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NASA LRN 1015 (NASA TM 102840) (lrn1015-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: NASA LRN 1015 (NASA TM 102840) (lrn1015-il)
Reynolds number: 100,000
Max Cl/Cd: 34.03 at α=9°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-lrn1015-il-100000-n5.txt
Download as CSV file: xf-lrn1015-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.0754   0.10607   0.10015  -0.1030   0.8304   0.0583
 -11.000  -0.0898   0.10317   0.09732  -0.1077   0.8278   0.0616
 -10.750  -0.0956   0.09999   0.09417  -0.1111   0.8254   0.0619
 -10.500  -0.0867   0.09603   0.09022  -0.1114   0.8236   0.0626
 -10.250  -0.0707   0.09310   0.08730  -0.1102   0.8214   0.0637
 -10.000  -0.0627   0.09035   0.08457  -0.1106   0.8191   0.0647
  -9.750  -0.0576   0.08752   0.08177  -0.1115   0.8168   0.0659
  -9.500  -0.0551   0.08453   0.07881  -0.1126   0.8146   0.0670
  -9.000  -0.0935   0.06820   0.06242  -0.1243   0.8091   0.0356
  -8.750  -0.0948   0.06563   0.05988  -0.1244   0.8064   0.0348
  -8.500  -0.1068   0.06284   0.05709  -0.1242   0.8028   0.0341
  -8.000  -0.1522   0.05433   0.04801  -0.1218   0.7962   0.0300
  -7.750  -0.1481   0.05196   0.04551  -0.1207   0.7942   0.0298
  -7.500  -0.1442   0.04957   0.04293  -0.1194   0.7920   0.0295
  -7.250  -0.1406   0.04742   0.04062  -0.1178   0.7885   0.0292
  -7.000  -0.1350   0.04511   0.03807  -0.1161   0.7853   0.0290
  -6.750  -0.1265   0.04288   0.03553  -0.1144   0.7827   0.0290
  -6.500  -0.1156   0.04067   0.03290  -0.1128   0.7805   0.0294
  -6.250  -0.1025   0.03856   0.03018  -0.1109   0.7785   0.0301
  -6.000  -0.0839   0.03694   0.02844  -0.1102   0.7767   0.0308
  -5.750  -0.0715   0.03572   0.02701  -0.1083   0.7727   0.0309
  -5.500  -0.0547   0.03443   0.02545  -0.1068   0.7697   0.0310
  -5.250  -0.0351   0.03322   0.02401  -0.1057   0.7673   0.0313
  -5.000  -0.0130   0.03208   0.02266  -0.1048   0.7652   0.0317
  -4.750   0.0109   0.03101   0.02139  -0.1041   0.7633   0.0322
  -4.500   0.0363   0.03002   0.02023  -0.1035   0.7617   0.0331
  -4.250   0.0530   0.02965   0.01975  -0.1018   0.7582   0.0347
  -4.000   0.0687   0.02944   0.01942  -0.1000   0.7545   0.0362
  -3.750   0.0879   0.02884   0.01888  -0.0988   0.7515   0.0377
  -3.500   0.1101   0.02828   0.01830  -0.0979   0.7491   0.0390
  -3.250   0.1336   0.02776   0.01773  -0.0971   0.7472   0.0408
  -3.000   0.1576   0.02735   0.01723  -0.0963   0.7457   0.0433
  -2.750   0.1678   0.02747   0.01742  -0.0940   0.7413   0.0463
  -2.500   0.1795   0.02764   0.01756  -0.0918   0.7364   0.0500
  -2.250   0.1999   0.02747   0.01734  -0.0907   0.7337   0.0544
  -2.000   0.2239   0.02721   0.01707  -0.0901   0.7316   0.0656
  -1.750   0.2487   0.02655   0.01670  -0.0896   0.7300   0.1244
  -1.500   0.2437   0.02523   0.01739  -0.0850   0.7250   0.5811
  -1.250   0.2380   0.02584   0.01859  -0.0780   0.7193   0.7599
  -1.000   0.2449   0.02618   0.01900  -0.0724   0.7163   0.8432
  -0.750   0.2570   0.02631   0.01915  -0.0669   0.7144   0.9081
  -0.500   0.3017   0.02643   0.01912  -0.0689   0.7135   0.9403
  -0.250   0.3175   0.02746   0.02009  -0.0687   0.7062   0.9544
   0.000   0.3556   0.02780   0.02028  -0.0713   0.7031   0.9632
   0.250   0.3951   0.02795   0.02029  -0.0739   0.7009   0.9712
   0.500   0.4395   0.02801   0.02021  -0.0772   0.6994   0.9764
   0.750   0.4815   0.02798   0.02007  -0.0800   0.6981   0.9821
   1.000   0.5228   0.02801   0.02000  -0.0828   0.6966   0.9875
   1.250   0.5082   0.02936   0.02138  -0.0781   0.6856   1.0000
   1.500   0.5287   0.02925   0.02118  -0.0768   0.6833   1.0000
   1.750   0.5552   0.02905   0.02090  -0.0764   0.6817   1.0000
   2.000   0.5240   0.03038   0.02220  -0.0686   0.6693   1.0000
   2.250   0.5559   0.03021   0.02196  -0.0691   0.6675   1.0000
   2.750   0.5792   0.03136   0.02303  -0.0655   0.6540   1.0000
   3.000   0.6130   0.03108   0.02269  -0.0662   0.6520   1.0000
