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NASA SC(2)-0612 AIRFOIL (sc20612-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NASA SC(2)-0612 AIRFOIL (sc20612-il)
Reynolds number: 1,000,000
Max Cl/Cd: 77.94 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-sc20612-il-1000000.txt
Download as CSV file: xf-sc20612-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.000  -1.0935   0.10266   0.09984  -0.0343   1.0000   0.0178
 -18.750  -1.1235   0.09302   0.09005  -0.0398   1.0000   0.0178
 -18.500  -1.1475   0.08463   0.08151  -0.0446   1.0000   0.0178
 -18.250  -1.1660   0.07748   0.07422  -0.0488   1.0000   0.0179
 -18.000  -1.1808   0.07110   0.06770  -0.0525   1.0000   0.0179
 -17.750  -1.1921   0.06555   0.06203  -0.0556   1.0000   0.0180
 -17.500  -1.2008   0.06065   0.05701  -0.0582   1.0000   0.0181
 -17.250  -1.2070   0.05633   0.05257  -0.0603   1.0000   0.0182
 -17.000  -1.2112   0.05251   0.04864  -0.0620   1.0000   0.0183
 -16.750  -1.2136   0.04908   0.04511  -0.0634   1.0000   0.0184
 -16.500  -1.2146   0.04603   0.04195  -0.0644   1.0000   0.0185
 -16.250  -1.2142   0.04331   0.03914  -0.0651   1.0000   0.0187
 -16.000  -1.2123   0.04084   0.03658  -0.0656   1.0000   0.0188
 -15.750  -1.2090   0.03862   0.03425  -0.0658   1.0000   0.0190
 -15.500  -1.2042   0.03659   0.03213  -0.0659   1.0000   0.0192
 -15.250  -1.1982   0.03476   0.03021  -0.0659   1.0000   0.0193
 -15.000  -1.1909   0.03311   0.02848  -0.0657   1.0000   0.0195
 -14.750  -1.1825   0.03164   0.02693  -0.0653   1.0000   0.0196
 -14.500  -1.1733   0.03031   0.02553  -0.0648   1.0000   0.0197
 -14.250  -1.1691   0.02870   0.02384  -0.0637   1.0000   0.0199
 -14.000  -1.1716   0.02691   0.02196  -0.0617   1.0000   0.0202
 -13.750  -1.1742   0.02561   0.02062  -0.0589   1.0000   0.0205
 -13.500  -1.1808   0.02460   0.01958  -0.0549   1.0000   0.0206
 -13.250  -1.1762   0.02360   0.01854  -0.0528   1.0000   0.0209
 -13.000  -1.1673   0.02269   0.01759  -0.0513   1.0000   0.0212
 -12.750  -1.1547   0.02185   0.01671  -0.0503   1.0000   0.0215
 -12.500  -1.1392   0.02105   0.01587  -0.0497   1.0000   0.0218
 -12.250  -1.1213   0.02030   0.01506  -0.0494   1.0000   0.0222
 -12.000  -1.1014   0.01961   0.01432  -0.0493   1.0000   0.0226
 -11.750  -1.0727   0.01898   0.01364  -0.0507   0.9994   0.0231
 -11.500  -1.0406   0.01843   0.01303  -0.0526   0.9986   0.0235
 -11.250  -1.0096   0.01727   0.01183  -0.0550   0.9976   0.0244
 -11.000  -0.9777   0.01661   0.01115  -0.0569   0.9968   0.0252
 -10.750  -0.9453   0.01608   0.01059  -0.0587   0.9959   0.0260
 -10.500  -0.9123   0.01559   0.01007  -0.0606   0.9952   0.0268
 -10.250  -0.8790   0.01516   0.00961  -0.0624   0.9945   0.0275
 -10.000  -0.8455   0.01450   0.00892  -0.0645   0.9940   0.0288
  -9.750  -0.8117   0.01404   0.00847  -0.0664   0.9935   0.0301
  -9.500  -0.7802   0.01367   0.00808  -0.0678   0.9923   0.0314
  -9.250  -0.7481   0.01332   0.00771  -0.0691   0.9909   0.0326
  -9.000  -0.7149   0.01285   0.00727  -0.0709   0.9897   0.0349
  -8.750  -0.6814   0.01256   0.00698  -0.0725   0.9885   0.0370
  -8.500  -0.6471   0.01217   0.00661  -0.0743   0.9875   0.0397
  -8.250  -0.6129   0.01191   0.00636  -0.0760   0.9865   0.0425
  -8.000  -0.5782   0.01159   0.00605  -0.0779   0.9857   0.0455
  -7.750  -0.5434   0.01132   0.00580  -0.0797   0.9850   0.0487
