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NASA/LANGLEY MS(1)-0313 AIRFOIL (ms313-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: NASA/LANGLEY MS(1)-0313 AIRFOIL (ms313-il)
Reynolds number: 500,000
Max Cl/Cd: 74.38 at α=2.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-ms313-il-500000.txt
Download as CSV file: xf-ms313-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA/LANGLEY MS(1)-0313 AIRFOIL                 
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.6729   0.08134   0.07874  -0.0447   1.0000   0.0200
 -12.750  -0.7111   0.06851   0.06576  -0.0551   1.0000   0.0196
 -12.500  -0.7468   0.05917   0.05621  -0.0620   1.0000   0.0193
 -12.250  -0.7803   0.05184   0.04862  -0.0659   1.0000   0.0191
 -12.000  -0.8093   0.04609   0.04259  -0.0673   1.0000   0.0190
 -11.750  -0.8322   0.04195   0.03821  -0.0666   1.0000   0.0190
 -11.500  -0.8506   0.03883   0.03484  -0.0643   1.0000   0.0191
 -11.250  -0.8673   0.03666   0.03246  -0.0599   1.0000   0.0192
 -11.000  -0.8690   0.03386   0.02934  -0.0582   0.9980   0.0195
 -10.750  -0.8480   0.03052   0.02558  -0.0604   0.9948   0.0198
 -10.500  -0.8227   0.02818   0.02289  -0.0621   0.9918   0.0201
 -10.250  -0.7966   0.02585   0.02026  -0.0637   0.9885   0.0205
 -10.000  -0.7677   0.02389   0.01821  -0.0654   0.9862   0.0211
  -9.750  -0.7351   0.02279   0.01705  -0.0674   0.9844   0.0217
  -9.250  -0.6734   0.02079   0.01485  -0.0702   0.9778   0.0230
  -9.000  -0.6425   0.01985   0.01378  -0.0714   0.9741   0.0238
  -8.750  -0.6113   0.01897   0.01276  -0.0726   0.9709   0.0247
  -8.500  -0.5846   0.01790   0.01172  -0.0731   0.9656   0.0258
  -8.250  -0.5568   0.01732   0.01112  -0.0735   0.9600   0.0268
  -8.000  -0.5288   0.01671   0.01044  -0.0739   0.9555   0.0278
  -7.750  -0.5032   0.01619   0.00985  -0.0737   0.9490   0.0288
  -7.500  -0.4785   0.01532   0.00894  -0.0735   0.9434   0.0300
  -7.250  -0.4524   0.01481   0.00843  -0.0735   0.9385   0.0315
  -7.000  -0.4259   0.01442   0.00802  -0.0735   0.9326   0.0332
  -6.750  -0.3990   0.01412   0.00764  -0.0734   0.9273   0.0347
  -6.500  -0.3733   0.01336   0.00690  -0.0735   0.9228   0.0371
  -6.250  -0.3455   0.01300   0.00653  -0.0737   0.9176   0.0395
  -6.000  -0.3178   0.01255   0.00605  -0.0739   0.9129   0.0425
  -5.750  -0.2900   0.01219   0.00569  -0.0741   0.9087   0.0462
  -5.500  -0.2615   0.01182   0.00529  -0.0745   0.9044   0.0507
  -5.250  -0.2326   0.01150   0.00499  -0.0749   0.8997   0.0566
  -5.000  -0.2036   0.01113   0.00465  -0.0754   0.8955   0.0660
  -4.750  -0.1745   0.01079   0.00435  -0.0758   0.8919   0.0810
  -4.500  -0.1448   0.01033   0.00407  -0.0766   0.8881   0.1165
  -4.250  -0.1144   0.00962   0.00376  -0.0779   0.8838   0.2073
  -4.000  -0.0828   0.00875   0.00343  -0.0797   0.8800   0.3445
  -3.750  -0.0502   0.00790   0.00322  -0.0815   0.8768   0.5124
  -3.500  -0.0200   0.00774   0.00325  -0.0820   0.8735   0.5807
