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NASA/LANGLEY MS(1)-0317 AIRFOIL (ms317-il)

NASA/LANGLEY MS(1)-0317 AIRFOIL - NASA/Langley MS(1)-0317 general aviation airfoil


Airfoil ms317-il
Details Dat file Parser  
(ms317-il) NASA/LANGLEY MS(1)-0317 AIRFOIL
NASA/Langley MS(1)-0317 general aviation airfoil
Max thickness 17% at 37.5% chord.
Max camber 1.7% at 72.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 NASA/LANGLEY MS(1)-0317 AIRFOIL
45.        45.
 
 0.00000   0.00099
  .00200    .01248
  .00500    .01950
  .01250    .03099
  .02500    .04322
  .03750    .05210
  .05000    .05893
  .07500    .06840
  .10000    .07511
  .12500    .08033
  .15000    .08454
  .17500    .08805
  .20000    .09096
  .22500    .09339
  .25000    .09536
  .27500    .09694
  .30000    .09815
  .32500    .09901
  .35000    .09952
  .37500    .09972
  .40000    .09956
  .42500    .09909
  .45000    .09826
  .47500    .09700
  .50000    .09535
  .52500    .09323
  .55000    .09073
  .57500    .08777
  .60000    .08448
  .62500    .08079
  .65000    .07672
  .67500    .07232
  .70000    .06763
  .72500    .06269
  .75000    .05755
  .77500    .05225
  .80000    .04687
  .82500    .04132
  .85000    .03576
  .87500    .03013
  .90000    .02444
  .92500    .01873
  .95000    .01302
  .97500    .00720
 1.00000    .00125
 
 0.00000   0.00099
  .00200   -.00857
  .00500   -.01366
  .01250   -.02105
  .02500   -.02866
  .03750   -.03423
  .05000   -.03865
  .07500   -.04541
  .10000   -.05058
  .12500   -.05477
  .15000   -.05817
  .17500   -.06099
  .20000   -.06330
  .22500   -.06527
  .25000   -.06685
  .27500   -.06812
  .30000   -.06909
  .32500   -.06978
  .35000   -.07021
  .37500   -.07036
  .40000   -.07019
  .42500   -.06967
  .45000   -.06880
  .47500   -.06755
  .50000   -.06591
  .52500   -.06389
  .55000   -.06138
  .57500   -.05845
  .60000   -.05501
  .62500   -.05106
  .65000   -.04674
  .67500   -.04214
  .70000   -.03735
  .72500   -.03255
  .75000   -.02780
  .77500   -.02309
  .80000   -.01857
  .82500   -.01433
  .85000   -.01049
  .87500   -.00719
  .90000   -.00460
  .92500   -.00289
  .95000   -.00232
  .97500   -.00324
 1.00000   -.00597
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Lednicer format dat file
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Polars for NASA/LANGLEY MS(1)-0317 AIRFOIL (ms317-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   ms317-il50,000928.4 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ms317-il50,000524.2 at α=9.25°Mach=0 Ncrit=5Xfoil predictionDetails
   ms317-il100,000936.2 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ms317-il100,000535.5 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   ms317-il200,000948.5 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ms317-il200,000547.7 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   ms317-il500,000969.9 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ms317-il500,000564.6 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ms317-il1,000,000980.4 at α=1.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ms317-il1,000,000580.7 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
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