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GOE 619 AIRFOIL (goe619-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 619 AIRFOIL (goe619-il)
Reynolds number: 500,000
Max Cl/Cd: 82.04 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe619-il-500000-n5.txt
Download as CSV file: xf-goe619-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 619 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
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.6817   0.08353   0.08035  -0.0671   1.0000   0.0254
 -14.750  -0.7166   0.07470   0.07138  -0.0722   1.0000   0.0254
 -14.500  -0.7473   0.06734   0.06391  -0.0764   1.0000   0.0255
 -14.250  -0.7727   0.06122   0.05769  -0.0796   1.0000   0.0255
 -14.000  -0.7986   0.05528   0.05166  -0.0827   1.0000   0.0255
 -13.750  -0.8247   0.04960   0.04588  -0.0855   1.0000   0.0257
 -13.500  -0.8518   0.04427   0.04048  -0.0877   1.0000   0.0257
 -13.250  -0.8591   0.03727   0.03329  -0.0970   0.9973   0.0258
 -13.000  -0.8497   0.03251   0.02826  -0.1052   0.9895   0.0260
 -12.750  -0.8292   0.03028   0.02584  -0.1085   0.9842   0.0263
 -12.500  -0.8101   0.02861   0.02402  -0.1099   0.9780   0.0264
 -12.250  -0.7901   0.02675   0.02203  -0.1115   0.9726   0.0268
 -12.000  -0.7721   0.02522   0.02042  -0.1120   0.9656   0.0272
 -11.750  -0.7485   0.02398   0.01911  -0.1129   0.9602   0.0276
 -11.500  -0.7239   0.02291   0.01796  -0.1137   0.9547   0.0279
 -11.250  -0.6978   0.02192   0.01688  -0.1145   0.9484   0.0282
 -11.000  -0.6660   0.02093   0.01579  -0.1164   0.9444   0.0286
 -10.750  -0.6380   0.02007   0.01483  -0.1174   0.9377   0.0289
 -10.500  -0.6067   0.01926   0.01393  -0.1188   0.9318   0.0294
 -10.250  -0.5748   0.01849   0.01306  -0.1203   0.9254   0.0299
 -10.000  -0.5446   0.01780   0.01227  -0.1214   0.9170   0.0303
  -9.750  -0.5143   0.01714   0.01149  -0.1223   0.9087   0.0306
  -9.500  -0.4865   0.01656   0.01080  -0.1227   0.8993   0.0309
  -9.250  -0.4595   0.01606   0.01019  -0.1228   0.8901   0.0312
  -9.000  -0.4330   0.01559   0.00962  -0.1227   0.8802   0.0314
  -8.750  -0.4096   0.01501   0.00895  -0.1221   0.8699   0.0319
  -8.500  -0.3851   0.01449   0.00834  -0.1217   0.8605   0.0324
  -8.250  -0.3611   0.01406   0.00784  -0.1211   0.8510   0.0328
  -8.000  -0.3362   0.01366   0.00736  -0.1206   0.8425   0.0335
  -7.750  -0.3114   0.01332   0.00694  -0.1200   0.8332   0.0341
  -7.500  -0.2862   0.01301   0.00655  -0.1195   0.8245   0.0348
  -7.250  -0.2610   0.01271   0.00618  -0.1189   0.8154   0.0354
  -7.000  -0.2354   0.01245   0.00583  -0.1184   0.8076   0.0359
  -6.750  -0.2098   0.01219   0.00550  -0.1178   0.7991   0.0366
  -6.500  -0.1840   0.01197   0.00519  -0.1173   0.7911   0.0372
  -6.250  -0.1585   0.01169   0.00486  -0.1168   0.7826   0.0385
  -6.000  -0.1326   0.01146   0.00457  -0.1163   0.7750   0.0400
  -5.750  -0.1067   0.01123   0.00431  -0.1158   0.7669   0.0420
  -5.500  -0.0808   0.01102   0.00405  -0.1152   0.7594   0.0455
