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NASA/LANGLEY MS(1)-0313 AIRFOIL (ms313-il)

NASA/LANGLEY MS(1)-0313 AIRFOIL - NASA/Langley MS(1)-0313 general aviation airfoil (buggy


Airfoil ms313-il
Details Dat file Parser  
(ms313-il) NASA/LANGLEY MS(1)-0313 AIRFOIL
NASA/Langley MS(1)-0313 general aviation airfoil (buggy
Max thickness 13.1% at 37.5% chord.
Max camber 1.8% at 67.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 
 NASA/LANGLEY MS(1)-0313 AIRFOIL
45.        45.
 
 0.00000   0.000986
  .00200    .009475
  .00500    .015120
  .01250    .024286
  .02500    .034450
  .03750    .041872
  .05000    .047433
  .07500    .055169
  .10000    .060608
  .12500    .064805
  .15000    .068189
  .17500    .070963
  .20000    .073274
  .22500    .075199
  .25000    .076777
  .27500    .078033
  .30000    .078991
  .32500    .079678
  .35000    .080119
  .37500    .080324
  .40000    .080293
  .42500    .080026
  .45000    .079517
  .47500    .078763
  .50000    .077753
  .52500    .076464
  .55000    .074868
  .57500    .072934
  .60000    .070636
  .62500    .067958
  .65000    .064903
  .67500    .061488
  .70000    .057745
  .72500    .053710
  .75000    .049418
  .77500    .044899
  .80000    .040179
  .82500    .035288
  .85000    .030259
  .87500    .025177
  .90000    .020079
  .92500    .014950
  .95000    .009822
  .97500    .004699
 1.00000   -.000471
 
 0.00000   0.000986
  .00200   -.006272
  .00500   -.009977
  .01250   -.015246
  .02500   -.020594
  .03750   -.024404
  .05000   -.027454
  .07500   -.032278
  .10000   -.036076
  .12500   -.039204
  .15000   -.041819
  .17500   -.044001
  .20000   -.045806
  .22500   -.047282
  .25000   -.048471
  .27500   -.049410
  .30000   -.050129
  .32500   -.050645
  .35000   -.050960
  .37500   -.051059
  .40000   -.050919
  .42500   -.050512
  .45000   -.049814
  .47500   -.048812
  .50000   -.047511
  .52500   -.045918
  .55000   -.044024
  .57500   -.041812
  .60000   -.039274
  .62500   -.036426
  .65000   -.033315
  .67500   -.030007
  .70000   -.026571
  .72500   -.023071
  .75000   -.019568
  .77500   -.016140
  .80000   -.012881
  .82500   -.009897
  .85000   -.007286
  .87500   -.005135
  .90000   -.003535
  .92500   -.002607
  .95000   -.002523
  .97500   -.003540
 1.00000   -.006054
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Polars for NASA/LANGLEY MS(1)-0313 AIRFOIL (ms313-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   ms313-il50,000931.6 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   ms313-il50,000529.8 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ms313-il100,000946.4 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ms313-il100,000539.5 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ms313-il200,000955.5 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ms313-il200,000550.5 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
   ms313-il500,000974.4 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ms313-il500,000569.8 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ms313-il1,000,000985.3 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ms313-il1,000,000587.1 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
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