  -3.250   0.0102   0.00772   0.00330  -0.0824   0.8695   0.6139
  -3.000   0.0401   0.00775   0.00334  -0.0827   0.8655   0.6356
  -2.750   0.0697   0.00780   0.00338  -0.0829   0.8618   0.6525
  -2.500   0.0991   0.00787   0.00343  -0.0830   0.8584   0.6662
  -2.250   0.1288   0.00796   0.00349  -0.0833   0.8549   0.6780
  -2.000   0.1584   0.00807   0.00360  -0.0835   0.8507   0.6912
  -1.750   0.1867   0.00819   0.00376  -0.0833   0.8464   0.7036
  -1.500   0.2155   0.00822   0.00372  -0.0832   0.8405   0.7109
  -1.250   0.2429   0.00815   0.00363  -0.0826   0.8285   0.7160
  -1.000   0.2706   0.00812   0.00354  -0.0821   0.8149   0.7234
  -0.750   0.2986   0.00813   0.00352  -0.0818   0.8058   0.7301
  -0.500   0.3272   0.00814   0.00354  -0.0817   0.7973   0.7352
  -0.250   0.3566   0.00815   0.00349  -0.0819   0.7899   0.7394
   0.000   0.3866   0.00813   0.00344  -0.0823   0.7805   0.7432
   0.250   0.4152   0.00811   0.00341  -0.0822   0.7719   0.7461
   0.500   0.4441   0.00810   0.00341  -0.0823   0.7620   0.7493
   0.750   0.4733   0.00811   0.00340  -0.0824   0.7526   0.7527
   1.000   0.5026   0.00813   0.00338  -0.0826   0.7412   0.7564
   1.250   0.5321   0.00815   0.00336  -0.0829   0.7264   0.7599
   1.500   0.5603   0.00816   0.00334  -0.0828   0.7086   0.7626
   1.750   0.5885   0.00820   0.00336  -0.0827   0.6862   0.7656
   2.000   0.6161   0.00831   0.00338  -0.0825   0.6527   0.7689
   2.250   0.6419   0.00863   0.00341  -0.0821   0.5875   0.7725
   2.500   0.6641   0.00942   0.00365  -0.0812   0.4782   0.7758
   2.750   0.6858   0.01020   0.00399  -0.0804   0.3840   0.7788
   3.000   0.7090   0.01085   0.00430  -0.0798   0.3126   0.7818
   3.250   0.7333   0.01140   0.00458  -0.0794   0.2588   0.7850
   3.500   0.7584   0.01188   0.00486  -0.0791   0.2208   0.7886
   3.750   0.7846   0.01229   0.00511  -0.0790   0.1939   0.7922
   4.000   0.8099   0.01264   0.00537  -0.0787   0.1744   0.7951
   4.250   0.8355   0.01297   0.00564  -0.0784   0.1604   0.7981
   4.500   0.8614   0.01327   0.00591  -0.0781   0.1499   0.8017
   4.750   0.8872   0.01363   0.00622  -0.0779   0.1411   0.8054
   5.000   0.9138   0.01392   0.00649  -0.0778   0.1346   0.8090
   5.250   0.9376   0.01434   0.00688  -0.0772   0.1281   0.8120
   5.500   0.9636   0.01457   0.00715  -0.0769   0.1248   0.8155
   5.750   0.9891   0.01486   0.00747  -0.0765   0.1210   0.8194
   6.000   1.0139   0.01526   0.00784  -0.0762   0.1173   0.8233
   6.250   1.0369   0.01577   0.00836  -0.0755   0.1136   0.8268
   6.500   1.0619   0.01602   0.00868  -0.0750   0.1116   0.8304
   6.750   1.0866   0.01632   0.00902  -0.0745   0.1091   0.8346
   7.000   1.1112   0.01667   0.00940  -0.0741   0.1068   0.8389
   7.250   1.1344   0.01709   0.00984  -0.0735   0.1045   0.8427
   7.500   1.1552   0.01769   0.01045  -0.0724   0.1020   0.8467
   7.750   1.1766   0.01829   0.01110  -0.0714   0.1001   0.8515
