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NASA SC(2)-0710 AIRFOIL (sc20710-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NASA SC(2)-0710 AIRFOIL (sc20710-il)
Reynolds number: 500,000
Max Cl/Cd: 63.65 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sc20710-il-500000-n5.txt
Download as CSV file: xf-sc20710-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA SC(2)-0710 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
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.9609   0.07610   0.07282  -0.0491   1.0000   0.0135
 -15.750  -0.9967   0.06457   0.06102  -0.0570   1.0000   0.0134
 -15.500  -1.0174   0.05729   0.05355  -0.0618   1.0000   0.0134
 -15.250  -1.0317   0.05192   0.04802  -0.0648   1.0000   0.0134
 -15.000  -1.0415   0.04773   0.04367  -0.0666   1.0000   0.0135
 -14.750  -1.0490   0.04423   0.04004  -0.0675   1.0000   0.0135
 -14.500  -1.0546   0.04131   0.03699  -0.0677   1.0000   0.0136
 -14.250  -1.0591   0.03880   0.03435  -0.0673   1.0000   0.0137
 -14.000  -1.0631   0.03662   0.03207  -0.0662   1.0000   0.0138
 -13.750  -1.0677   0.03477   0.03012  -0.0644   1.0000   0.0139
 -13.500  -1.0758   0.03323   0.02848  -0.0614   1.0000   0.0140
 -13.250  -1.0800   0.03175   0.02691  -0.0588   1.0000   0.0141
 -13.000  -1.0761   0.03023   0.02528  -0.0576   1.0000   0.0142
 -12.750  -1.0678   0.02879   0.02372  -0.0569   1.0000   0.0144
 -12.500  -1.0558   0.02742   0.02222  -0.0565   1.0000   0.0146
 -12.250  -1.0385   0.02610   0.02077  -0.0569   0.9997   0.0148
 -12.000  -1.0115   0.02477   0.01928  -0.0589   0.9987   0.0151
 -11.750  -0.9840   0.02358   0.01795  -0.0607   0.9975   0.0153
 -11.500  -0.9560   0.02251   0.01674  -0.0623   0.9965   0.0156
 -11.250  -0.9273   0.02157   0.01568  -0.0639   0.9955   0.0159
 -11.000  -0.8983   0.02048   0.01451  -0.0657   0.9947   0.0164
 -10.750  -0.8681   0.01970   0.01367  -0.0674   0.9940   0.0169
 -10.500  -0.8395   0.01900   0.01293  -0.0686   0.9928   0.0174
 -10.250  -0.8103   0.01832   0.01217  -0.0698   0.9916   0.0179
 -10.000  -0.7805   0.01766   0.01145  -0.0711   0.9905   0.0184
  -9.750  -0.7502   0.01704   0.01075  -0.0725   0.9894   0.0190
  -9.500  -0.7193   0.01646   0.01010  -0.0739   0.9884   0.0196
  -9.250  -0.6880   0.01583   0.00943  -0.0754   0.9875   0.0204
  -9.000  -0.6564   0.01535   0.00894  -0.0769   0.9866   0.0214
  -8.750  -0.6243   0.01491   0.00846  -0.0784   0.9858   0.0226
  -8.500  -0.5917   0.01449   0.00799  -0.0799   0.9851   0.0239
  -8.250  -0.5588   0.01404   0.00754  -0.0816   0.9845   0.0257
  -8.000  -0.5259   0.01370   0.00719  -0.0831   0.9839   0.0277
  -7.750  -0.4941   0.01338   0.00682  -0.0844   0.9830   0.0296
  -7.500  -0.4644   0.01298   0.00644  -0.0853   0.9812   0.0319
  -7.250  -0.4333   0.01269   0.00613  -0.0864   0.9796   0.0341
  -7.000  -0.4014   0.01240   0.00581  -0.0876   0.9783   0.0361
  -6.750  -0.3689   0.01207   0.00551  -0.0890   0.9772   0.0390
  -6.500  -0.3364   0.01183   0.00527  -0.0903   0.9762   0.0421
  -6.250  -0.3035   0.01155   0.00500  -0.0918   0.9754   0.0459
  -6.000  -0.2704   0.01131   0.00479  -0.0932   0.9746   0.0509
  -5.750  -0.2368   0.01105   0.00456  -0.0948   0.9739   0.0569
  -5.500  -0.2033   0.01083   0.00435  -0.0963   0.9733   0.0632
  -5.250  -0.1693   0.01058   0.00415  -0.0979   0.9728   0.0733
  -5.000  -0.1351   0.01033   0.00397  -0.0996   0.9723   0.0859
  -4.750  -0.1008   0.01010   0.00381  -0.1013   0.9718   0.1037
  -4.250  -0.0356   0.00948   0.00352  -0.1042   0.9689   0.1786
  -4.000  -0.0006   0.00908   0.00336  -0.1063   0.9677   0.2423
  -3.500   0.0779   0.00790   0.00302  -0.1128   0.9674   0.4656
  -3.250   0.1136   0.00761   0.00308  -0.1149   0.9668   0.5641
  -3.000   0.1456   0.00758   0.00312  -0.1158   0.9654   0.5899
  -2.750   0.1782   0.00756   0.00316  -0.1167   0.9640   0.6135
  -2.500   0.2127   0.00751   0.00316  -0.1180   0.9623   0.6333
  -2.250   0.2487   0.00741   0.00309  -0.1196   0.9601   0.6475
  -2.000   0.2818   0.00728   0.00299  -0.1204   0.9542   0.6529
  -1.750   0.3188   0.00703   0.00272  -0.1219   0.9442   0.6591
