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NASA SC(2)-0612 AIRFOIL (sc20612-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NASA SC(2)-0612 AIRFOIL (sc20612-il)
Reynolds number: 500,000
Max Cl/Cd: 65.04 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sc20612-il-500000-n5.txt
Download as CSV file: xf-sc20612-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA SC(2)-0612 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
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -1.0317   0.10278   0.09919  -0.0339   1.0000   0.0178
 -18.000  -1.0651   0.09220   0.08842  -0.0400   1.0000   0.0178
 -17.750  -1.0900   0.08343   0.07948  -0.0451   1.0000   0.0178
 -17.500  -1.1089   0.07603   0.07191  -0.0494   1.0000   0.0178
 -17.250  -1.1231   0.06967   0.06541  -0.0532   1.0000   0.0179
 -17.000  -1.1339   0.06420   0.05979  -0.0562   1.0000   0.0180
 -16.750  -1.1417   0.05947   0.05492  -0.0587   1.0000   0.0181
 -16.500  -1.1470   0.05535   0.05067  -0.0607   1.0000   0.0182
 -16.250  -1.1505   0.05171   0.04690  -0.0623   1.0000   0.0184
 -16.000  -1.1522   0.04850   0.04358  -0.0634   1.0000   0.0185
 -15.750  -1.1527   0.04564   0.04060  -0.0642   1.0000   0.0187
 -15.500  -1.1514   0.04306   0.03791  -0.0647   1.0000   0.0189
 -15.250  -1.1488   0.04074   0.03548  -0.0650   1.0000   0.0190
 -15.000  -1.1448   0.03863   0.03326  -0.0651   1.0000   0.0192
 -14.750  -1.1393   0.03674   0.03127  -0.0650   1.0000   0.0194
 -14.500  -1.1326   0.03505   0.02947  -0.0647   1.0000   0.0196
 -14.250  -1.1261   0.03342   0.02775  -0.0642   1.0000   0.0199
 -14.000  -1.1222   0.03170   0.02598  -0.0635   1.0000   0.0202
 -13.750  -1.1170   0.03026   0.02449  -0.0625   1.0000   0.0204
 -13.500  -1.1119   0.02903   0.02321  -0.0610   1.0000   0.0207
 -13.250  -1.1087   0.02796   0.02209  -0.0588   1.0000   0.0210
 -13.000  -1.1094   0.02700   0.02109  -0.0558   1.0000   0.0212
 -12.750  -1.1055   0.02604   0.02008  -0.0535   1.0000   0.0215
 -12.500  -1.0971   0.02511   0.01909  -0.0519   1.0000   0.0218
 -12.250  -1.0860   0.02421   0.01814  -0.0507   1.0000   0.0221
 -12.000  -1.0724   0.02335   0.01721  -0.0498   1.0000   0.0225
 -11.750  -1.0544   0.02251   0.01630  -0.0497   0.9998   0.0230
 -11.500  -1.0252   0.02166   0.01537  -0.0515   0.9985   0.0234
 -11.250  -0.9963   0.02071   0.01437  -0.0534   0.9972   0.0241
 -11.000  -0.9662   0.01992   0.01355  -0.0553   0.9958   0.0248
 -10.750  -0.9353   0.01923   0.01283  -0.0571   0.9947   0.0256
 -10.500  -0.9039   0.01861   0.01216  -0.0589   0.9937   0.0265
 -10.250  -0.8736   0.01804   0.01153  -0.0604   0.9922   0.0275
 -10.000  -0.8434   0.01741   0.01088  -0.0618   0.9905   0.0286
  -9.750  -0.8124   0.01689   0.01035  -0.0633   0.9888   0.0299
  -9.500  -0.7807   0.01640   0.00983  -0.0648   0.9873   0.0313
  -9.250  -0.7485   0.01591   0.00931  -0.0665   0.9860   0.0327
  -9.000  -0.7160   0.01545   0.00887  -0.0681   0.9849   0.0345
  -8.750  -0.6832   0.01506   0.00846  -0.0698   0.9839   0.0367
  -8.500  -0.6500   0.01466   0.00805  -0.0715   0.9831   0.0390
  -8.250  -0.6165   0.01431   0.00771  -0.0732   0.9824   0.0418
  -8.000  -0.5864   0.01399   0.00737  -0.0741   0.9801   0.0441
  -7.750  -0.5550   0.01362   0.00701  -0.0754   0.9780   0.0467
