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NASA/LANGLEY MS(1)-0313 AIRFOIL (ms313-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NASA/LANGLEY MS(1)-0313 AIRFOIL (ms313-il)
Reynolds number: 1,000,000
Max Cl/Cd: 87.09 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ms313-il-1000000-n5.txt
Download as CSV file: xf-ms313-il-1000000-n5.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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -0.9770   0.11413   0.11160  -0.0215   1.0000   0.0086
 -18.000  -1.0483   0.09596   0.09317  -0.0314   1.0000   0.0084
 -17.750  -1.1105   0.07973   0.07670  -0.0410   1.0000   0.0084
 -17.500  -1.1454   0.06904   0.06579  -0.0478   1.0000   0.0084
 -17.250  -1.1673   0.06138   0.05797  -0.0526   1.0000   0.0084
 -17.000  -1.1816   0.05553   0.05196  -0.0560   1.0000   0.0084
 -16.750  -1.1915   0.05080   0.04709  -0.0584   1.0000   0.0084
 -16.500  -1.1976   0.04683   0.04300  -0.0602   1.0000   0.0084
 -16.250  -1.2043   0.04303   0.03908  -0.0617   1.0000   0.0085
 -16.000  -1.2086   0.03969   0.03562  -0.0627   1.0000   0.0086
 -15.750  -1.2093   0.03690   0.03272  -0.0633   1.0000   0.0087
 -15.500  -1.2071   0.03450   0.03023  -0.0636   1.0000   0.0088
 -15.250  -1.2022   0.03245   0.02809  -0.0638   1.0000   0.0089
 -15.000  -1.1952   0.03065   0.02621  -0.0637   1.0000   0.0089
 -14.750  -1.1864   0.02907   0.02456  -0.0635   1.0000   0.0091
 -14.500  -1.1764   0.02766   0.02307  -0.0632   1.0000   0.0092
 -14.250  -1.1654   0.02639   0.02173  -0.0628   1.0000   0.0093
 -14.000  -1.1545   0.02522   0.02050  -0.0621   1.0000   0.0094
 -13.750  -1.1441   0.02417   0.01939  -0.0612   1.0000   0.0095
 -13.500  -1.1293   0.02321   0.01837  -0.0608   1.0000   0.0096
 -13.250  -1.1121   0.02237   0.01747  -0.0604   1.0000   0.0098
 -13.000  -1.0872   0.02154   0.01658  -0.0614   0.9925   0.0100
 -12.750  -1.0610   0.02075   0.01572  -0.0624   0.9841   0.0102
 -12.500  -1.0349   0.02001   0.01491  -0.0632   0.9751   0.0104
 -12.250  -1.0096   0.01932   0.01415  -0.0637   0.9657   0.0106
 -11.750  -0.9624   0.01814   0.01280  -0.0637   0.9450   0.0108
 -11.500  -0.9399   0.01745   0.01204  -0.0634   0.9362   0.0111
 -11.250  -0.9164   0.01685   0.01137  -0.0633   0.9279   0.0114
 -11.000  -0.8920   0.01635   0.01082  -0.0632   0.9208   0.0117
 -10.750  -0.8668   0.01588   0.01030  -0.0632   0.9135   0.0120
 -10.500  -0.8415   0.01546   0.00981  -0.0632   0.9068   0.0123
 -10.250  -0.8153   0.01504   0.00934  -0.0633   0.9007   0.0126
 -10.000  -0.7890   0.01464   0.00889  -0.0634   0.8948   0.0129
  -9.750  -0.7624   0.01426   0.00844  -0.0635   0.8897   0.0132
  -9.500  -0.7352   0.01390   0.00803  -0.0638   0.8848   0.0135
  -9.250  -0.7081   0.01348   0.00758  -0.0640   0.8796   0.0139
  -9.000  -0.6810   0.01310   0.00716  -0.0642   0.8745   0.0145
  -8.750  -0.6532   0.01277   0.00680  -0.0645   0.8700   0.0150
  -8.500  -0.6251   0.01246   0.00647  -0.0648   0.8654   0.0156
  -8.250  -0.5969   0.01218   0.00615  -0.0651   0.8610   0.0162
  -7.750  -0.5400   0.01160   0.00551  -0.0658   0.8530   0.0176
  -7.500  -0.5113   0.01132   0.00523  -0.0662   0.8486   0.0184
  -7.250  -0.4824   0.01108   0.00496  -0.0666   0.8442   0.0193
  -6.750  -0.4243   0.01060   0.00444  -0.0674   0.8369   0.0213