  -1.500   0.3506   0.00690   0.00261  -0.1223   0.9304   0.6659
  -1.250   0.3811   0.00684   0.00253  -0.1224   0.9102   0.6721
  -1.000   0.4118   0.00682   0.00243  -0.1226   0.8835   0.6787
  -0.750   0.4392   0.00692   0.00242  -0.1219   0.8389   0.6835
  -0.500   0.4576   0.00775   0.00246  -0.1193   0.6613   0.6871
  -0.250   0.4758   0.00891   0.00278  -0.1174   0.4739   0.6899
   0.000   0.4991   0.00971   0.00302  -0.1167   0.3445   0.6925
   0.250   0.5245   0.01027   0.00321  -0.1164   0.2560   0.6946
   0.500   0.5502   0.01074   0.00342  -0.1160   0.1906   0.6964
   0.750   0.5765   0.01114   0.00362  -0.1157   0.1426   0.6985
   1.000   0.6033   0.01149   0.00382  -0.1155   0.1087   0.7007
   1.250   0.6306   0.01177   0.00402  -0.1154   0.0889   0.7030
   1.500   0.6581   0.01203   0.00421  -0.1153   0.0753   0.7055
   1.750   0.6857   0.01229   0.00441  -0.1152   0.0660   0.7082
   2.000   0.7131   0.01257   0.00464  -0.1150   0.0579   0.7106
   2.250   0.7402   0.01279   0.00487  -0.1148   0.0525   0.7124
   2.500   0.7671   0.01307   0.00512  -0.1145   0.0472   0.7142
   2.750   0.7943   0.01331   0.00537  -0.1143   0.0436   0.7161
   3.000   0.8211   0.01361   0.00565  -0.1141   0.0402   0.7182
   3.250   0.8482   0.01387   0.00593  -0.1138   0.0377   0.7204
   3.500   0.8751   0.01415   0.00621  -0.1136   0.0351   0.7226
   3.750   0.9016   0.01452   0.00655  -0.1133   0.0326   0.7249
   4.000   0.9285   0.01480   0.00687  -0.1130   0.0309   0.7268
   4.250   0.9547   0.01511   0.00721  -0.1126   0.0289   0.7286
   4.500   0.9804   0.01549   0.00760  -0.1122   0.0271   0.7307
   4.750   1.0063   0.01586   0.00802  -0.1117   0.0256   0.7331
   5.000   1.0322   0.01623   0.00843  -0.1112   0.0241   0.7356
   5.250   1.0579   0.01662   0.00883  -0.1108   0.0227   0.7379
   5.500   1.0832   0.01709   0.00932  -0.1103   0.0215   0.7402
   5.750   1.1088   0.01751   0.00978  -0.1098   0.0205   0.7424
   6.000   1.1338   0.01794   0.01027  -0.1092   0.0196   0.7441
   6.250   1.1584   0.01841   0.01078  -0.1085   0.0188   0.7458
   6.500   1.1825   0.01894   0.01136  -0.1078   0.0182   0.7477
   6.750   1.2059   0.01960   0.01206  -0.1070   0.0176   0.7497
   7.000   1.2297   0.02018   0.01274  -0.1062   0.0172   0.7519
   7.250   1.2531   0.02081   0.01345  -0.1053   0.0168   0.7542
   7.500   1.2762   0.02147   0.01420  -0.1044   0.0164   0.7564
   7.750   1.2990   0.02216   0.01497  -0.1035   0.0161   0.7586
   8.000   1.3212   0.02285   0.01575  -0.1025   0.0157   0.7603
   8.250   1.3428   0.02357   0.01657  -0.1014   0.0154   0.7623
   8.500   1.3641   0.02433   0.01742  -0.1003   0.0151   0.7645
   8.750   1.3847   0.02513   0.01831  -0.0991   0.0149   0.7668
   9.000   1.4044   0.02602   0.01929  -0.0977   0.0146   0.7692
   9.250   1.4216   0.02724   0.02060  -0.0961   0.0142   0.7715
   9.500   1.4404   0.02819   0.02170  -0.0946   0.0140   0.7738
   9.750   1.4579   0.02921   0.02289  -0.0930   0.0138   0.7757
  10.000   1.4740   0.03034   0.02419  -0.0911   0.0137   0.7777
  10.250   1.4886   0.03156   0.02559  -0.0891   0.0135   0.7798
  10.500   1.5017   0.03288   0.02708  -0.0868   0.0133   0.7820
  10.750   1.5130   0.03426   0.02865  -0.0844   0.0131   0.7843
  11.000   1.5219   0.03573   0.03030  -0.0817   0.0130   0.7868
  11.250   1.5274   0.03727   0.03201  -0.0785   0.0128   0.7892
  11.500   1.5271   0.03880   0.03373  -0.0744   0.0127   0.7912
  11.750   1.5267   0.04057   0.03569  -0.0707   0.0126   0.7932
  12.000   1.5254   0.04249   0.03780  -0.0672   0.0125   0.7952
  12.250   1.5214   0.04473   0.04022  -0.0638   0.0124   0.7973
  12.500   1.5158   0.04719   0.04288  -0.0607   0.0123   0.7994
  12.750   1.5081   0.05000   0.04587  -0.0580   0.0123   0.8015
  13.000   1.4975   0.05332   0.04938  -0.0558   0.0122   0.8037
  13.250   1.4835   0.05731   0.05358  -0.0544   0.0122   0.8056
  13.500   1.4647   0.06234   0.05885  -0.0541   0.0121   0.8071
  13.750   1.4420   0.06876   0.06550  -0.0557   0.0121   0.8087
  14.000   1.4094   0.07855   0.07558  -0.0612   0.0121   0.8099
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