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NASA LRN 1015 (NASA TM 102840) (lrn1015-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: NASA LRN 1015 (NASA TM 102840) (lrn1015-il)
Reynolds number: 500,000
Max Cl/Cd: 127.7 at α=6°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-lrn1015-il-500000.txt
Download as CSV file: xf-lrn1015-il-500000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.0268   0.08901   0.08570  -0.0970   0.7685   0.0208
 -11.000  -0.0240   0.08546   0.08216  -0.0983   0.7673   0.0213
 -10.750  -0.0227   0.08163   0.07833  -0.0998   0.7662   0.0219
 -10.500  -0.0238   0.07736   0.07406  -0.1016   0.7651   0.0224
 -10.250  -0.0393   0.07000   0.06672  -0.1062   0.7641   0.0231
 -10.000  -0.0470   0.06416   0.06088  -0.1094   0.7631   0.0231
  -9.750  -0.0613   0.05609   0.05280  -0.1152   0.7619   0.0231
  -9.500  -0.0877   0.06351   0.06006  -0.1262   0.7645   0.0230
  -9.000  -0.1100   0.04154   0.03820  -0.1218   0.7569   0.0235
  -8.750  -0.1310   0.03866   0.03525  -0.1205   0.7547   0.0235
  -8.500  -0.1388   0.03638   0.03294  -0.1186   0.7528   0.0236
  -8.250  -0.1394   0.03401   0.03052  -0.1174   0.7512   0.0237
  -8.000  -0.1374   0.03172   0.02817  -0.1163   0.7496   0.0240
  -7.750  -0.1334   0.02947   0.02582  -0.1152   0.7482   0.0243
  -7.500  -0.1283   0.02708   0.02331  -0.1140   0.7466   0.0248
  -7.250  -0.1219   0.02459   0.02068  -0.1128   0.7449   0.0256
  -7.000  -0.1272   0.02129   0.01664  -0.1088   0.7427   0.0280
  -6.750  -0.1127   0.01794   0.01339  -0.1090   0.7412   0.0287
  -6.500  -0.0951   0.01640   0.01181  -0.1084   0.7395   0.0293
  -6.250  -0.0769   0.01503   0.01035  -0.1078   0.7378   0.0305
  -6.000  -0.0638   0.01297   0.00770  -0.1056   0.7360   0.0342
  -5.750  -0.0417   0.01156   0.00634  -0.1057   0.7345   0.0351
  -5.500  -0.0194   0.01056   0.00526  -0.1054   0.7331   0.0366
  -5.250   0.0013   0.00947   0.00379  -0.1044   0.7318   0.0415
  -5.000   0.0336   0.01900   0.01220  -0.1074   0.7333   0.0232
  -4.750   0.0602   0.01773   0.01084  -0.1071   0.7320   0.0230
  -4.500   0.0868   0.01686   0.00985  -0.1067   0.7308   0.0232
  -4.250   0.1121   0.01589   0.00885  -0.1063   0.7294   0.0235
  -4.000   0.1363   0.01515   0.00815  -0.1057   0.7277   0.0240
  -3.750   0.1611   0.01467   0.00771  -0.1052   0.7257   0.0249
  -3.500   0.1866   0.01434   0.00739  -0.1048   0.7238   0.0262
  -3.250   0.2125   0.01405   0.00707  -0.1045   0.7221   0.0274
  -3.000   0.2375   0.01358   0.00659  -0.1040   0.7204   0.0284
  -2.750   0.2631   0.01317   0.00618  -0.1037   0.7189   0.0302
  -2.500   0.2900   0.01290   0.00589  -0.1035   0.7174   0.0324
  -2.250   0.3169   0.01261   0.00558  -0.1034   0.7161   0.0359
  -2.000   0.3444   0.01244   0.00538  -0.1033   0.7148   0.0424
  -1.750   0.3668   0.01173   0.00519  -0.1027   0.7130   0.1828
  -1.500   0.3794   0.01018   0.00513  -0.1009   0.7107   0.6121
  -1.250   0.4011   0.01001   0.00537  -0.0994   0.7085   0.7373
  -1.000   0.4267   0.01011   0.00551  -0.0986   0.7065   0.7829
  -0.750   0.4516   0.01024   0.00569  -0.0976   0.7046   0.8138
  -0.500   0.4768   0.01035   0.00581  -0.0966   0.7030   0.8340
  -0.250   0.5024   0.01043   0.00588  -0.0957   0.7014   0.8497
   0.000   0.5299   0.01045   0.00587  -0.0954   0.7000   0.8568
   0.250   0.5581   0.01053   0.00590  -0.0954   0.6982   0.8635
   0.500   0.5823   0.01056   0.00597  -0.0947   0.6955   0.8689
   0.750   0.6080   0.01058   0.00600  -0.0943   0.6926   0.8747
   1.000   0.6357   0.01054   0.00593  -0.0942   0.6900   0.8804
   1.250   0.6637   0.01037   0.00574  -0.0941   0.6873   0.8849
   1.500   0.6937   0.01019   0.00550  -0.0944   0.6845   0.8895
   1.750   0.7200   0.01014   0.00544  -0.0941   0.6806   0.8945
   2.000   0.7456   0.01004   0.00537  -0.0936   0.6764   0.8989
   2.250   0.7731   0.00990   0.00522  -0.0935   0.6729   0.9031
   2.500   0.8023   0.00977   0.00505  -0.0937   0.6699   0.9074
   2.750   0.8294   0.00973   0.00500  -0.0936   0.6662   0.9119
   3.000   0.8536   0.00964   0.00496  -0.0929   0.6614   0.9161
   3.250   0.8806   0.00952   0.00485  -0.0927   0.6573   0.9207
