   0.0806   1.0000
  14.750   1.3909   0.05855   0.05120  -0.0276   0.0667   1.0000
  15.000   1.3800   0.06269   0.05523  -0.0276   0.0485   1.0000
  15.250   1.3696   0.06692   0.05941  -0.0278   0.0399   1.0000
  15.500   1.3604   0.07114   0.06364  -0.0282   0.0351   1.0000
  15.750   1.3554   0.07493   0.06752  -0.0286   0.0328   1.0000
  16.000   1.3486   0.07908   0.07175  -0.0293   0.0306   1.0000
  16.250   1.3410   0.08345   0.07622  -0.0301   0.0291   1.0000
  16.500   1.3342   0.08781   0.08071  -0.0311   0.0281   1.0000
  16.750   1.3289   0.09205   0.08508  -0.0321   0.0268   1.0000
  17.000   1.3226   0.09652   0.08968  -0.0334   0.0259   1.0000
  17.250   1.3153   0.10124   0.09453  -0.0348   0.0252   1.0000
  17.500   1.3063   0.10634   0.09975  -0.0365   0.0245   1.0000
  17.750   1.2961   0.11169   0.10522  -0.0385   0.0239   1.0000
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