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NASA LRN 1015 (NASA TM 102840) (lrn1015-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NASA LRN 1015 (NASA TM 102840) (lrn1015-il)
Reynolds number: 1,000,000
Max Cl/Cd: 154.83 at α=5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-lrn1015-il-1000000.txt
Download as CSV file: xf-lrn1015-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA LRN 1015 (NASA TM 102840)                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.1002   0.09492   0.09189  -0.1057   0.7488   0.0127
 -11.500  -0.0944   0.09198   0.08893  -0.1071   0.7472   0.0128
 -11.250  -0.0884   0.08910   0.08605  -0.1085   0.7456   0.0128
 -11.000  -0.0825   0.08646   0.08343  -0.1095   0.7447   0.0130
 -10.750  -0.0792   0.08324   0.08024  -0.1109   0.7436   0.0131
 -10.500  -0.0754   0.08022   0.07724  -0.1123   0.7422   0.0132
 -10.250  -0.0730   0.07695   0.07399  -0.1138   0.7409   0.0134
 -10.000  -0.0708   0.07369   0.07074  -0.1154   0.7395   0.0137
  -9.750  -0.0726   0.06968   0.06675  -0.1175   0.7381   0.0138
  -9.500  -0.0776   0.06509   0.06219  -0.1201   0.7366   0.0140
  -9.250  -0.0987   0.05725   0.05438  -0.1268   0.7348   0.0139
  -9.000  -0.1222   0.05220   0.04927  -0.1290   0.7328   0.0139
  -8.750  -0.1430   0.04930   0.04629  -0.1270   0.7304   0.0141
  -8.500  -0.1558   0.04573   0.04263  -0.1255   0.7288   0.0140
  -8.250  -0.1616   0.04215   0.03892  -0.1239   0.7274   0.0147
  -8.000  -0.1783   0.03578   0.03200  -0.1197   0.7257   0.0155
  -7.750  -0.1906   0.03021   0.02606  -0.1165   0.7241   0.0158
  -7.500  -0.1757   0.02838   0.02416  -0.1156   0.7226   0.0160
  -7.250  -0.1578   0.02712   0.02283  -0.1149   0.7212   0.0162
  -7.000  -0.1391   0.02593   0.02154  -0.1142   0.7197   0.0165
  -6.750  -0.1340   0.02077   0.01560  -0.1105   0.7182   0.0160
  -6.500  -0.1121   0.01885   0.01359  -0.1098   0.7167   0.0143
  -6.250  -0.0906   0.01686   0.01131  -0.1087   0.7151   0.0140
  -6.000  -0.0671   0.01532   0.00954  -0.1079   0.7137   0.0138
  -5.750  -0.0418   0.01446   0.00858  -0.1075   0.7126   0.0141
  -5.500  -0.0159   0.01384   0.00789  -0.1072   0.7113   0.0145
  -5.250   0.0101   0.01323   0.00721  -0.1068   0.7099   0.0150
  -5.000   0.0361   0.01265   0.00657  -0.1064   0.7083   0.0152
  -4.750   0.0631   0.01235   0.00620  -0.1062   0.7068   0.0156
  -4.500   0.0865   0.01142   0.00525  -0.1056   0.7054   0.0162
  -4.250   0.1126   0.01103   0.00486  -0.1053   0.7040   0.0166
  -4.000   0.1391   0.01072   0.00453  -0.1051   0.7026   0.0171
  -3.750   0.1659   0.01046   0.00424  -0.1049   0.7011   0.0177
  -3.500   0.1929   0.01024   0.00399  -0.1048   0.6993   0.0184
  -3.250   0.2201   0.01008   0.00381  -0.1047   0.6979   0.0190
  -3.000   0.2461   0.00971   0.00345  -0.1044   0.6967   0.0204
  -2.750   0.2735   0.00953   0.00328  -0.1044   0.6951   0.0218