   3.500   0.9092   0.00943   0.00472  -0.0929   0.6537   0.9252
   3.750   0.9330   0.00939   0.00474  -0.0922   0.6488   0.9301
   4.000   0.9578   0.00931   0.00469  -0.0916   0.6434   0.9353
   4.250   0.9853   0.00921   0.00457  -0.0915   0.6386   0.9406
   4.500   1.0087   0.00918   0.00462  -0.0908   0.6322   0.9465
   4.750   1.0344   0.00912   0.00457  -0.0904   0.6258   0.9531
   5.000   1.0610   0.00910   0.00459  -0.0903   0.6186   0.9599
   5.250   1.0906   0.00909   0.00460  -0.0909   0.6103   0.9667
   5.500   1.1225   0.00913   0.00468  -0.0921   0.6000   0.9740
   5.750   1.1558   0.00919   0.00474  -0.0936   0.5854   0.9824
   6.000   1.1889   0.00931   0.00483  -0.0952   0.5671   0.9985
   6.250   1.2069   0.00952   0.00496  -0.0936   0.5467   1.0000
   6.500   1.2223   0.00985   0.00519  -0.0917   0.5201   1.0000
   6.750   1.2328   0.01034   0.00553  -0.0889   0.4894   1.0000
   7.000   1.2359   0.01096   0.00598  -0.0847   0.4581   1.0000
   7.250   1.2336   0.01170   0.00657  -0.0797   0.4290   1.0000
   7.500   1.2304   0.01260   0.00734  -0.0749   0.4019   1.0000
   8.000   1.2248   0.01504   0.00955  -0.0671   0.3530   1.0000
   8.250   1.2243   0.01643   0.01083  -0.0640   0.3304   1.0000
   8.500   1.2269   0.01773   0.01202  -0.0614   0.3089   1.0000
   8.750   1.2313   0.01896   0.01317  -0.0590   0.2896   1.0000
   9.000   1.2369   0.02016   0.01430  -0.0569   0.2727   1.0000
   9.250   1.2434   0.02135   0.01541  -0.0549   0.2568   1.0000
   9.500   1.2508   0.02249   0.01650  -0.0531   0.2423   1.0000
   9.750   1.2586   0.02364   0.01760  -0.0514   0.2289   1.0000
  10.000   1.2667   0.02480   0.01871  -0.0498   0.2164   1.0000
  10.250   1.2741   0.02602   0.01987  -0.0482   0.2047   1.0000
  10.500   1.2836   0.02714   0.02096  -0.0468   0.1930   1.0000
  10.750   1.2938   0.02823   0.02204  -0.0455   0.1834   1.0000
  11.000   1.3016   0.02950   0.02327  -0.0441   0.1736   1.0000
  11.250   1.3115   0.03068   0.02444  -0.0429   0.1642   1.0000
  11.500   1.3219   0.03187   0.02563  -0.0419   0.1565   1.0000
  11.750   1.3304   0.03322   0.02695  -0.0407   0.1485   1.0000
  12.000   1.3418   0.03438   0.02813  -0.0398   0.1417   1.0000
  12.250   1.3497   0.03583   0.02957  -0.0387   0.1348   1.0000
  12.500   1.3605   0.03709   0.03086  -0.0379   0.1290   1.0000
  12.750   1.3697   0.03850   0.03227  -0.0370   0.1233   1.0000
  13.000   1.3767   0.04011   0.03388  -0.0360   0.1181   1.0000
  13.250   1.3882   0.04137   0.03519  -0.0353   0.1137   1.0000
  13.500   1.3957   0.04301   0.03683  -0.0345   0.1094   1.0000
  13.750   1.4020   0.04477   0.03861  -0.0336   0.1053   1.0000
  14.000   1.4140   0.04604   0.03997  -0.0331   0.1022   1.0000
  14.250   1.4221   0.04770   0.04165  -0.0325   0.0982   1.0000
  14.500   1.4263   0.04974   0.04368  -0.0318   0.0944   1.0000
  14.750   1.4369   0.05122   0.04524  -0.0314   0.0918   1.0000
  15.000   1.4474   0.05273   0.04682  -0.0311   0.0885   1.0000
  15.250   1.4543   0.05462   0.04873  -0.0307   0.0855   1.0000
  15.500   1.4570   0.05693   0.05106  -0.0301   0.0828   1.0000
  15.750   1.4661   0.05864   0.05286  -0.0299   0.0806   1.0000
  16.000   1.4752   0.06039   0.05470  -0.0297   0.0786   1.0000
  16.250   1.4823   0.06237   0.05674  -0.0296   0.0764   1.0000
  16.500   1.4871   0.06463   0.05905  -0.0294   0.0742   1.0000
  16.750   1.4888   0.06725   0.06170  -0.0293   0.0721   1.0000
  17.000   1.4936   0.06956   0.06409  -0.0293   0.0704   1.0000
  17.250   1.5014   0.07157   0.06622  -0.0294   0.0688   1.0000
  17.500   1.5078   0.07380   0.06853  -0.0296   0.0665   1.0000
  17.750   1.5111   0.07642   0.07120  -0.0298   0.0643   1.0000
  18.000   1.5106   0.07956   0.07439  -0.0302   0.0622   1.0000
  18.250   1.5121   0.08246   0.07737  -0.0306   0.0605   1.0000
  18.500   1.5182   0.08483   0.07987  -0.0311   0.0587   1.0000
  18.750   1.5218   0.08756   0.08270  -0.0317   0.0566   1.0000
  19.000   1.5221   0.09078   0.08597  -0.0324   0.0545   1.0000
  19.250   1.5182   0.09463   0.08987  -0.0334   0.0525   1.0000
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