  -6.500  -0.3949   0.01038   0.00422  -0.0679   0.8330   0.0228
  -6.250  -0.3655   0.01018   0.00401  -0.0684   0.8290   0.0242
  -6.000  -0.3361   0.00997   0.00378  -0.0688   0.8251   0.0259
  -5.750  -0.3065   0.00978   0.00359  -0.0693   0.8216   0.0279
  -5.500  -0.2767   0.00959   0.00340  -0.0698   0.8180   0.0301
  -5.250  -0.2469   0.00940   0.00322  -0.0703   0.8144   0.0332
  -5.000  -0.2171   0.00923   0.00306  -0.0708   0.8108   0.0364
  -4.500  -0.1572   0.00890   0.00275  -0.0719   0.8039   0.0462
  -4.250  -0.1270   0.00872   0.00261  -0.0725   0.8005   0.0543
  -4.000  -0.0968   0.00855   0.00248  -0.0731   0.7970   0.0647
  -3.750  -0.0666   0.00838   0.00235  -0.0737   0.7934   0.0788
  -3.500  -0.0362   0.00817   0.00222  -0.0744   0.7902   0.1025
  -3.250  -0.0053   0.00790   0.00210  -0.0752   0.7870   0.1388
  -3.000   0.0258   0.00759   0.00197  -0.0762   0.7835   0.1890
  -2.750   0.0572   0.00724   0.00185  -0.0772   0.7799   0.2530
  -2.500   0.0885   0.00694   0.00174  -0.0782   0.7764   0.3154
  -2.250   0.1210   0.00645   0.00159  -0.0797   0.7715   0.4190
  -2.000   0.1527   0.00609   0.00149  -0.0808   0.7590   0.5141
  -1.750   0.1829   0.00598   0.00144  -0.0814   0.7375   0.5607
  -1.500   0.2129   0.00594   0.00143  -0.0818   0.7145   0.5990
  -1.250   0.2428   0.00596   0.00145  -0.0822   0.6984   0.6262
  -1.000   0.2725   0.00600   0.00146  -0.0825   0.6818   0.6364
  -0.750   0.3017   0.00611   0.00146  -0.0827   0.6566   0.6437
  -0.500   0.3304   0.00628   0.00150  -0.0829   0.6159   0.6528
  -0.250   0.3584   0.00658   0.00159  -0.0830   0.5599   0.6620
   0.000   0.3858   0.00698   0.00172  -0.0830   0.4950   0.6691
   0.250   0.4129   0.00742   0.00187  -0.0830   0.4274   0.6733
   0.500   0.4400   0.00785   0.00202  -0.0831   0.3634   0.6763
   0.750   0.4676   0.00818   0.00216  -0.0832   0.3161   0.6794
   1.000   0.4955   0.00846   0.00228  -0.0833   0.2787   0.6825
   1.250   0.5235   0.00873   0.00241  -0.0834   0.2465   0.6857
   1.500   0.5514   0.00898   0.00253  -0.0835   0.2199   0.6889
   1.750   0.5796   0.00921   0.00265  -0.0837   0.1986   0.6917
   2.000   0.6076   0.00942   0.00278  -0.0838   0.1791   0.6944
   2.250   0.6356   0.00963   0.00292  -0.0839   0.1630   0.6973
   2.500   0.6638   0.00981   0.00305  -0.0840   0.1514   0.7004
   2.750   0.6918   0.01001   0.00319  -0.0841   0.1411   0.7034
   3.000   0.7199   0.01019   0.00333  -0.0842   0.1329   0.7063
   3.250   0.7479   0.01037   0.00346  -0.0843   0.1259   0.7090
   3.500   0.7759   0.01054   0.00362  -0.0844   0.1198   0.7118
   3.750   0.8036   0.01074   0.00379  -0.0844   0.1134   0.7146
   4.000   0.8314   0.01091   0.00395  -0.0845   0.1089   0.7177
   4.250   0.8590   0.01111   0.00413  -0.0845   0.1043   0.7208
   4.500   0.8865   0.01131   0.00430  -0.0845   0.1003   0.7237
   4.750   0.9142   0.01148   0.00448  -0.0845   0.0981   0.7264
   5.000   0.9416   0.01166   0.00467  -0.0845   0.0954   0.7293
   5.250   0.9686   0.01187   0.00488  -0.0845   0.0926   0.7323
   5.500   0.9955   0.01210   0.00509  -0.0844   0.0897   0.7354
   5.750   1.0224   0.01231   0.00532  -0.0843   0.0877   0.7386
   6.000   1.0495   0.01251   0.00553  -0.0842   0.0864   0.7416
   6.500   1.1026   0.01294   0.00600  -0.0839   0.0828   0.7474
   6.750   1.1288   0.01318   0.00625  -0.0837   0.0811   0.7507
