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GOE 476 AIRFOIL (goe476-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: GOE 476 AIRFOIL (goe476-il)
Reynolds number: 200,000
Max Cl/Cd: 75.19 at α=7.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe476-il-200000.txt
Download as CSV file: xf-goe476-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 476 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
  ------ -------- --------- --------- -------- -------- --------
  -9.500  -0.1513   0.09904   0.09532  -0.0695   0.9713   0.0877
  -9.250  -0.1280   0.09545   0.09172  -0.0739   0.9675   0.0899
  -9.000  -0.1455   0.08895   0.08522  -0.0888   0.9545   0.0948
  -8.750  -0.1093   0.08575   0.08199  -0.0884   0.9524   0.0956
  -8.500  -0.0814   0.08327   0.07951  -0.0888   0.9442   0.0971
  -8.250  -0.0535   0.07991   0.07612  -0.0934   0.9387   0.0996
  -8.000  -0.0644   0.07176   0.06791  -0.1125   0.9207   0.1055
  -7.750  -0.0280   0.06957   0.06570  -0.1113   0.9137   0.1065
  -7.500   0.0056   0.06701   0.06309  -0.1136   0.9048   0.1081
  -7.250   0.0251   0.06426   0.06028  -0.1168   0.8898   0.1112
  -7.000  -0.0171   0.05753   0.05324  -0.1262   0.8639   0.1173
  -6.750   0.0051   0.05602   0.05175  -0.1245   0.8521   0.1182
  -6.500  -0.0627   0.03978   0.03456  -0.1266   0.8346   0.0951
  -6.250  -0.0411   0.03856   0.03331  -0.1262   0.8254   0.0958
  -6.000  -0.0345   0.03518   0.02967  -0.1244   0.8146   0.0924
  -5.750  -0.0307   0.03124   0.02527  -0.1224   0.8057   0.0915
  -5.500  -0.0241   0.02795   0.02153  -0.1198   0.7962   0.0911
  -5.250  -0.0091   0.02542   0.01851  -0.1182   0.7892   0.0916
  -5.000   0.0054   0.02376   0.01649  -0.1160   0.7803   0.0928
  -4.750   0.0264   0.02252   0.01480  -0.1146   0.7737   0.0944
  -4.500   0.0483   0.02143   0.01361  -0.1137   0.7668   0.0960
  -4.250   0.0716   0.02084   0.01297  -0.1128   0.7597   0.0975
  -4.000   0.0979   0.02025   0.01224  -0.1124   0.7539   0.0994
  -3.750   0.1213   0.01971   0.01158  -0.1114   0.7474   0.1016
  -3.500   0.1453   0.01922   0.01087  -0.1104   0.7407   0.1043
  -3.250   0.1722   0.01854   0.01011  -0.1101   0.7354   0.1069
  -3.000   0.1973   0.01826   0.00983  -0.1095   0.7298   0.1095
  -2.750   0.2216   0.01796   0.00947  -0.1086   0.7235   0.1127
  -2.500   0.2488   0.01768   0.00902  -0.1081   0.7180   0.1166
  -2.250   0.2758   0.01731   0.00869  -0.1079   0.7129   0.1208
  -2.000   0.2990   0.01714   0.00853  -0.1068   0.7063   0.1255
  -1.750   0.3257   0.01682   0.00813  -0.1063   0.7008   0.1310
  -1.500   0.3543   0.01667   0.00798  -0.1062   0.6962   0.1379
  -1.250   0.3770   0.01650   0.00782  -0.1051   0.6902   0.1458
  -1.000   0.4020   0.01636   0.00773  -0.1044   0.6844   0.1551
  -0.750   0.4296   0.01612   0.00749  -0.1041   0.6795   0.1666
  -0.500   0.4549   0.01601   0.00738  -0.1035   0.6742   0.1797
  -0.250   0.4779   0.01595   0.00737  -0.1024   0.6678   0.1923
   0.000   0.5044   0.01577   0.00722  -0.1020   0.6624   0.2054
   0.250   0.5328   0.01569   0.00712  -0.1020   0.6578   0.2188
   0.500   0.5537   0.01571   0.00721  -0.1005   0.6515   0.2311
   0.750   0.5784   0.01560   0.00718  -0.0998   0.6459   0.2452
   1.000   0.6061   0.01551   0.00712  -0.0996   0.6413   0.2620
   1.250   0.6286   0.01549   0.00722  -0.0985   0.6360   0.2826
   1.500   0.6493   0.01537   0.00730  -0.0970   0.6300   0.3167
   1.750   0.8227   0.01384   0.00730  -0.1268   0.6222   1.0000
   2.000   0.8422   0.01403   0.00745  -0.1251   0.6153   1.0000
   2.250   0.8641   0.01416   0.00752  -0.1238   0.6089   1.0000
   2.500   0.8901   0.01428   0.00751  -0.1232   0.6037   1.0000
   2.750   0.9103   0.01450   0.00773  -0.1217   0.5979   1.0000
   3.000   0.9309   0.01468   0.00790  -0.1201   0.5919   1.0000
   3.250   0.9555   0.01482   0.00796  -0.1194   0.5869   1.0000
   3.500   0.9796   0.01501   0.00808  -0.1185   0.5817   1.0000
   3.750   0.9970   0.01520   0.00831  -0.1164   0.5751   1.0000
   4.000   1.0203   0.01534   0.00841  -0.1154   0.5698   1.0000
