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NASA LRN 1015 (NASA TM 102840) (lrn1015-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: NASA LRN 1015 (NASA TM 102840) (lrn1015-il)
Reynolds number: 200,000
Max Cl/Cd: 70.79 at α=7.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-lrn1015-il-200000.txt
Download as CSV file: xf-lrn1015-il-200000.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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.750  -0.0469   0.09429   0.08995  -0.1141   0.8423   0.0456
 -10.500  -0.0487   0.09116   0.08682  -0.1162   0.8400   0.0471
 -10.250  -0.0697   0.08665   0.08242  -0.1220   0.8371   0.0483
 -10.000  -0.0837   0.08167   0.07751  -0.1270   0.8343   0.0484
  -9.750  -0.0574   0.08012   0.07595  -0.1219   0.8331   0.0497
  -9.500  -0.0467   0.07821   0.07406  -0.1212   0.8311   0.0509
  -9.250  -0.0430   0.07570   0.07157  -0.1217   0.8289   0.0524
  -9.000  -0.0459   0.07246   0.06835  -0.1233   0.8266   0.0541
  -8.750  -0.0571   0.06827   0.06419  -0.1265   0.8239   0.0552
  -8.500  -0.0739   0.06437   0.06033  -0.1289   0.8206   0.0555
  -8.250  -0.0995   0.06176   0.05767  -0.1283   0.8172   0.0565
  -8.000  -0.1370   0.06059   0.05605  -0.1262   0.8135   0.0580
  -7.750  -0.1357   0.05583   0.05127  -0.1258   0.8114   0.0591
  -7.500  -0.1193   0.05340   0.04895  -0.1254   0.8097   0.0605
  -7.250  -0.1102   0.05174   0.04728  -0.1244   0.8073   0.0624
  -7.000  -0.1055   0.05005   0.04549  -0.1232   0.8045   0.0659
  -6.750  -0.1123   0.04792   0.04289  -0.1209   0.8012   0.0710
  -6.500  -0.0953   0.04576   0.04086  -0.1205   0.7990   0.0734
  -6.000  -0.0712   0.04230   0.03704  -0.1181   0.7947   0.0865
  -5.750  -0.0535   0.04116   0.03579  -0.1171   0.7932   0.0930
  -5.500  -0.0487   0.03981   0.03431  -0.1152   0.7893   0.1009
  -5.250  -0.0340   0.03892   0.03339  -0.1138   0.7858   0.1076
  -5.000  -0.0199   0.03743   0.03178  -0.1126   0.7830   0.1185
  -4.750   0.0111   0.03214   0.02473  -0.1078   0.7810   0.0486
  -4.500   0.0354   0.02942   0.02194  -0.1073   0.7796   0.0455
  -4.250   0.0623   0.02807   0.02035  -0.1066   0.7783   0.0441
  -4.000   0.0704   0.02818   0.02041  -0.1040   0.7730   0.0450
  -3.750   0.0869   0.02789   0.02002  -0.1023   0.7694   0.0458
  -3.500   0.1102   0.02721   0.01925  -0.1014   0.7670   0.0458
  -3.250   0.1365   0.02650   0.01848  -0.1007   0.7651   0.0462
  -3.000   0.1641   0.02589   0.01781  -0.1003   0.7635   0.0474
  -2.750   0.1912   0.02524   0.01715  -0.0999   0.7623   0.0494
  -2.500   0.1773   0.02645   0.01845  -0.0946   0.7535   0.0506
  -2.250   0.1997   0.02623   0.01828  -0.0938   0.7508   0.0550
  -2.000   0.2261   0.02586   0.01787  -0.0934   0.7491   0.0596
  -1.750   0.2554   0.02545   0.01743  -0.0934   0.7476   0.0708
  -1.500   0.2450   0.02666   0.01871  -0.0885   0.7393   0.0794
  -1.250   0.2439   0.02464   0.01895  -0.0844   0.7353   0.6233
  -1.000   0.2550   0.02473   0.01953  -0.0791   0.7331   0.8163
  -0.750   0.2696   0.02484   0.01969  -0.0743   0.7315   0.8688
  -0.500   0.2394   0.02638   0.02128  -0.0662   0.7204   0.8820
  -0.250   0.2462   0.02633   0.02128  -0.0601   0.7178   0.9289
   0.000   0.3506   0.02677   0.02159  -0.0724   0.7187   0.9738
   0.250   0.4069   0.02669   0.02137  -0.0775   0.7177   0.9771
   0.500   0.4579   0.02651   0.02109  -0.0816   0.7167   0.9811
   0.750   0.5072   0.02630   0.02078  -0.0854   0.7158   0.9844
   1.000   0.5576   0.02600   0.02040  -0.0893   0.7150   0.9869
   1.250   0.6061   0.02563   0.01994  -0.0928   0.7143   0.9896
   1.500   0.6185   0.02720   0.02157  -0.0935   0.7027   1.0000
   1.750   0.5517   0.02839   0.02278  -0.0790   0.6904   1.0000
   2.000   0.5770   0.02804   0.02238  -0.0783   0.6875   1.0000
   2.250   0.6165   0.02749   0.02177  -0.0797   0.6861   1.0000
   2.500   0.6577   0.02674   0.02099  -0.0812   0.6851   1.0000
   2.750   0.7012   0.02588   0.02008  -0.0829   0.6843   1.0000
   3.000   0.7447   0.02498   0.01914  -0.0847   0.6836   1.0000
   3.250   0.7135   0.02635   0.02052  -0.0765   0.6704   1.0000