   7.000   1.1546   0.01344   0.00652  -0.0835   0.0793   0.7541
   7.250   1.1801   0.01373   0.00682  -0.0831   0.0774   0.7574
   7.500   1.2058   0.01400   0.00711  -0.0829   0.0762   0.7602
   7.750   1.2316   0.01421   0.00737  -0.0826   0.0751   0.7632
   8.000   1.2571   0.01445   0.00765  -0.0823   0.0735   0.7667
   8.250   1.2820   0.01472   0.00794  -0.0819   0.0717   0.7705
   8.500   1.3066   0.01502   0.00825  -0.0815   0.0702   0.7741
   8.750   1.3308   0.01534   0.00858  -0.0810   0.0685   0.7772
   9.000   1.3542   0.01570   0.00896  -0.0804   0.0664   0.7807
   9.250   1.3783   0.01598   0.00930  -0.0798   0.0656   0.7844
   9.500   1.4021   0.01627   0.00963  -0.0793   0.0646   0.7885
   9.750   1.4254   0.01658   0.00998  -0.0787   0.0632   0.7923
  10.000   1.4481   0.01691   0.01035  -0.0779   0.0617   0.7962
  10.250   1.4700   0.01728   0.01074  -0.0771   0.0598   0.8004
  10.500   1.4912   0.01769   0.01117  -0.0761   0.0579   0.8046
  10.750   1.5118   0.01809   0.01161  -0.0751   0.0566   0.8086
  11.000   1.5323   0.01844   0.01203  -0.0740   0.0554   0.8131
  11.250   1.5515   0.01884   0.01247  -0.0727   0.0536   0.8183
  11.500   1.5673   0.01928   0.01294  -0.0709   0.0517   0.8236
  11.750   1.5835   0.01981   0.01350  -0.0692   0.0494   0.8289
  12.000   1.6006   0.02031   0.01406  -0.0676   0.0476   0.8347
  12.250   1.6170   0.02089   0.01467  -0.0661   0.0449   0.8404
  12.500   1.6316   0.02160   0.01539  -0.0645   0.0416   0.8467
  12.750   1.6470   0.02226   0.01610  -0.0629   0.0391   0.8540
  13.000   1.6601   0.02309   0.01697  -0.0612   0.0360   0.8621
  13.250   1.6733   0.02392   0.01784  -0.0595   0.0335   0.8719
  13.500   1.6846   0.02487   0.01885  -0.0577   0.0309   0.8837
  13.750   1.6962   0.02580   0.01985  -0.0559   0.0291   0.8989
  14.000   1.7060   0.02669   0.02086  -0.0539   0.0276   0.9266
  14.250   1.7126   0.02767   0.02193  -0.0514   0.0264   1.0000
  14.500   1.7229   0.02887   0.02318  -0.0499   0.0251   1.0000
  14.750   1.7341   0.03000   0.02437  -0.0486   0.0243   1.0000
  15.000   1.7439   0.03126   0.02569  -0.0472   0.0233   1.0000
  15.250   1.7522   0.03268   0.02715  -0.0458   0.0222   1.0000
  15.500   1.7589   0.03425   0.02878  -0.0444   0.0213   1.0000
  15.750   1.7664   0.03576   0.03037  -0.0431   0.0206   1.0000
  16.000   1.7733   0.03737   0.03206  -0.0419   0.0199   1.0000
  16.250   1.7786   0.03916   0.03392  -0.0408   0.0192   1.0000
  16.500   1.7820   0.04116   0.03599  -0.0396   0.0184   1.0000
  16.750   1.7835   0.04338   0.03829  -0.0385   0.0177   1.0000
  17.000   1.7853   0.04565   0.04063  -0.0377   0.0171   1.0000
  17.250   1.7867   0.04804   0.04311  -0.0369   0.0166   1.0000
  17.500   1.7862   0.05071   0.04588  -0.0364   0.0160   1.0000
  17.750   1.7833   0.05376   0.04902  -0.0360   0.0154   1.0000
  18.000   1.7785   0.05718   0.05253  -0.0359   0.0148   1.0000
  18.250   1.7721   0.06095   0.05640  -0.0361   0.0144   1.0000
  18.500   1.7653   0.06492   0.06049  -0.0366   0.0140   1.0000
  18.750   1.7567   0.06932   0.06501  -0.0375   0.0136   1.0000
  19.000   1.7450   0.07436   0.07019  -0.0388   0.0133   1.0000
  19.250   1.7295   0.08020   0.07617  -0.0408   0.0130   1.0000
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