   3.500   0.6442   0.03199   0.02355  -0.0636   0.6382   1.0000
   3.750   0.6725   0.03185   0.02340  -0.0636   0.6345   1.0000
   4.000   0.6806   0.03266   0.02420  -0.0616   0.6245   1.0000
   4.250   0.7152   0.03213   0.02365  -0.0621   0.6221   1.0000
   4.750   0.7533   0.03259   0.02412  -0.0601   0.6077   1.0000
   5.250   0.7939   0.03283   0.02439  -0.0583   0.5931   1.0000
   5.500   0.8284   0.03198   0.02357  -0.0585   0.5903   1.0000
   5.750   0.8359   0.03286   0.02448  -0.0566   0.5779   1.0000
   6.250   0.8791   0.03277   0.02445  -0.0549   0.5620   1.0000
   6.500   0.8910   0.03343   0.02516  -0.0534   0.5497   1.0000
   7.000   0.9379   0.03308   0.02487  -0.0520   0.5313   1.0000
   7.250   0.9541   0.03349   0.02533  -0.0509   0.5179   1.0000
   7.500   0.9745   0.03357   0.02545  -0.0500   0.5046   1.0000
   7.750   0.9985   0.03338   0.02526  -0.0493   0.4908   1.0000
   8.000   1.0238   0.03308   0.02497  -0.0487   0.4756   1.0000
   8.250   1.0498   0.03274   0.02460  -0.0481   0.4581   1.0000
   8.500   1.0766   0.03234   0.02411  -0.0475   0.4379   1.0000
   8.750   1.0973   0.03246   0.02414  -0.0465   0.4153   1.0000
   9.000   1.1155   0.03278   0.02433  -0.0454   0.3914   1.0000
   9.250   1.1298   0.03346   0.02488  -0.0441   0.3682   1.0000
   9.500   1.1417   0.03436   0.02568  -0.0427   0.3461   1.0000
   9.750   1.1522   0.03538   0.02658  -0.0413   0.3255   1.0000
  10.000   1.1614   0.03656   0.02768  -0.0399   0.3065   1.0000
  10.250   1.1702   0.03781   0.02887  -0.0386   0.2890   1.0000
  10.500   1.1789   0.03912   0.03012  -0.0374   0.2730   1.0000
  10.750   1.1879   0.04043   0.03139  -0.0362   0.2587   1.0000
  11.000   1.1966   0.04180   0.03271  -0.0351   0.2455   1.0000
  11.250   1.2056   0.04321   0.03414  -0.0342   0.2328   1.0000
  11.500   1.2150   0.04463   0.03556  -0.0333   0.2214   1.0000
  11.750   1.2239   0.04610   0.03704  -0.0324   0.2110   1.0000
  12.000   1.2323   0.04765   0.03858  -0.0315   0.2012   1.0000
  12.250   1.2417   0.04916   0.04015  -0.0308   0.1918   1.0000
  12.500   1.2498   0.05078   0.04173  -0.0300   0.1842   1.0000
  12.750   1.2596   0.05234   0.04340  -0.0294   0.1760   1.0000
  13.000   1.2677   0.05400   0.04503  -0.0287   0.1697   1.0000
  13.250   1.2774   0.05563   0.04680  -0.0282   0.1625   1.0000
  13.500   1.2848   0.05743   0.04860  -0.0277   0.1566   1.0000
  13.750   1.2941   0.05914   0.05042  -0.0272   0.1506   1.0000
  14.000   1.3020   0.06098   0.05234  -0.0268   0.1452   1.0000
  14.250   1.3105   0.06273   0.05405  -0.0263   0.1408   1.0000
  14.500   1.3199   0.06452   0.05603  -0.0260   0.1362   1.0000
  14.750   1.3278   0.06645   0.05806  -0.0257   0.1319   1.0000
  15.000   1.3362   0.06828   0.05990  -0.0254   0.1283   1.0000
  15.250   1.3444   0.07025   0.06201  -0.0252   0.1247   1.0000
  15.500   1.3510   0.07244   0.06436  -0.0251   0.1209   1.0000
  15.750   1.3574   0.07460   0.06662  -0.0250   0.1177   1.0000
  16.000   1.3667   0.07641   0.06846  -0.0248   0.1150   1.0000
  16.250   1.3744   0.07852   0.07071  -0.0248   0.1124   1.0000
  16.500   1.3779   0.08122   0.07365  -0.0249   0.1097   1.0000
  16.750   1.3813   0.08389   0.07649  -0.0251   0.1070   1.0000
  17.000   1.3857   0.08641   0.07911  -0.0253   0.1045   1.0000
  17.250   1.3932   0.08848   0.08123  -0.0255   0.1022   1.0000
  17.500   1.3954   0.09139   0.08430  -0.0259   0.1000   1.0000
  17.750   1.3891   0.09555   0.08873  -0.0268   0.0977   1.0000
  18.000   1.3840   0.09959   0.09298  -0.0279   0.0954   1.0000
  18.250   1.3811   0.10328   0.09681  -0.0290   0.0930   1.0000
  18.500   1.3838   0.10609   0.09971  -0.0298   0.0907   1.0000
  18.750   1.3864   0.10894   0.10261  -0.0307   0.0886   1.0000
  19.000   1.3694   0.11519   0.10918  -0.0332   0.0871   1.0000
  19.250   1.3518   0.12171   0.11598  -0.0360   0.0854   1.0000
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