  -7.500  -0.5087   0.01115   0.00563  -0.0814   0.9843   0.0509
  -7.250  -0.4729   0.01076   0.00528  -0.0836   0.9838   0.0550
  -7.000  -0.4375   0.01053   0.00505  -0.0854   0.9833   0.0577
  -6.750  -0.4019   0.01028   0.00480  -0.0874   0.9828   0.0606
  -6.500  -0.3660   0.00999   0.00455  -0.0895   0.9824   0.0646
  -6.250  -0.3343   0.00980   0.00436  -0.0904   0.9803   0.0673
  -6.000  -0.3009   0.00954   0.00413  -0.0919   0.9785   0.0715
  -5.750  -0.2662   0.00929   0.00392  -0.0936   0.9773   0.0769
  -5.500  -0.2311   0.00903   0.00371  -0.0954   0.9762   0.0848
  -5.250  -0.1960   0.00877   0.00351  -0.0972   0.9750   0.0967
  -5.000  -0.1604   0.00845   0.00330  -0.0991   0.9739   0.1190
  -4.750  -0.1235   0.00802   0.00308  -0.1015   0.9730   0.1605
  -4.500  -0.0859   0.00752   0.00284  -0.1042   0.9720   0.2222
  -4.250  -0.0474   0.00695   0.00260  -0.1071   0.9710   0.3044
  -4.000  -0.0085   0.00636   0.00235  -0.1102   0.9700   0.3993
  -3.750   0.0286   0.00575   0.00215  -0.1127   0.9670   0.5166
  -3.500   0.0606   0.00557   0.00211  -0.1136   0.9621   0.5635
  -3.250   0.0918   0.00550   0.00207  -0.1141   0.9580   0.5845
  -3.000   0.1219   0.00547   0.00205  -0.1144   0.9532   0.5968
  -2.750   0.1503   0.00544   0.00200  -0.1142   0.9454   0.6063
  -2.500   0.1784   0.00540   0.00197  -0.1139   0.9353   0.6144
  -2.250   0.2068   0.00540   0.00192  -0.1136   0.9249   0.6231
  -2.000   0.2352   0.00541   0.00194  -0.1134   0.9136   0.6311
  -1.750   0.2637   0.00545   0.00192  -0.1132   0.8994   0.6381
  -1.500   0.2921   0.00547   0.00194  -0.1130   0.8847   0.6442
  -1.250   0.3208   0.00556   0.00200  -0.1129   0.8705   0.6516
  -1.000   0.3493   0.00564   0.00203  -0.1127   0.8527   0.6579
  -0.750   0.3776   0.00574   0.00208  -0.1125   0.8338   0.6620
  -0.500   0.4061   0.00584   0.00211  -0.1124   0.8104   0.6651
  -0.250   0.4341   0.00599   0.00215  -0.1121   0.7786   0.6683
   0.000   0.4615   0.00624   0.00220  -0.1118   0.7328   0.6708
   0.250   0.4864   0.00670   0.00228  -0.1111   0.6376   0.6736
   0.500   0.5090   0.00756   0.00253  -0.1101   0.4886   0.6759
   0.750   0.5334   0.00830   0.00277  -0.1096   0.3693   0.6779
   1.000   0.5588   0.00890   0.00298  -0.1092   0.2760   0.6798
   1.250   0.5852   0.00938   0.00318  -0.1090   0.2094   0.6817
   1.500   0.6119   0.00981   0.00337  -0.1088   0.1573   0.6838
   1.750   0.6392   0.01017   0.00355  -0.1087   0.1221   0.6859
   2.000   0.6669   0.01047   0.00373  -0.1086   0.0991   0.6878
   2.250   0.6947   0.01075   0.00391  -0.1085   0.0846   0.6893
   2.500   0.7228   0.01090   0.00405  -0.1085   0.0782   0.6919
   2.750   0.7505   0.01114   0.00425  -0.1084   0.0720   0.6939
   3.000   0.7786   0.01130   0.00443  -0.1083   0.0687   0.6957
   3.250   0.8063   0.01154   0.00463  -0.1082   0.0646   0.6975
   3.500   0.8339   0.01177   0.00485  -0.1080   0.0616   0.6993
   3.750   0.8618   0.01195   0.00504  -0.1079   0.0593   0.7012
   4.000   0.8893   0.01219   0.00526  -0.1078   0.0563   0.7030
   4.250   0.9165   0.01246   0.00552  -0.1076   0.0532   0.7048
   4.500   0.9443   0.01265   0.00571  -0.1074   0.0510   0.7064
   4.750   0.9714   0.01291   0.00594  -0.1072   0.0482   0.7081
   5.000   0.9984   0.01316   0.00620  -0.1070   0.0454   0.7107
   5.250   1.0257   0.01334   0.00640  -0.1068   0.0428   0.7129