  -2.500   0.3011   0.00937   0.00311  -0.1043   0.6935   0.0230
  -2.250   0.3284   0.00914   0.00288  -0.1042   0.6919   0.0254
  -2.000   0.3563   0.00900   0.00274  -0.1043   0.6902   0.0283
  -1.750   0.3840   0.00881   0.00257  -0.1043   0.6886   0.0368
  -1.500   0.4068   0.00797   0.00238  -0.1038   0.6870   0.2446
  -1.250   0.4286   0.00712   0.00228  -0.1033   0.6853   0.4943
  -1.000   0.4525   0.00668   0.00230  -0.1027   0.6831   0.6520
  -0.750   0.4778   0.00651   0.00239  -0.1021   0.6817   0.7374
  -0.500   0.5049   0.00652   0.00248  -0.1018   0.6799   0.7738
  -0.250   0.5325   0.00656   0.00255  -0.1017   0.6778   0.7950
   0.000   0.5602   0.00660   0.00260  -0.1015   0.6757   0.8089
   0.250   0.5886   0.00661   0.00258  -0.1015   0.6733   0.8174
   0.500   0.6169   0.00660   0.00255  -0.1016   0.6701   0.8225
   0.750   0.6449   0.00661   0.00254  -0.1016   0.6662   0.8275
   1.000   0.6729   0.00659   0.00252  -0.1016   0.6622   0.8321
   1.250   0.7008   0.00655   0.00249  -0.1016   0.6588   0.8363
   1.500   0.7288   0.00656   0.00247  -0.1016   0.6554   0.8404
   1.750   0.7569   0.00660   0.00249  -0.1017   0.6518   0.8446
   2.000   0.7847   0.00660   0.00251  -0.1018   0.6478   0.8483
   2.250   0.8124   0.00658   0.00250  -0.1018   0.6437   0.8519
   2.500   0.8399   0.00660   0.00250  -0.1018   0.6397   0.8552
   2.750   0.8675   0.00662   0.00254  -0.1018   0.6356   0.8586
   3.000   0.8951   0.00664   0.00258  -0.1018   0.6309   0.8620
   3.250   0.9225   0.00667   0.00259  -0.1018   0.6255   0.8649
   3.500   0.9494   0.00669   0.00263  -0.1018   0.6199   0.8682
   3.750   0.9764   0.00671   0.00267  -0.1017   0.6136   0.8713
   4.000   1.0026   0.00677   0.00272  -0.1015   0.6071   0.8747
   4.250   1.0293   0.00682   0.00279  -0.1014   0.5988   0.8782
   4.500   1.0551   0.00690   0.00285  -0.1011   0.5902   0.8814
   4.750   1.0792   0.00699   0.00293  -0.1005   0.5777   0.8851
   5.000   1.1024   0.00712   0.00303  -0.0997   0.5609   0.8888
   5.250   1.1230   0.00736   0.00319  -0.0985   0.5365   0.8930
   5.500   1.1410   0.00769   0.00341  -0.0968   0.5086   0.8973
   5.750   1.1551   0.00809   0.00371  -0.0944   0.4773   0.9026
   6.000   1.1647   0.00864   0.00409  -0.0911   0.4416   0.9092
   6.250   1.1731   0.00914   0.00448  -0.0877   0.4105   0.9168
   6.500   1.1772   0.00960   0.00485  -0.0834   0.3837   0.9283
   6.750   1.1803   0.01010   0.00532  -0.0790   0.3587   0.9533
   7.000   1.1988   0.01084   0.00594  -0.0784   0.3289   1.0000
   7.250   1.2055   0.01150   0.00651  -0.0753   0.3089   1.0000
   7.500   1.2097   0.01233   0.00726  -0.0721   0.2889   1.0000
   7.750   1.2158   0.01327   0.00812  -0.0695   0.2728   1.0000
   8.000   1.2237   0.01422   0.00902  -0.0673   0.2574   1.0000
   8.250   1.2326   0.01517   0.00990  -0.0654   0.2430   1.0000