   8.000   1.2010   0.01861   0.01148  -0.0710   0.0987   0.8565
   8.250   1.2235   0.01891   0.01187  -0.0702   0.0969   0.8609
   8.500   1.2461   0.01926   0.01227  -0.0694   0.0948   0.8659
   8.750   1.2685   0.01964   0.01269  -0.0687   0.0928   0.8714
   9.000   1.2882   0.02014   0.01322  -0.0675   0.0909   0.8768
   9.250   1.3053   0.02108   0.01418  -0.0660   0.0883   0.8831
   9.500   1.3260   0.02148   0.01467  -0.0650   0.0873   0.8896
   9.750   1.3455   0.02181   0.01511  -0.0637   0.0860   0.8968
  10.000   1.3634   0.02217   0.01557  -0.0621   0.0844   0.9050
  10.250   1.3790   0.02255   0.01604  -0.0602   0.0828   0.9152
  10.500   1.3940   0.02294   0.01651  -0.0582   0.0813   0.9291
  10.750   1.4043   0.02328   0.01693  -0.0553   0.0798   0.9666
  11.000   1.4207   0.02415   0.01780  -0.0541   0.0777   1.0000
  11.250   1.4388   0.02506   0.01877  -0.0532   0.0760   1.0000
  11.500   1.4580   0.02554   0.01936  -0.0525   0.0747   1.0000
  11.750   1.4763   0.02612   0.02001  -0.0516   0.0729   1.0000
  12.000   1.4936   0.02675   0.02070  -0.0507   0.0711   1.0000
  12.250   1.5100   0.02743   0.02142  -0.0497   0.0694   1.0000
  12.500   1.5232   0.02842   0.02241  -0.0484   0.0674   1.0000
  12.750   1.5362   0.02950   0.02356  -0.0471   0.0655   1.0000
  13.000   1.5526   0.03019   0.02437  -0.0462   0.0639   1.0000
  13.250   1.5680   0.03098   0.02524  -0.0453   0.0620   1.0000
  13.500   1.5827   0.03183   0.02613  -0.0444   0.0600   1.0000
  13.750   1.5927   0.03309   0.02739  -0.0431   0.0579   1.0000
  14.000   1.6043   0.03429   0.02868  -0.0420   0.0559   1.0000
  14.250   1.6190   0.03521   0.02971  -0.0413   0.0537   1.0000
  14.500   1.6318   0.03629   0.03083  -0.0405   0.0515   1.0000
  14.750   1.6377   0.03802   0.03255  -0.0394   0.0492   1.0000
  15.000   1.6489   0.03933   0.03399  -0.0386   0.0473   1.0000
  15.250   1.6587   0.04079   0.03553  -0.0378   0.0452   1.0000
  15.500   1.6647   0.04261   0.03740  -0.0369   0.0435   1.0000
  16.000   1.6695   0.04712   0.04208  -0.0352   0.0404   1.0000
  16.250   1.6731   0.04935   0.04443  -0.0346   0.0390   1.0000
  16.500   1.6735   0.05199   0.04714  -0.0341   0.0376   1.0000
  16.750   1.6693   0.05527   0.05049  -0.0339   0.0364   1.0000
  17.000   1.6612   0.05918   0.05449  -0.0340   0.0354   1.0000
  17.250   1.6594   0.06250   0.05798  -0.0342   0.0345   1.0000
  17.500   1.6547   0.06631   0.06192  -0.0348   0.0335   1.0000
  17.750   1.6465   0.07078   0.06652  -0.0358   0.0327   1.0000
  18.000   1.6350   0.07594   0.07181  -0.0374   0.0320   1.0000
  18.250   1.6195   0.08195   0.07794  -0.0396   0.0314   1.0000
  18.500   1.5994   0.08892   0.08504  -0.0425   0.0309   1.0000
  18.750   1.5758   0.09671   0.09298  -0.0460   0.0305   1.0000
  19.000   1.5498   0.10512   0.10152  -0.0500   0.0301   1.0000
  19.250   1.5276   0.11304   0.10962  -0.0540   0.0298   1.0000
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