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GOE 255 (MVA CA.6) AIRFOIL (goe255-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: GOE 255 (MVA CA.6) AIRFOIL (goe255-il)
Reynolds number: 100,000
Max Cl/Cd: 47.25 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe255-il-100000-n5.txt
Download as CSV file: xf-goe255-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 255 (MVA CA.6) AIRFOIL                      
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.3611   0.11667   0.11171  -0.0642   1.0000   0.0293
 -13.750  -0.4742   0.08947   0.08421  -0.0770   1.0000   0.0276
 -13.500  -0.5125   0.08101   0.07559  -0.0806   1.0000   0.0273
 -13.250  -0.5403   0.07530   0.06976  -0.0823   1.0000   0.0272
 -13.000  -0.5648   0.07085   0.06524  -0.0829   1.0000   0.0271
 -12.750  -0.5795   0.06638   0.06066  -0.0850   0.9975   0.0273
 -12.500  -0.5763   0.06118   0.05528  -0.0908   0.9909   0.0277
 -12.250  -0.5689   0.05645   0.05035  -0.0967   0.9841   0.0284
 -12.000  -0.5599   0.05211   0.04580  -0.1021   0.9754   0.0293
 -11.750  -0.5482   0.04817   0.04159  -0.1071   0.9664   0.0304
 -11.500  -0.5345   0.04487   0.03813  -0.1112   0.9565   0.0314
 -11.250  -0.5210   0.04200   0.03519  -0.1147   0.9453   0.0325
 -11.000  -0.5145   0.03957   0.03263  -0.1162   0.9292   0.0336
 -10.750  -0.5117   0.03762   0.03055  -0.1158   0.9120   0.0346
 -10.500  -0.5037   0.03586   0.02862  -0.1153   0.8987   0.0359
 -10.250  -0.4933   0.03420   0.02680  -0.1149   0.8873   0.0375
 -10.000  -0.4830   0.03270   0.02523  -0.1143   0.8762   0.0396
  -9.750  -0.4674   0.03130   0.02368  -0.1141   0.8676   0.0428
  -9.500  -0.4517   0.02989   0.02218  -0.1138   0.8592   0.0465
  -9.250  -0.4344   0.02866   0.02081  -0.1133   0.8511   0.0516
  -9.000  -0.4158   0.02739   0.01948  -0.1131   0.8439   0.0588
  -8.750  -0.3966   0.02627   0.01828  -0.1128   0.8366   0.0698
  -8.500  -0.3759   0.02523   0.01715  -0.1125   0.8294   0.0833
  -8.250  -0.3532   0.02431   0.01618  -0.1125   0.8230   0.0985
  -8.000  -0.3310   0.02360   0.01543  -0.1122   0.8154   0.1146
  -7.750  -0.3052   0.02292   0.01472  -0.1125   0.8098   0.1344
  -7.500  -0.2820   0.02251   0.01423  -0.1123   0.8019   0.1570
  -7.250  -0.2565   0.02203   0.01373  -0.1124   0.7957   0.1783
  -7.000  -0.2314   0.02160   0.01321  -0.1123   0.7894   0.1960
  -6.750  -0.2067   0.02121   0.01275  -0.1120   0.7825   0.2117
  -6.500  -0.1795   0.02080   0.01225  -0.1121   0.7771   0.2278
  -6.250  -0.1551   0.02052   0.01194  -0.1118   0.7702   0.2433
  -6.000  -0.1289   0.02027   0.01164  -0.1116   0.7639   0.2595
  -5.750  -0.1010   0.02007   0.01139  -0.1117   0.7587   0.2773
  -5.500  -0.0763   0.02002   0.01134  -0.1113   0.7512   0.2948
  -5.250  -0.0483   0.01996   0.01119  -0.1113   0.7453   0.3135
  -5.000  -0.0213   0.01999   0.01109  -0.1112   0.7391   0.3327
  -4.750   0.0050   0.02007   0.01110  -0.1109   0.7323   0.3509
