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GOE 367 AIRFOIL (goe367-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 367 AIRFOIL (goe367-il)
Reynolds number: 500,000
Max Cl/Cd: 83.71 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe367-il-500000-n5.txt
Download as CSV file: xf-goe367-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 367 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.8298   0.04997   0.04633  -0.1049   1.0000   0.0301
 -15.000  -0.8531   0.04181   0.03786  -0.1136   0.9903   0.0301
 -14.750  -0.8579   0.03759   0.03339  -0.1173   0.9795   0.0302
 -14.500  -0.8577   0.03477   0.03039  -0.1184   0.9687   0.0304
 -14.250  -0.8554   0.03282   0.02832  -0.1179   0.9571   0.0305
 -14.000  -0.8515   0.03130   0.02669  -0.1165   0.9460   0.0307
 -13.750  -0.8460   0.03005   0.02532  -0.1147   0.9356   0.0309
 -13.500  -0.8390   0.02897   0.02414  -0.1127   0.9249   0.0310
 -13.250  -0.8306   0.02808   0.02314  -0.1106   0.9150   0.0312
 -13.000  -0.8193   0.02728   0.02223  -0.1087   0.9056   0.0315
 -12.750  -0.8046   0.02650   0.02135  -0.1073   0.8968   0.0317
 -12.500  -0.7891   0.02572   0.02046  -0.1060   0.8886   0.0320
 -12.250  -0.7724   0.02493   0.01955  -0.1048   0.8808   0.0323
 -12.000  -0.7552   0.02413   0.01861  -0.1037   0.8729   0.0326
 -11.750  -0.7370   0.02334   0.01768  -0.1026   0.8658   0.0329
 -11.500  -0.7179   0.02258   0.01679  -0.1017   0.8579   0.0332
 -11.250  -0.6981   0.02186   0.01592  -0.1007   0.8509   0.0335
 -11.000  -0.6772   0.02117   0.01510  -0.0999   0.8439   0.0338
 -10.750  -0.6557   0.02053   0.01432  -0.0992   0.8373   0.0342
 -10.500  -0.6335   0.01995   0.01359  -0.0985   0.8314   0.0344
 -10.250  -0.6114   0.01930   0.01286  -0.0979   0.8248   0.0347
 -10.000  -0.5888   0.01874   0.01223  -0.0972   0.8185   0.0351
  -9.750  -0.5651   0.01827   0.01170  -0.0967   0.8130   0.0355
  -9.500  -0.5409   0.01784   0.01121  -0.0963   0.8069   0.0358
  -9.250  -0.5165   0.01746   0.01075  -0.0958   0.8000   0.0363
  -9.000  -0.4917   0.01710   0.01031  -0.0954   0.7930   0.0368
  -8.750  -0.4668   0.01672   0.00986  -0.0950   0.7857   0.0374
  -8.500  -0.4418   0.01635   0.00939  -0.0946   0.7799   0.0379
  -8.250  -0.4164   0.01597   0.00893  -0.0943   0.7747   0.0384
  -8.000  -0.3907   0.01561   0.00850  -0.0940   0.7694   0.0389
  -7.750  -0.3650   0.01528   0.00808  -0.0937   0.7642   0.0393
  -7.500  -0.3399   0.01486   0.00763  -0.0933   0.7597   0.0399
  -7.250  -0.3139   0.01454   0.00729  -0.0931   0.7548   0.0405
  -7.000  -0.2876   0.01426   0.00697  -0.0929   0.7498   0.0412
  -6.750  -0.2613   0.01400   0.00666  -0.0927   0.7452   0.0419
  -6.500  -0.2347   0.01375   0.00636  -0.0925   0.7408   0.0427
  -6.250  -0.2079   0.01351   0.00608  -0.0923   0.7360   0.0436
  -6.000  -0.1810   0.01330   0.00582  -0.0922   0.7312   0.0444
  -5.750  -0.1549   0.01301   0.00550  -0.0919   0.7267   0.0454
  -5.500  -0.1283   0.01277   0.00525  -0.0917   0.7222   0.0463
  -5.250  -0.1013   0.01256   0.00502  -0.0916   0.7173   0.0474