  -7.500  -0.5224   0.01332   0.00670  -0.0768   0.9762   0.0495
  -7.250  -0.4891   0.01299   0.00637  -0.0783   0.9748   0.0523
  -7.000  -0.4553   0.01266   0.00606  -0.0800   0.9737   0.0554
  -6.750  -0.4209   0.01238   0.00577  -0.0817   0.9726   0.0581
  -6.500  -0.3858   0.01205   0.00547  -0.0837   0.9716   0.0615
  -6.250  -0.3508   0.01176   0.00519  -0.0855   0.9705   0.0655
  -6.000  -0.3158   0.01149   0.00493  -0.0873   0.9696   0.0692
  -5.750  -0.2856   0.01123   0.00471  -0.0881   0.9663   0.0746
  -5.500  -0.2533   0.01097   0.00449  -0.0893   0.9640   0.0819
  -5.250  -0.2199   0.01071   0.00427  -0.0908   0.9619   0.0915
  -5.000  -0.1858   0.01042   0.00406  -0.0924   0.9601   0.1039
  -4.750  -0.1513   0.01012   0.00384  -0.0941   0.9586   0.1215
  -4.500  -0.1163   0.00979   0.00364  -0.0960   0.9572   0.1475
  -4.250  -0.0805   0.00941   0.00342  -0.0981   0.9560   0.1851
  -4.000  -0.0463   0.00896   0.00322  -0.1001   0.9531   0.2443
  -3.750  -0.0106   0.00845   0.00301  -0.1024   0.9503   0.3179
  -3.500   0.0265   0.00793   0.00278  -0.1050   0.9479   0.3948
  -3.250   0.0646   0.00739   0.00264  -0.1078   0.9460   0.4968
  -3.000   0.0987   0.00722   0.00265  -0.1092   0.9433   0.5509
  -2.750   0.1309   0.00717   0.00267  -0.1100   0.9397   0.5787
  -2.500   0.1605   0.00715   0.00268  -0.1101   0.9326   0.5974
  -2.250   0.1918   0.00712   0.00268  -0.1106   0.9269   0.6119
  -2.000   0.2209   0.00713   0.00270  -0.1105   0.9173   0.6246
  -1.750   0.2499   0.00714   0.00268  -0.1103   0.9020   0.6369
  -1.500   0.2779   0.00717   0.00270  -0.1099   0.8831   0.6446
  -1.250   0.3064   0.00721   0.00266  -0.1096   0.8605   0.6506
  -1.000   0.3345   0.00730   0.00260  -0.1092   0.8267   0.6550
  -0.750   0.3616   0.00743   0.00261  -0.1087   0.7877   0.6579
  -0.500   0.3879   0.00768   0.00262  -0.1080   0.7331   0.6606
  -0.250   0.4132   0.00807   0.00268  -0.1072   0.6556   0.6633
   0.000   0.4361   0.00879   0.00286  -0.1062   0.5356   0.6658
   0.250   0.4600   0.00953   0.00308  -0.1056   0.4197   0.6682
   0.500   0.4857   0.01012   0.00328  -0.1053   0.3305   0.6707
   0.750   0.5118   0.01060   0.00347  -0.1051   0.2606   0.6727
   1.000   0.5382   0.01101   0.00366  -0.1048   0.2090   0.6746
   1.250   0.5652   0.01137   0.00385  -0.1046   0.1673   0.6766
   1.500   0.5923   0.01171   0.00405  -0.1045   0.1356   0.6787
   1.750   0.6199   0.01198   0.00423  -0.1044   0.1163   0.6807
   2.000   0.6477   0.01223   0.00441  -0.1044   0.1016   0.6826
   2.250   0.6754   0.01250   0.00460  -0.1043   0.0889   0.6845
   2.500   0.7032   0.01275   0.00479  -0.1043   0.0798   0.6864
   2.750   0.7309   0.01302   0.00499  -0.1042   0.0727   0.6882
   3.000   0.7587   0.01323   0.00520  -0.1041   0.0684   0.6899
   3.250   0.7859   0.01347   0.00543  -0.1039   0.0642   0.6915
   3.500   0.8131   0.01372   0.00569  -0.1037   0.0612   0.6933
   3.750   0.8403   0.01396   0.00595  -0.1035   0.0583   0.6954
   4.000   0.8671   0.01425   0.00622  -0.1032   0.0552   0.6977
   4.250   0.8941   0.01453   0.00650  -0.1030   0.0527   0.6999
   4.500   0.9211   0.01479   0.00678  -0.1027   0.0503   0.7020
   4.750   0.9479   0.01509   0.00707  -0.1025   0.0477   0.7040