  -4.500   0.0337   0.02012   0.01100  -0.1110   0.7271   0.3682
  -4.250   0.0596   0.02018   0.01094  -0.1107   0.7206   0.3822
  -4.000   0.0866   0.02019   0.01081  -0.1106   0.7146   0.3947
  -3.750   0.1154   0.02013   0.01067  -0.1107   0.7100   0.4050
  -3.500   0.1410   0.02016   0.01060  -0.1105   0.7037   0.4151
  -3.250   0.1679   0.02015   0.01052  -0.1104   0.6981   0.4245
  -3.000   0.1968   0.02009   0.01034  -0.1106   0.6938   0.4337
  -2.750   0.2227   0.02012   0.01032  -0.1104   0.6882   0.4423
  -2.500   0.2491   0.02013   0.01028  -0.1102   0.6826   0.4502
  -2.250   0.2776   0.02008   0.01015  -0.1104   0.6783   0.4585
  -2.000   0.3048   0.02010   0.01010  -0.1104   0.6736   0.4663
  -1.750   0.3300   0.02015   0.01016  -0.1101   0.6678   0.4736
  -1.500   0.3582   0.02015   0.01005  -0.1102   0.6634   0.4817
  -1.250   0.3870   0.02008   0.00995  -0.1104   0.6596   0.4891
  -1.000   0.4107   0.02023   0.01010  -0.1099   0.6533   0.4989
  -0.750   0.4373   0.02021   0.01010  -0.1097   0.6482   0.5088
  -0.500   0.4667   0.02014   0.00996  -0.1100   0.6444   0.5191
  -0.250   0.4901   0.02028   0.01016  -0.1094   0.6386   0.5267
   0.000   0.5166   0.02034   0.01020  -0.1094   0.6340   0.5341
   0.250   0.5449   0.02032   0.01018  -0.1095   0.6305   0.5412
   0.500   0.5721   0.02039   0.01021  -0.1096   0.6267   0.5493
   0.750   0.5952   0.02053   0.01044  -0.1090   0.6212   0.5569
   1.250   0.6512   0.02050   0.01041  -0.1092   0.6133   0.5785
   1.500   0.6744   0.02072   0.01071  -0.1086   0.6088   0.5910
   1.750   0.6987   0.02089   0.01097  -0.1082   0.6048   0.6063
   2.000   0.7250   0.02094   0.01110  -0.1081   0.6012   0.6262
   2.250   0.7534   0.02086   0.01109  -0.1081   0.5979   0.6542
   2.500   0.7736   0.02101   0.01145  -0.1069   0.5928   0.6912
   2.750   0.7942   0.02104   0.01171  -0.1055   0.5880   0.7466
   3.000   0.8201   0.02081   0.01175  -0.1046   0.5840   0.8479
   3.250   0.8586   0.02081   0.01179  -0.1068   0.5794   1.0000
   3.500   0.8785   0.02117   0.01215  -0.1058   0.5735   1.0000
   3.750   0.9051   0.02130   0.01221  -0.1058   0.5689   1.0000
   4.000   0.9349   0.02138   0.01220  -0.1063   0.5653   1.0000
   4.250   0.9511   0.02191   0.01279  -0.1047   0.5597   1.0000
   4.500   0.9746   0.02218   0.01306  -0.1042   0.5548   1.0000
   4.750   1.0038   0.02225   0.01307  -0.1046   0.5506   1.0000
   5.000   1.0217   0.02269   0.01356  -0.1032   0.5447   1.0000
   5.250   1.0426   0.02301   0.01390  -0.1023   0.5387   1.0000
   5.500   1.0724   0.02304   0.01387  -0.1027   0.5338   1.0000
   5.750   1.0858   0.02360   0.01451  -0.1006   0.5269   1.0000
   6.000   1.1075   0.02388   0.01481  -0.0998   0.5207   1.0000
   6.250   1.1345   0.02401   0.01492  -0.0998   0.5153   1.0000
   6.500   1.1435   0.02466   0.01568  -0.0971   0.5074   1.0000
   6.750   1.1695   0.02478   0.01578  -0.0968   0.5011   1.0000