   8.500   1.2421   0.01611   0.01079  -0.0635   0.2296   1.0000
   8.750   1.2518   0.01705   0.01168  -0.0617   0.2171   1.0000
   9.000   1.2614   0.01801   0.01258  -0.0600   0.2049   1.0000
   9.250   1.2726   0.01891   0.01345  -0.0584   0.1939   1.0000
   9.500   1.2839   0.01981   0.01431  -0.0569   0.1835   1.0000
   9.750   1.2941   0.02079   0.01525  -0.0554   0.1740   1.0000
  10.000   1.3057   0.02170   0.01613  -0.0540   0.1648   1.0000
  10.250   1.3173   0.02262   0.01704  -0.0527   0.1569   1.0000
  10.500   1.3279   0.02362   0.01800  -0.0513   0.1487   1.0000
  10.750   1.3407   0.02450   0.01888  -0.0502   0.1421   1.0000
  11.000   1.3506   0.02557   0.01992  -0.0489   0.1348   1.0000
  11.250   1.3632   0.02649   0.02085  -0.0478   0.1287   1.0000
  11.500   1.3741   0.02753   0.02188  -0.0466   0.1226   1.0000
  11.750   1.3854   0.02859   0.02294  -0.0455   0.1169   1.0000
  12.000   1.3972   0.02964   0.02398  -0.0445   0.1116   1.0000
  12.250   1.4071   0.03085   0.02518  -0.0434   0.1057   1.0000
  12.500   1.4195   0.03191   0.02626  -0.0426   0.1012   1.0000
  12.750   1.4296   0.03313   0.02747  -0.0416   0.0967   1.0000
  13.000   1.4407   0.03432   0.02867  -0.0408   0.0912   1.0000
  13.250   1.4510   0.03559   0.02993  -0.0399   0.0870   1.0000
  13.500   1.4609   0.03691   0.03126  -0.0390   0.0836   1.0000
  13.750   1.4722   0.03814   0.03253  -0.0383   0.0804   1.0000
  14.000   1.4833   0.03939   0.03381  -0.0376   0.0780   1.0000
  14.250   1.4929   0.04078   0.03520  -0.0369   0.0748   1.0000
  14.500   1.5002   0.04240   0.03684  -0.0361   0.0715   1.0000
  14.750   1.5118   0.04368   0.03817  -0.0356   0.0700   1.0000
  15.000   1.5229   0.04500   0.03954  -0.0350   0.0684   1.0000
  15.250   1.5317   0.04656   0.04113  -0.0345   0.0662   1.0000
  15.500   1.5399   0.04817   0.04276  -0.0339   0.0644   1.0000
  15.750   1.5459   0.05002   0.04464  -0.0333   0.0619   1.0000
  16.000   1.5542   0.05168   0.04638  -0.0328   0.0605   1.0000
  16.250   1.5649   0.05313   0.04789  -0.0325   0.0592   1.0000
  16.500   1.5730   0.05485   0.04966  -0.0322   0.0573   1.0000
  16.750   1.5791   0.05679   0.05160  -0.0318   0.0546   1.0000
  17.000   1.5826   0.05902   0.05387  -0.0314   0.0522   1.0000
  17.250   1.5912   0.06076   0.05568  -0.0312   0.0508   1.0000
  17.500   1.5981   0.06268   0.05766  -0.0311   0.0491   1.0000
  17.750   1.6020   0.06498   0.05999  -0.0309   0.0466   1.0000
  18.000   1.6034   0.06759   0.06262  -0.0308   0.0438   1.0000
  18.250   1.6093   0.06972   0.06483  -0.0308   0.0421   1.0000
  18.500   1.6103   0.07245   0.06758  -0.0309   0.0388   1.0000
  18.750   1.6106   0.07530   0.07046  -0.0310   0.0357   1.0000
  19.000   1.6060   0.07885   0.07401  -0.0313   0.0309   1.0000
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