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NASA LRN 1015 (NASA TM 102840) (lrn1015-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NASA LRN 1015 (NASA TM 102840) (lrn1015-il)
Reynolds number: 500,000
Max Cl/Cd: 112.89 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-lrn1015-il-500000-n5.txt
Download as CSV file: xf-lrn1015-il-500000-n5.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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.750  -0.0847   0.08550   0.08170  -0.1066   0.7381   0.0104
 -10.500  -0.0841   0.08170   0.07793  -0.1083   0.7368   0.0101
 -10.250  -0.0880   0.07704   0.07329  -0.1104   0.7354   0.0103
 -10.000  -0.0923   0.07247   0.06875  -0.1126   0.7340   0.0102
  -9.750  -0.1010   0.06714   0.06345  -0.1155   0.7325   0.0098
  -9.500  -0.1165   0.06021   0.05655  -0.1205   0.7309   0.0099
  -9.250  -0.1519   0.05202   0.04828  -0.1258   0.7289   0.0098
  -9.000  -0.1847   0.04742   0.04358  -0.1239   0.7269   0.0096
  -8.750  -0.2008   0.04317   0.03917  -0.1222   0.7250   0.0096
  -8.500  -0.2117   0.03873   0.03450  -0.1200   0.7232   0.0097
  -8.250  -0.2165   0.03443   0.02990  -0.1177   0.7215   0.0098
  -8.000  -0.2168   0.03017   0.02527  -0.1153   0.7199   0.0099
  -7.750  -0.2111   0.02645   0.02113  -0.1130   0.7184   0.0102
  -7.500  -0.2008   0.02302   0.01720  -0.1109   0.7169   0.0107
  -7.250  -0.1837   0.02075   0.01451  -0.1095   0.7155   0.0110
  -7.000  -0.1628   0.01917   0.01259  -0.1085   0.7141   0.0112
  -6.750  -0.1401   0.01805   0.01130  -0.1079   0.7128   0.0114
  -6.500  -0.1161   0.01728   0.01045  -0.1075   0.7115   0.0116
  -6.250  -0.0914   0.01670   0.00981  -0.1071   0.7101   0.0118
  -6.000  -0.0663   0.01613   0.00919  -0.1067   0.7086   0.0121
  -5.750  -0.0411   0.01556   0.00854  -0.1063   0.7070   0.0125
  -5.500  -0.0158   0.01500   0.00791  -0.1059   0.7053   0.0128
  -5.250   0.0095   0.01446   0.00730  -0.1055   0.7037   0.0132
  -5.000   0.0349   0.01397   0.00674  -0.1051   0.7022   0.0135
  -4.750   0.0610   0.01362   0.00632  -0.1048   0.7009   0.0140
  -4.500   0.0862   0.01317   0.00587  -0.1045   0.6996   0.0146
  -4.250   0.1124   0.01287   0.00555  -0.1043   0.6983   0.0152
  -4.000   0.1386   0.01255   0.00519  -0.1040   0.6970   0.0158
  -3.750   0.1645   0.01225   0.00488  -0.1037   0.6953   0.0164
  -3.500   0.1907   0.01199   0.00460  -0.1035   0.6936   0.0170
  -3.250   0.2168   0.01170   0.00431  -0.1032   0.6920   0.0178
  -3.000   0.2435   0.01148   0.00411  -0.1031   0.6903   0.0188
  -2.750   0.2705   0.01130   0.00391  -0.1030   0.6886   0.0201
  -2.500   0.2975   0.01111   0.00372  -0.1029   0.6869   0.0222
  -2.250   0.3250   0.01096   0.00355  -0.1028   0.6854   0.0247
  -2.000   0.3524   0.01080   0.00339  -0.1028   0.6840   0.0282
  -1.750   0.3800   0.01066   0.00325  -0.1028   0.6825   0.0357
  -1.500   0.4060   0.01030   0.00312  -0.1027   0.6809   0.1055
  -1.250   0.4283   0.00953   0.00303  -0.1023   0.6790   0.3141
  -1.000   0.4476   0.00856   0.00299  -0.1013   0.6770   0.5906
  -0.750   0.4696   0.00828   0.00319  -0.0999   0.6749   0.7334
  -0.500   0.4957   0.00833   0.00331  -0.0993   0.6729   0.7743
  -0.250   0.5228   0.00839   0.00337  -0.0990   0.6710   0.7959
   0.000   0.5507   0.00841   0.00337  -0.0990   0.6691   0.8036
   0.250   0.5792   0.00844   0.00335  -0.0991   0.6673   0.8102
   0.500   0.6073   0.00849   0.00337  -0.0992   0.6652   0.8163
   0.750   0.6343   0.00852   0.00343  -0.0990   0.6625   0.8212
   1.000   0.6617   0.00855   0.00346  -0.0989   0.6593   0.8265
   1.250   0.6895   0.00855   0.00342  -0.0989   0.6554   0.8315
   1.500   0.7174   0.00851   0.00334  -0.0989   0.6510   0.8353
   1.750   0.7434   0.00852   0.00339  -0.0986   0.6449   0.8393
   2.000   0.7706   0.00852   0.00337  -0.0985   0.6397   0.8434
   2.250   0.7982   0.00854   0.00335  -0.0985   0.6354   0.8473
   2.500   0.8247   0.00857   0.00342  -0.0983   0.6296   0.8506
   2.750   0.8510   0.00858   0.00342  -0.0980   0.6233   0.8540
   3.000   0.8773   0.00862   0.00347  -0.0978   0.6171   0.8577
   3.250   0.9036   0.00866   0.00352  -0.0976   0.6103   0.8615