   5.000   0.9745   0.01540   0.00738  -0.1022   0.0453   0.7059
   5.500   1.0273   0.01600   0.00799  -0.1016   0.0403   0.7095
   5.750   1.0532   0.01631   0.00835  -0.1011   0.0382   0.7115
   6.000   1.0790   0.01664   0.00870  -0.1007   0.0361   0.7135
   6.250   1.1044   0.01702   0.00908  -0.1002   0.0342   0.7155
   6.500   1.1299   0.01738   0.00948  -0.0997   0.0325   0.7175
   6.750   1.1551   0.01776   0.00988  -0.0991   0.0309   0.7196
   7.000   1.1798   0.01820   0.01032  -0.0986   0.0295   0.7218
   7.250   1.2045   0.01865   0.01081  -0.0979   0.0285   0.7239
   7.500   1.2289   0.01910   0.01130  -0.0973   0.0276   0.7259
   7.750   1.2529   0.01956   0.01180  -0.0966   0.0266   0.7277
   8.000   1.2762   0.02006   0.01235  -0.0957   0.0258   0.7296
   8.250   1.2985   0.02067   0.01299  -0.0948   0.0250   0.7317
   8.500   1.3212   0.02121   0.01361  -0.0938   0.0245   0.7340
   8.750   1.3436   0.02176   0.01424  -0.0929   0.0239   0.7364
   9.000   1.3657   0.02233   0.01487  -0.0919   0.0232   0.7388
   9.250   1.3874   0.02292   0.01551  -0.0908   0.0226   0.7412
   9.500   1.4084   0.02354   0.01618  -0.0897   0.0221   0.7435
   9.750   1.4282   0.02425   0.01694  -0.0884   0.0216   0.7458
  10.000   1.4459   0.02510   0.01786  -0.0868   0.0211   0.7479
  10.250   1.4645   0.02582   0.01868  -0.0853   0.0208   0.7502
  10.500   1.4824   0.02657   0.01953  -0.0837   0.0205   0.7525
  10.750   1.4992   0.02736   0.02043  -0.0819   0.0202   0.7549
  11.000   1.5146   0.02818   0.02135  -0.0800   0.0198   0.7574
  11.250   1.5285   0.02904   0.02230  -0.0778   0.0195   0.7599
  11.500   1.5389   0.02992   0.02327  -0.0751   0.0193   0.7624
  11.750   1.5486   0.03085   0.02431  -0.0723   0.0190   0.7645
  12.000   1.5585   0.03187   0.02544  -0.0697   0.0188   0.7668
  12.250   1.5679   0.03296   0.02664  -0.0673   0.0185   0.7692
  12.500   1.5760   0.03417   0.02794  -0.0648   0.0183   0.7718
  12.750   1.5827   0.03551   0.02938  -0.0623   0.0181   0.7745
  13.000   1.5876   0.03703   0.03100  -0.0598   0.0180   0.7771
  13.250   1.5904   0.03878   0.03285  -0.0573   0.0178   0.7796
  13.500   1.5900   0.04084   0.03504  -0.0547   0.0176   0.7818
  13.750   1.5917   0.04282   0.03717  -0.0526   0.0175   0.7840
  14.000   1.5929   0.04493   0.03945  -0.0508   0.0174   0.7864
  14.250   1.5927   0.04727   0.04195  -0.0491   0.0172   0.7891
  14.500   1.5909   0.04991   0.04475  -0.0478   0.0171   0.7918
  14.750   1.5870   0.05291   0.04791  -0.0468   0.0170   0.7945
  15.000   1.5810   0.05633   0.05150  -0.0462   0.0168   0.7970
  15.250   1.5732   0.06021   0.05556  -0.0462   0.0167   0.7991
  15.500   1.5626   0.06474   0.06027  -0.0469   0.0166   0.8013
  15.750   1.5488   0.07013   0.06586  -0.0484   0.0165   0.8035
  16.000   1.5317   0.07663   0.07256  -0.0512   0.0165   0.8056
  16.250   1.5099   0.08467   0.08081  -0.0555   0.0164   0.8076
  16.500   1.4817   0.09461   0.09097  -0.0614   0.0164   0.8090
  16.750   1.4446   0.10699   0.10360  -0.0691   0.0165   0.8099
  17.000   1.3970   0.12190   0.11876  -0.0783   0.0165   0.8100
  17.250   1.3325   0.14118   0.13831  -0.0906   0.0167   0.8091
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