  -5.000  -0.0744   0.01237   0.00480  -0.0915   0.7123   0.0486
  -4.750  -0.0474   0.01221   0.00458  -0.0913   0.7075   0.0497
  -4.500  -0.0203   0.01202   0.00438  -0.0912   0.7026   0.0509
  -4.250   0.0065   0.01180   0.00417  -0.0910   0.6971   0.0526
  -4.000   0.0334   0.01165   0.00398  -0.0908   0.6914   0.0544
  -3.750   0.0604   0.01151   0.00382  -0.0907   0.6851   0.0562
  -3.500   0.0872   0.01136   0.00364  -0.0905   0.6768   0.0582
  -3.250   0.1137   0.01122   0.00348  -0.0902   0.6686   0.0608
  -3.000   0.1407   0.01110   0.00335  -0.0901   0.6601   0.0638
  -2.750   0.1672   0.01098   0.00322  -0.0898   0.6530   0.0688
  -2.500   0.1943   0.01085   0.00314  -0.0897   0.6458   0.0772
  -2.250   0.2210   0.01076   0.00308  -0.0895   0.6380   0.0897
  -2.000   0.2480   0.01070   0.00303  -0.0894   0.6298   0.1001
  -1.750   0.2747   0.01066   0.00298  -0.0892   0.6203   0.1081
  -1.500   0.3016   0.01064   0.00294  -0.0890   0.6107   0.1150
  -1.250   0.3279   0.01062   0.00290  -0.0887   0.6010   0.1207
  -1.000   0.3547   0.01060   0.00287  -0.0886   0.5910   0.1268
  -0.750   0.3810   0.01063   0.00284  -0.0883   0.5813   0.1317
  -0.500   0.4071   0.01062   0.00283  -0.0880   0.5708   0.1382
  -0.250   0.4331   0.01064   0.00282  -0.0877   0.5607   0.1443
   0.000   0.4586   0.01068   0.00282  -0.0873   0.5502   0.1514
   0.250   0.4846   0.01069   0.00283  -0.0870   0.5406   0.1603
   0.500   0.5097   0.01072   0.00286  -0.0865   0.5314   0.1721
   0.750   0.5356   0.01068   0.00288  -0.0863   0.5233   0.1952
   1.000   0.5592   0.01051   0.00293  -0.0857   0.5152   0.2777
   1.250   0.5791   0.00986   0.00297  -0.0846   0.5083   0.5121
   1.500   0.5878   0.00901   0.00327  -0.0803   0.5013   0.8636
   1.750   0.6094   0.00918   0.00344  -0.0787   0.4933   0.9028
   2.000   0.6323   0.00933   0.00357  -0.0776   0.4841   0.9201
   2.250   0.6549   0.00952   0.00371  -0.0764   0.4742   0.9326
   2.500   0.6780   0.00970   0.00384  -0.0754   0.4636   0.9424
   2.750   0.7010   0.00986   0.00395  -0.0743   0.4543   0.9515
   3.000   0.7266   0.01008   0.00410  -0.0739   0.4441   0.9592
   3.250   0.7511   0.01025   0.00423  -0.0733   0.4341   0.9671
   3.500   0.7803   0.01048   0.00439  -0.0738   0.4240   0.9710
   3.750   0.8095   0.01066   0.00453  -0.0743   0.4150   0.9745
   4.000   0.8371   0.01089   0.00470  -0.0745   0.4074   0.9799
   4.250   0.8714   0.01110   0.00488  -0.0762   0.3995   0.9831
   4.500   0.9090   0.01139   0.00511  -0.0786   0.3916   0.9865
   4.750   0.9473   0.01163   0.00533  -0.0812   0.3843   0.9904
   5.000   0.9742   0.01187   0.00553  -0.0814   0.3776   0.9928
   5.250   1.0022   0.01209   0.00572  -0.0818   0.3707   0.9942
   5.500   1.0285   0.01235   0.00593  -0.0820   0.3613   0.9961
   5.750   1.0537   0.01261   0.00616  -0.0819   0.3540   0.9984
   6.000   1.0706   0.01279   0.00634  -0.0801   0.3483   1.0000
   6.250   1.0712   0.01293   0.00648  -0.0749   0.3441   1.0000
   6.500   1.0780   0.01313   0.00666  -0.0710   0.3400   1.0000