   3.500   0.9297   0.00872   0.00356  -0.0974   0.6034   0.8652
   3.750   0.9547   0.00877   0.00363  -0.0969   0.5944   0.8685
   4.000   0.9794   0.00884   0.00371  -0.0964   0.5844   0.8722
   4.250   1.0031   0.00895   0.00378  -0.0957   0.5717   0.8762
   4.500   1.0259   0.00909   0.00388  -0.0949   0.5563   0.8802
   4.750   1.0465   0.00927   0.00402  -0.0936   0.5380   0.8841
   5.000   1.0644   0.00953   0.00421  -0.0919   0.5166   0.8888
   5.250   1.0787   0.00990   0.00447  -0.0895   0.4896   0.8943
   5.500   1.0881   0.01037   0.00482  -0.0863   0.4605   0.9006
   5.750   1.0921   0.01089   0.00524  -0.0820   0.4318   0.9099
   6.000   1.0896   0.01148   0.00574  -0.0766   0.4039   0.9236
   6.250   1.0936   0.01227   0.00643  -0.0730   0.3735   0.9484
   6.750   1.1069   0.01437   0.00830  -0.0685   0.3201   1.0000
   7.000   1.1130   0.01542   0.00927  -0.0662   0.3009   1.0000
   7.250   1.1205   0.01646   0.01023  -0.0641   0.2833   1.0000
   7.500   1.1300   0.01742   0.01112  -0.0623   0.2689   1.0000
   7.750   1.1385   0.01844   0.01207  -0.0604   0.2530   1.0000
   8.000   1.1477   0.01945   0.01301  -0.0586   0.2380   1.0000
   8.250   1.1580   0.02041   0.01392  -0.0570   0.2253   1.0000
   8.500   1.1686   0.02137   0.01483  -0.0555   0.2142   1.0000
   8.750   1.1802   0.02229   0.01572  -0.0541   0.2032   1.0000
   9.000   1.1921   0.02321   0.01661  -0.0528   0.1934   1.0000
   9.250   1.2026   0.02422   0.01758  -0.0514   0.1837   1.0000
   9.500   1.2148   0.02515   0.01849  -0.0502   0.1744   1.0000
   9.750   1.2260   0.02615   0.01946  -0.0489   0.1654   1.0000
  10.000   1.2373   0.02716   0.02046  -0.0477   0.1575   1.0000
  10.250   1.2499   0.02810   0.02140  -0.0466   0.1510   1.0000
  10.500   1.2615   0.02912   0.02242  -0.0455   0.1441   1.0000
  10.750   1.2734   0.03016   0.02345  -0.0445   0.1382   1.0000
  11.000   1.2858   0.03119   0.02449  -0.0436   0.1321   1.0000
  11.250   1.2970   0.03233   0.02563  -0.0426   0.1265   1.0000
  11.500   1.3096   0.03339   0.02672  -0.0418   0.1215   1.0000
  11.750   1.3206   0.03459   0.02791  -0.0409   0.1158   1.0000
  12.000   1.3323   0.03575   0.02910  -0.0401   0.1111   1.0000
  12.250   1.3436   0.03698   0.03034  -0.0393   0.1063   1.0000
  12.500   1.3540   0.03829   0.03166  -0.0384   0.1020   1.0000
  12.750   1.3658   0.03951   0.03292  -0.0378   0.0987   1.0000
  13.000   1.3771   0.04079   0.03425  -0.0371   0.0956   1.0000
  13.250   1.3873   0.04218   0.03566  -0.0364   0.0921   1.0000
  13.500   1.3962   0.04372   0.03722  -0.0357   0.0886   1.0000
  13.750   1.4073   0.04507   0.03863  -0.0352   0.0860   1.0000
  14.000   1.4176   0.04652   0.04013  -0.0346   0.0834   1.0000
  14.250   1.4250   0.04824   0.04186  -0.0340   0.0796   1.0000
  14.500   1.4337   0.04988   0.04354  -0.0335   0.0764   1.0000
  14.750   1.4429   0.05150   0.04521  -0.0331   0.0733   1.0000
  15.000   1.4501   0.05333   0.04707  -0.0326   0.0703   1.0000
  15.250   1.4564   0.05529   0.04905  -0.0322   0.0675   1.0000
  15.500   1.4647   0.05707   0.05092  -0.0319   0.0662   1.0000
  15.750   1.4733   0.05884   0.05277  -0.0317   0.0643   1.0000
  16.000   1.4800   0.06084   0.05483  -0.0314   0.0622   1.0000
  16.250   1.4854   0.06302   0.05704  -0.0313   0.0599   1.0000
  16.500   1.4902   0.06530   0.05939  -0.0311   0.0585   1.0000
  16.750   1.4962   0.06746   0.06162  -0.0311   0.0563   1.0000
  17.000   1.5020   0.06968   0.06392  -0.0311   0.0541   1.0000
  17.250   1.5065   0.07208   0.06639  -0.0312   0.0523   1.0000
  17.500   1.5090   0.07478   0.06915  -0.0314   0.0505   1.0000
  17.750   1.5113   0.07753   0.07197  -0.0317   0.0487   1.0000
  18.000   1.5156   0.08008   0.07462  -0.0320   0.0470   1.0000
  18.250   1.5178   0.08293   0.07753  -0.0324   0.0444   1.0000
  18.500   1.5165   0.08627   0.08092  -0.0330   0.0418   1.0000
  18.750   1.5173   0.08940   0.08414  -0.0337   0.0395   1.0000
  19.000   1.5159   0.09287   0.08767  -0.0345   0.0363   1.0000
  19.250   1.5129   0.09661   0.09147  -0.0354   0.0331   1.0000
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