   5.500   1.0519   0.01368   0.00672  -0.1064   0.0397   0.7150
   5.750   1.0789   0.01389   0.00695  -0.1061   0.0377   0.7171
   6.000   1.1052   0.01420   0.00724  -0.1058   0.0354   0.7192
   6.250   1.1312   0.01456   0.00761  -0.1053   0.0336   0.7212
   6.500   1.1574   0.01485   0.00791  -0.1049   0.0321   0.7233
   6.750   1.1832   0.01521   0.00826  -0.1045   0.0307   0.7252
   7.000   1.2078   0.01571   0.00877  -0.1038   0.0292   0.7270
   7.250   1.2335   0.01601   0.00912  -0.1033   0.0284   0.7296
   7.500   1.2588   0.01635   0.00950  -0.1028   0.0275   0.7318
   7.750   1.2836   0.01674   0.00991  -0.1022   0.0265   0.7339
   8.000   1.3072   0.01727   0.01046  -0.1013   0.0255   0.7360
   8.250   1.3300   0.01789   0.01113  -0.1004   0.0248   0.7381
   8.500   1.3542   0.01830   0.01159  -0.0996   0.0243   0.7403
   8.750   1.3779   0.01876   0.01209  -0.0988   0.0238   0.7424
   9.000   1.4012   0.01925   0.01262  -0.0980   0.0232   0.7442
   9.250   1.4240   0.01974   0.01315  -0.0971   0.0227   0.7464
   9.500   1.4461   0.02028   0.01374  -0.0961   0.0223   0.7489
   9.750   1.4664   0.02098   0.01449  -0.0947   0.0217   0.7512
  10.000   1.4825   0.02211   0.01570  -0.0928   0.0211   0.7536
  10.250   1.5028   0.02274   0.01640  -0.0915   0.0209   0.7561
  10.500   1.5231   0.02332   0.01706  -0.0902   0.0207   0.7585
  10.750   1.5425   0.02397   0.01778  -0.0887   0.0204   0.7609
  11.000   1.5608   0.02467   0.01855  -0.0871   0.0201   0.7629
  11.250   1.5780   0.02538   0.01935  -0.0854   0.0198   0.7656
  11.500   1.5939   0.02611   0.02016  -0.0834   0.0195   0.7681
  11.750   1.6088   0.02681   0.02094  -0.0813   0.0192   0.7705
  12.000   1.6217   0.02756   0.02175  -0.0789   0.0189   0.7730
  12.250   1.6300   0.02837   0.02263  -0.0758   0.0187   0.7756
  12.500   1.6393   0.02933   0.02365  -0.0729   0.0185   0.7781
  12.750   1.6471   0.03044   0.02483  -0.0701   0.0183   0.7802
  13.000   1.6524   0.03177   0.02626  -0.0671   0.0181   0.7831
  13.250   1.6538   0.03345   0.02806  -0.0638   0.0179   0.7857
  13.500   1.6480   0.03581   0.03059  -0.0601   0.0176   0.7881
  13.750   1.6483   0.03775   0.03266  -0.0573   0.0175   0.7907
  14.000   1.6528   0.03934   0.03437  -0.0551   0.0174   0.7934
  14.250   1.6564   0.04109   0.03623  -0.0530   0.0174   0.7959
  14.500   1.6581   0.04309   0.03835  -0.0511   0.0173   0.7984
  14.750   1.6577   0.04535   0.04076  -0.0494   0.0172   0.8011
  15.000   1.6559   0.04789   0.04344  -0.0479   0.0171   0.8038
  15.250   1.6524   0.05076   0.04644  -0.0467   0.0170   0.8064
  15.500   1.6464   0.05406   0.04988  -0.0459   0.0169   0.8090
  15.750   1.6388   0.05779   0.05375  -0.0457   0.0168   0.8115
  16.000   1.6287   0.06213   0.05823  -0.0460   0.0167   0.8136
  16.250   1.6154   0.06723   0.06350  -0.0472   0.0167   0.8161
  16.500   1.5994   0.07326   0.06971  -0.0494   0.0166   0.8183
  16.750   1.5797   0.08050   0.07713  -0.0528   0.0166   0.8203
  17.000   1.5561   0.08898   0.08580  -0.0575   0.0166   0.8221
  17.250   1.5257   0.09934   0.09636  -0.0636   0.0166   0.8234
  17.500   1.4878   0.11156   0.10880  -0.0711   0.0166   0.8242
  17.750   1.4409   0.12597   0.12342  -0.0801   0.0167   0.8244
  18.000   1.3801   0.14414   0.14184  -0.0920   0.0168   0.8237
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