   6.750   1.0937   0.01334   0.00688  -0.0690   0.3356   1.0000
   7.000   1.1110   0.01360   0.00714  -0.0674   0.3307   1.0000
   7.250   1.1284   0.01394   0.00746  -0.0659   0.3257   1.0000
   7.500   1.1474   0.01426   0.00778  -0.0647   0.3215   1.0000
   7.750   1.1679   0.01455   0.00810  -0.0638   0.3172   1.0000
   8.000   1.1873   0.01491   0.00846  -0.0628   0.3126   1.0000
   8.250   1.2057   0.01534   0.00888  -0.0616   0.3080   1.0000
   8.500   1.2255   0.01572   0.00928  -0.0608   0.3040   1.0000
   8.750   1.2456   0.01610   0.00969  -0.0599   0.2993   1.0000
   9.000   1.2641   0.01656   0.01016  -0.0590   0.2940   1.0000
   9.250   1.2816   0.01710   0.01070  -0.0579   0.2884   1.0000
   9.500   1.2998   0.01761   0.01122  -0.0569   0.2800   1.0000
   9.750   1.3150   0.01830   0.01189  -0.0557   0.2697   1.0000
  10.000   1.3278   0.01915   0.01268  -0.0542   0.2532   1.0000
  10.250   1.3299   0.02066   0.01400  -0.0516   0.2161   1.0000
  10.500   1.3206   0.02301   0.01607  -0.0479   0.1726   1.0000
  10.750   1.3256   0.02451   0.01752  -0.0460   0.1593   1.0000
  11.000   1.3339   0.02585   0.01884  -0.0445   0.1495   1.0000
  11.250   1.3432   0.02714   0.02013  -0.0431   0.1404   1.0000
  11.500   1.3494   0.02868   0.02165  -0.0416   0.1268   1.0000
  11.750   1.3450   0.03109   0.02389  -0.0394   0.0967   1.0000
  12.000   1.3468   0.03310   0.02586  -0.0379   0.0879   1.0000
  12.250   1.3538   0.03476   0.02755  -0.0368   0.0849   1.0000
  12.500   1.3604   0.03650   0.02932  -0.0358   0.0824   1.0000
  12.750   1.3656   0.03841   0.03127  -0.0348   0.0800   1.0000
  13.000   1.3723   0.04022   0.03314  -0.0340   0.0781   1.0000
  13.250   1.3798   0.04199   0.03498  -0.0332   0.0766   1.0000
  13.500   1.3853   0.04400   0.03704  -0.0325   0.0749   1.0000
  13.750   1.3890   0.04624   0.03934  -0.0318   0.0732   1.0000
  14.000   1.3910   0.04868   0.04184  -0.0311   0.0717   1.0000
  14.250   1.3912   0.05135   0.04458  -0.0305   0.0702   1.0000
  14.500   1.3987   0.05332   0.04663  -0.0301   0.0690   1.0000
  14.750   1.4040   0.05555   0.04894  -0.0298   0.0675   1.0000
  15.000   1.4078   0.05799   0.05145  -0.0295   0.0658   1.0000
  15.250   1.4093   0.06070   0.05423  -0.0293   0.0642   1.0000
  15.500   1.4084   0.06374   0.05732  -0.0290   0.0626   1.0000
  15.750   1.4115   0.06634   0.06000  -0.0290   0.0611   1.0000
  16.000   1.4154   0.06887   0.06260  -0.0289   0.0591   1.0000
  16.250   1.4167   0.07174   0.06553  -0.0289   0.0568   1.0000
  16.500   1.4158   0.07491   0.06875  -0.0290   0.0548   1.0000
  16.750   1.4180   0.07769   0.07161  -0.0291   0.0522   1.0000
  17.000   1.4174   0.08084   0.07480  -0.0293   0.0494   1.0000
  17.250   1.4161   0.08412   0.07813  -0.0295   0.0466   1.0000
  17.500   1.4143   0.08748   0.08152  -0.0299   0.0436   1.0000
  17.750   1.4113   0.09102   0.08511  -0.0303   0.0412   1.0000
  18.000   1.4077   0.09465   0.08879  -0.0307   0.0389   1.0000
  18.250   1.4043   0.09826   0.09244  -0.0313   0.0370   1.0000
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