   3.500   0.7024   0.02762   0.02177  -0.0717   0.6588   1.0000
   3.750   0.7469   0.02664   0.02079  -0.0734   0.6576   1.0000
   4.000   0.7951   0.02548   0.01962  -0.0757   0.6569   1.0000
   4.250   0.8431   0.02422   0.01836  -0.0779   0.6562   1.0000
   4.500   0.8899   0.02295   0.01708  -0.0800   0.6554   1.0000
   4.750   0.9367   0.02174   0.01587  -0.0823   0.6544   1.0000
   5.000   0.9776   0.02080   0.01493  -0.0838   0.6520   1.0000
   5.250   0.9843   0.02118   0.01536  -0.0807   0.6421   1.0000
   5.500   1.0316   0.01991   0.01411  -0.0831   0.6401   1.0000
   5.750   1.0817   0.01858   0.01276  -0.0859   0.6379   1.0000
   6.000   1.0858   0.01897   0.01323  -0.0823   0.6269   1.0000
   6.250   1.1346   0.01772   0.01197  -0.0850   0.6231   1.0000
   6.500   1.1412   0.01794   0.01227  -0.0816   0.6117   1.0000
   6.750   1.1600   0.01773   0.01210  -0.0799   0.6014   1.0000
   7.000   1.1885   0.01716   0.01154  -0.0796   0.5907   1.0000
   7.250   1.2042   0.01701   0.01139  -0.0773   0.5764   1.0000
   7.500   1.2125   0.01719   0.01158  -0.0740   0.5587   1.0000
   7.750   1.2248   0.01734   0.01168  -0.0715   0.5378   1.0000
   8.000   1.2388   0.01754   0.01179  -0.0694   0.5129   1.0000
   8.250   1.2483   0.01805   0.01213  -0.0668   0.4835   1.0000
   8.500   1.2523   0.01893   0.01282  -0.0638   0.4521   1.0000
   8.750   1.2525   0.02012   0.01380  -0.0605   0.4211   1.0000
   9.250   1.2500   0.02297   0.01630  -0.0544   0.3656   1.0000
   9.500   1.2498   0.02446   0.01764  -0.0516   0.3421   1.0000
   9.750   1.2514   0.02592   0.01899  -0.0493   0.3205   1.0000
  10.000   1.2532   0.02743   0.02038  -0.0470   0.3011   1.0000
  10.250   1.2562   0.02891   0.02176  -0.0450   0.2836   1.0000
  10.500   1.2602   0.03038   0.02314  -0.0431   0.2674   1.0000
  10.750   1.2649   0.03185   0.02455  -0.0414   0.2522   1.0000
  11.000   1.2707   0.03328   0.02594  -0.0399   0.2381   1.0000
  11.250   1.2773   0.03472   0.02735  -0.0385   0.2253   1.0000
  11.500   1.2847   0.03614   0.02875  -0.0372   0.2140   1.0000
  11.750   1.2915   0.03764   0.03017  -0.0359   0.2036   1.0000
  12.000   1.2997   0.03909   0.03163  -0.0349   0.1935   1.0000
  12.250   1.3085   0.04052   0.03307  -0.0338   0.1843   1.0000
  12.500   1.3165   0.04203   0.03449  -0.0328   0.1760   1.0000
  12.750   1.3260   0.04348   0.03605  -0.0320   0.1680   1.0000
  13.000   1.3357   0.04490   0.03734  -0.0311   0.1607   1.0000
  13.250   1.3453   0.04640   0.03898  -0.0304   0.1542   1.0000
  13.500   1.3556   0.04783   0.04037  -0.0296   0.1486   1.0000
  13.750   1.3678   0.04915   0.04175  -0.0289   0.1433   1.0000
  14.000   1.3785   0.05060   0.04329  -0.0283   0.1386   1.0000
  14.250   1.3913   0.05186   0.04450  -0.0278   0.1340   1.0000
  14.500   1.4038   0.05323   0.04596  -0.0272   0.1301   1.0000
  14.750   1.4129   0.05488   0.04774  -0.0267   0.1262   1.0000
  15.000   1.4246   0.05630   0.04920  -0.0262   0.1229   1.0000
  15.250   1.4456   0.05702   0.04985  -0.0259   0.1189   1.0000
  15.500   1.4487   0.05922   0.05228  -0.0254   0.1162   1.0000
  15.750   1.4544   0.06123   0.05442  -0.0250   0.1129   1.0000
  16.000   1.4621   0.06304   0.05628  -0.0247   0.1098   1.0000
  16.250   1.4823   0.06382   0.05698  -0.0245   0.1060   1.0000
  16.500   1.4814   0.06653   0.05993  -0.0242   0.1041   1.0000
  16.750   1.4837   0.06903   0.06263  -0.0240   0.1016   1.0000
  17.000   1.4867   0.07139   0.06511  -0.0239   0.0988   1.0000
  17.250   1.4919   0.07352   0.06725  -0.0240   0.0959   1.0000
  17.500   1.4999   0.07551   0.06928  -0.0239   0.0928   1.0000
  17.750   1.4929   0.07918   0.07320  -0.0243   0.0906   1.0000
  18.000   1.4897   0.08251   0.07668  -0.0248   0.0879   1.0000
  18.250   1.4908   0.08529   0.07953  -0.0253   0.0853   1.0000
  18.500   1.5016   0.08682   0.08097  -0.0254   0.0819   1.0000
  18.750   1.4904   0.09143   0.08587  -0.0265   0.0803   1.0000
  19.000   1.4821   0.09578   0.09044  -0.0277   0.0780   1.0000
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