   7.000   1.1745   0.02545   0.01656  -0.0934   0.4925   1.0000
   7.250   1.1951   0.02564   0.01673  -0.0924   0.4843   1.0000
   7.500   1.1955   0.02653   0.01773  -0.0885   0.4735   1.0000
   7.750   1.2072   0.02707   0.01830  -0.0864   0.4634   1.0000
   8.000   1.2153   0.02780   0.01910  -0.0839   0.4525   1.0000
   8.250   1.2164   0.02900   0.02039  -0.0809   0.4401   1.0000
   8.500   1.2211   0.03013   0.02158  -0.0785   0.4279   1.0000
   8.750   1.2279   0.03122   0.02271  -0.0765   0.4158   1.0000
   9.000   1.2367   0.03225   0.02374  -0.0748   0.4037   1.0000
   9.250   1.2465   0.03326   0.02473  -0.0732   0.3921   1.0000
   9.500   1.2560   0.03440   0.02588  -0.0717   0.3816   1.0000
   9.750   1.2691   0.03529   0.02674  -0.0705   0.3729   1.0000
  10.000   1.2821   0.03624   0.02767  -0.0694   0.3649   1.0000
  10.250   1.2956   0.03720   0.02862  -0.0683   0.3579   1.0000
  10.500   1.3083   0.03826   0.02969  -0.0672   0.3512   1.0000
  10.750   1.3240   0.03905   0.03045  -0.0663   0.3445   1.0000
  11.000   1.3318   0.04052   0.03197  -0.0650   0.3363   1.0000
  11.250   1.3433   0.04160   0.03299  -0.0638   0.3272   1.0000
  11.500   1.3488   0.04323   0.03461  -0.0624   0.3172   1.0000
  11.750   1.3539   0.04492   0.03633  -0.0611   0.3078   1.0000
  12.000   1.3616   0.04638   0.03777  -0.0599   0.2986   1.0000
  12.250   1.3637   0.04848   0.03998  -0.0588   0.2908   1.0000
  12.500   1.3687   0.05030   0.04186  -0.0577   0.2830   1.0000
  12.750   1.3691   0.05264   0.04431  -0.0567   0.2748   1.0000
  13.000   1.3685   0.05508   0.04681  -0.0558   0.2656   1.0000
  13.250   1.3639   0.05816   0.05003  -0.0550   0.2563   1.0000
  13.500   1.3622   0.06091   0.05284  -0.0544   0.2471   1.0000
  13.750   1.3567   0.06432   0.05641  -0.0540   0.2371   1.0000
  14.000   1.3519   0.06775   0.05997  -0.0537   0.2268   1.0000
  14.250   1.3468   0.07127   0.06357  -0.0535   0.2156   1.0000
  14.500   1.3416   0.07489   0.06725  -0.0534   0.2037   1.0000
  14.750   1.3353   0.07870   0.07107  -0.0534   0.1910   1.0000
  15.250   1.3208   0.08668   0.07901  -0.0537   0.1683   1.0000
  15.500   1.3140   0.09071   0.08305  -0.0540   0.1594   1.0000
  15.750   1.3058   0.09500   0.08735  -0.0544   0.1512   1.0000
  16.000   1.2991   0.09922   0.09165  -0.0549   0.1429   1.0000
  16.250   1.2894   0.10390   0.09638  -0.0557   0.1348   1.0000
  16.500   1.2795   0.10877   0.10133  -0.0567   0.1242   1.0000
  16.750   1.2700   0.11369   0.10633  -0.0579   0.1130   1.0000
  17.000   1.2607   0.11866   0.11135  -0.0592   0.1019   1.0000
  17.250   1.2496   0.12395   0.11668  -0.0608   0.0907   1.0000
  17.500   1.2384   0.12937   0.12209  -0.0626   0.0810   1.0000
  17.750   1.2272   0.13490   0.12761  -0.0646   0.0699   1.0000
  18.000   1.2120   0.14120   0.13382  -0.0672   0.0430   1.0000
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