   4.250   1.0471   0.01550   0.00848  -0.1150   0.5656   1.0000
   4.500   1.0634   0.01574   0.00879  -0.1128   0.5595   1.0000
   4.750   1.0840   0.01588   0.00893  -0.1112   0.5535   1.0000
   5.000   1.1095   0.01597   0.00894  -0.1106   0.5485   1.0000
   5.250   1.1276   0.01618   0.00919  -0.1086   0.5425   1.0000
   5.500   1.1464   0.01631   0.00934  -0.1068   0.5360   1.0000
   5.750   1.1709   0.01639   0.00937  -0.1060   0.5309   1.0000
   6.000   1.1891   0.01660   0.00962  -0.1040   0.5250   1.0000
   6.250   1.2067   0.01675   0.00981  -0.1020   0.5184   1.0000
   6.500   1.2304   0.01681   0.00980  -0.1010   0.5126   1.0000
   6.750   1.2454   0.01701   0.01008  -0.0985   0.5057   1.0000
   7.000   1.2629   0.01710   0.01017  -0.0964   0.4983   1.0000
   7.250   1.2823   0.01721   0.01026  -0.0946   0.4912   1.0000
   7.500   1.2946   0.01736   0.01046  -0.0916   0.4825   1.0000
   7.750   1.3128   0.01746   0.01051  -0.0896   0.4744   1.0000
   8.000   1.3224   0.01765   0.01077  -0.0861   0.4651   1.0000
   8.250   1.3383   0.01783   0.01090  -0.0838   0.4566   1.0000
   8.500   1.3463   0.01807   0.01120  -0.0800   0.4468   1.0000
   8.750   1.3554   0.01831   0.01143  -0.0765   0.4373   1.0000
   9.000   1.3605   0.01857   0.01167  -0.0722   0.4267   1.0000
   9.250   1.3635   0.01891   0.01206  -0.0677   0.4150   1.0000
   9.500   1.3676   0.01932   0.01244  -0.0637   0.4020   1.0000
   9.750   1.3710   0.01982   0.01292  -0.0597   0.3879   1.0000
  10.000   1.3725   0.02047   0.01354  -0.0556   0.3723   1.0000
  10.250   1.3725   0.02127   0.01434  -0.0516   0.3544   1.0000
  10.500   1.3717   0.02226   0.01530  -0.0479   0.3345   1.0000
  10.750   1.3696   0.02347   0.01643  -0.0443   0.3144   1.0000
  11.000   1.3664   0.02491   0.01777  -0.0409   0.2961   1.0000
  11.250   1.3643   0.02646   0.01923  -0.0379   0.2814   1.0000
  11.500   1.3638   0.02806   0.02074  -0.0353   0.2693   1.0000
  11.750   1.3644   0.02967   0.02227  -0.0330   0.2593   1.0000
  12.000   1.3686   0.03115   0.02374  -0.0311   0.2500   1.0000
  12.250   1.3717   0.03272   0.02522  -0.0292   0.2423   1.0000
  12.500   1.3779   0.03416   0.02673  -0.0277   0.2346   1.0000
  12.750   1.3829   0.03568   0.02819  -0.0261   0.2276   1.0000
  13.000   1.3895   0.03715   0.02970  -0.0247   0.2210   1.0000
  13.250   1.3949   0.03872   0.03130  -0.0234   0.2144   1.0000
  13.500   1.4020   0.04018   0.03269  -0.0221   0.2082   1.0000
  13.750   1.4061   0.04196   0.03461  -0.0210   0.2019   1.0000
  14.000   1.4107   0.04368   0.03630  -0.0199   0.1956   1.0000
  14.250   1.4146   0.04555   0.03825  -0.0189   0.1893   1.0000
  14.500   1.4162   0.04769   0.04046  -0.0181   0.1825   1.0000
  14.750   1.4182   0.04979   0.04257  -0.0172   0.1760   1.0000
  15.000   1.4180   0.05226   0.04516  -0.0166   0.1686   1.0000
  15.250   1.4170   0.05479   0.04768  -0.0160   0.1616   1.0000
  15.500   1.4145   0.05766   0.05064  -0.0156   0.1533   1.0000
  15.750   1.4113   0.06061   0.05361  -0.0152   0.1452   1.0000
  16.000   1.4066   0.06376   0.05674  -0.0149   0.1373   1.0000
  16.250   1.4042   0.06675   0.05978  -0.0146   0.1296   1.0000
  16.500   1.4003   0.06981   0.06273  -0.0143   0.1232   1.0000
  16.750   1.3997   0.07270   0.06573  -0.0141   0.1171   1.0000
  17.000   1.3996   0.07534   0.06828  -0.0138   0.1126   1.0000
  17.250   1.4021   0.07779   0.07081  -0.0136   0.1087   1.0000
  17.500   1.4043   0.08031   0.07337  -0.0135   0.1051   1.0000
  17.750   1.4086   0.08243   0.07544  -0.0132   0.1021   1.0000
  18.000   1.4145   0.08438   0.07742  -0.0128   0.0995   1.0000
  18.250   1.4171   0.08693   0.08009  -0.0128   0.0968   1.0000
  18.500   1.4210   0.08926   0.08247  -0.0128   0.0945   1.0000
  18.750   1.4257   0.09140   0.08458  -0.0128   0.0921   1.0000
  19.000   1.4314   0.09335   0.08655  -0.0126   0.0898   1.0000
  19.250   1.4298   0.09662   0.08997  -0.0132   0.0876   1.0000
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