  -5.250  -0.0551   0.01074   0.00382  -0.1147   0.7514   0.0559
  -5.000  -0.0291   0.01057   0.00367  -0.1143   0.7441   0.0700
  -4.750  -0.0023   0.01046   0.00354  -0.1139   0.7366   0.0777
  -4.500   0.0241   0.01034   0.00341  -0.1135   0.7290   0.0842
  -4.250   0.0510   0.01027   0.00329  -0.1131   0.7219   0.0882
  -4.000   0.0776   0.01017   0.00316  -0.1126   0.7141   0.0922
  -3.750   0.1042   0.01008   0.00304  -0.1122   0.7068   0.0961
  -3.500   0.1309   0.01000   0.00293  -0.1118   0.6989   0.0995
  -3.250   0.1576   0.00996   0.00283  -0.1113   0.6912   0.1025
  -3.000   0.1838   0.00986   0.00272  -0.1108   0.6817   0.1077
  -2.750   0.2097   0.00980   0.00261  -0.1103   0.6704   0.1124
  -2.500   0.2351   0.00977   0.00252  -0.1096   0.6569   0.1170
  -2.250   0.2604   0.00972   0.00243  -0.1089   0.6437   0.1244
  -2.000   0.2864   0.00963   0.00235  -0.1083   0.6333   0.1358
  -1.750   0.3121   0.00954   0.00230  -0.1078   0.6251   0.1550
  -1.500   0.3385   0.00945   0.00227  -0.1073   0.6166   0.1795
  -1.000   0.3911   0.00937   0.00225  -0.1064   0.6018   0.2171
  -0.750   0.4173   0.00937   0.00225  -0.1059   0.5939   0.2301
  -0.500   0.4439   0.00936   0.00225  -0.1055   0.5860   0.2421
  -0.250   0.4696   0.00938   0.00226  -0.1049   0.5765   0.2525
   0.000   0.4958   0.00940   0.00227  -0.1044   0.5659   0.2621
   0.250   0.5213   0.00943   0.00229  -0.1038   0.5548   0.2715
   0.500   0.5466   0.00948   0.00231  -0.1031   0.5429   0.2820
   0.750   0.5720   0.00952   0.00235  -0.1025   0.5301   0.2935
   1.000   0.5970   0.00958   0.00239  -0.1017   0.5160   0.3028
   1.250   0.6212   0.00966   0.00244  -0.1009   0.4999   0.3166
   1.750   0.6677   0.00990   0.00261  -0.0988   0.4619   0.3477
   2.000   0.6902   0.01005   0.00272  -0.0977   0.4406   0.3648
   2.250   0.7121   0.01023   0.00286  -0.0965   0.4180   0.3878
   2.500   0.7334   0.01042   0.00302  -0.0952   0.3960   0.4142
   2.750   0.7547   0.01064   0.00318  -0.0939   0.3733   0.4360
   3.000   0.7758   0.01085   0.00336  -0.0925   0.3524   0.4601
   3.500   0.8172   0.01119   0.00371  -0.0898   0.3173   0.5266
   3.750   0.8263   0.01057   0.00397  -0.0858   0.3073   0.8407
   4.250   0.9136   0.01117   0.00452  -0.0929   0.2768   1.0000
   4.500   0.9347   0.01140   0.00470  -0.0915   0.2678   1.0000
   4.750   0.9553   0.01165   0.00489  -0.0901   0.2592   1.0000
   5.000   0.9758   0.01190   0.00509  -0.0887   0.2510   1.0000
   5.250   0.9959   0.01215   0.00530  -0.0871   0.2440   1.0000
   5.500   1.0156   0.01238   0.00550  -0.0855   0.2380   1.0000
   5.750   1.0342   0.01263   0.00571  -0.0837   0.2330   1.0000
   6.000   1.0533   0.01287   0.00594  -0.0820   0.2287   1.0000
   6.250   1.0729   0.01309   0.00616  -0.0805   0.2246   1.0000
   6.500   1.0920   0.01335   0.00641  -0.0788   0.2203   1.0000
   6.750   1.1099   0.01366   0.00669  -0.0770   0.2154   1.0000
   7.000   1.1293   0.01392   0.00695  -0.0755   0.2116   1.0000
   7.250   1.1482   0.01421   0.00724  -0.0740   0.2057   1.0000
   7.500   1.1653   0.01458   0.00757  -0.0722   0.1998   1.0000
   7.750   1.1841   0.01488   0.00788  -0.0707   0.1937   1.0000
   8.000   1.2014   0.01526   0.00823  -0.0690   0.1865   1.0000
   8.250   1.2188   0.01565   0.00860  -0.0673   0.1792   1.0000
   8.500   1.2350   0.01610   0.00901  -0.0656   0.1704   1.0000
   8.750   1.2506   0.01659   0.00946  -0.0638   0.1587   1.0000
   9.000   1.2612   0.01735   0.01009  -0.0614   0.1373   1.0000
   9.250   1.2591   0.01884   0.01128  -0.0575   0.0946   1.0000
   9.500   1.2577   0.02040   0.01265  -0.0540   0.0649   1.0000
   9.750   1.2695   0.02124   0.01347  -0.0521   0.0596   1.0000
  10.000   1.2829   0.02199   0.01424  -0.0505   0.0569   1.0000
  10.250   1.2959   0.02280   0.01507  -0.0489   0.0547   1.0000
  10.500   1.3082   0.02368   0.01596  -0.0474   0.0522   1.0000
  10.750   1.3216   0.02450   0.01683  -0.0460   0.0507   1.0000
  11.000   1.3351   0.02534   0.01771  -0.0447   0.0490   1.0000
  11.250   1.3475   0.02628   0.01868  -0.0434   0.0473   1.0000
  11.500   1.3579   0.02738   0.01981  -0.0420   0.0450   1.0000
  11.750   1.3683   0.02853   0.02098  -0.0407   0.0432   1.0000
  12.000   1.3805   0.02956   0.02205  -0.0396   0.0402   1.0000
  12.250   1.3894   0.03087   0.02336  -0.0384   0.0367   1.0000
  12.500   1.3876   0.03309   0.02547  -0.0366   0.0173   1.0000
  12.750   1.3882   0.03522   0.02764  -0.0352   0.0144   1.0000
  13.000   1.3932   0.03703   0.02953  -0.0341   0.0135   1.0000
  13.250   1.3970   0.03902   0.03161  -0.0331   0.0128   1.0000
  13.500   1.4003   0.04112   0.03379  -0.0323   0.0122   1.0000
  13.750   1.4052   0.04311   0.03587  -0.0316   0.0119   1.0000
  14.000   1.4086   0.04532   0.03816  -0.0310   0.0115   1.0000
  14.250   1.4113   0.04766   0.04059  -0.0305   0.0112   1.0000
  14.500   1.4133   0.05014   0.04316  -0.0301   0.0109   1.0000
  14.750   1.4132   0.05292   0.04603  -0.0298   0.0106   1.0000
  15.000   1.4111   0.05601   0.04923  -0.0296   0.0103   1.0000
  15.250   1.4088   0.05922   0.05254  -0.0297   0.0102   1.0000
  15.500   1.4048   0.06272   0.05615  -0.0298   0.0099   1.0000
  15.750   1.4035   0.06596   0.05949  -0.0301   0.0097   1.0000
  16.000   1.3997   0.06962   0.06326  -0.0306   0.0096   1.0000
  16.250   1.3958   0.07339   0.06713  -0.0312   0.0094   1.0000
  16.500   1.3903   0.07746   0.07131  -0.0320   0.0092   1.0000
  16.750   1.3831   0.08185   0.07582  -0.0330   0.0091   1.0000
  17.000   1.3753   0.08644   0.08051  -0.0342   0.0090   1.0000
  17.250   1.3669   0.09122   0.08541  -0.0355   0.0089   1.0000
  17.500   1.3568   0.09634   0.09066  -0.0371   0.0088   1.0000
  17.750   1.3463   0.10162   0.09605  -0.0388   0.0087   1.0000
  18.000   1.3365   0.10686   0.10140  -0.0407   0.0086   1.0000
  18.250   1.3259   0.11232   0.10697  -0.0427   0.0085   1.0000
  18.500   1.3151   0.11787   0.11263  -0.0449   0.0084   1.0000
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