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NASA/LANGLEY LS(1)-0417 (GA(W)-1) AIRFOIL (ls417-il)

NASA/LANGLEY LS(1)-0417 (GA(W)-1) AIRFOIL - NASA/Langley/Whitcomb LS(1)-0417 (GA(W)-1) general aviation airfoil


Airfoil ls417-il
Details Dat file Parser  
(ls417-il) NASA/LANGLEY LS(1)-0417 (GA(W)-1) AIRFOIL
NASA/Langley/Whitcomb LS(1)-0417 (GA(W)-1) general aviation airfoil
Max thickness 17% at 40% chord.
Max camber 2.4% at 65% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 NASA/LANGLEY LS(1)-0417 (GA(W)-1) AIRFOIL
38.        38.
 
 0.00000   0.00000
  .00200    .01300
  .00500    .02035
  .01250    .03069
  .02500    .04165
  .03750    .04974
  .05000    .05600
  .07500    .06561
  .10000    .07309
  .12500    .07909
  .15000    .08413
  .17500    .08848
  .20000    .09209
  .25000    .09778
  .30000    .10169
  .35000    .10409
  .40000    .10500
  .45000    .10456
  .50000    .10269
  .55000    .09917
  .57500    .09674
  .60000    .09374
  .62500    .09013
  .65000    .08604
  .67500    .08144
  .70000    .07639
  .72500    .07096
  .75000    .06517
  .77500    .05913
  .80000    .05291
  .82500    .04644
  .85000    .03983
  .87500    .03313
  .90000    .02639
  .92500    .01965
  .95000    .01287
  .97500    .00604
 1.00000   -.00074
 
 0.00000   0.00000
  .00200   -.00974
  .00500   -.01444
  .01250   -.02052
  .02500   -.02691
  .03750   -.03191
  .05000   -.03569
  .07500   -.04209
  .10000   -.04700
  .12500   -.05087
  .15000   -.05426
  .17500   -.05700
  .20000   -.05926
  .25000   -.06265
  .30000   -.06448
  .35000   -.06517
  .40000   -.06483
  .45000   -.06344
  .50000   -.06091
  .55000   -.05683
  .57500   -.05396
  .60000   -.05061
  .62500   -.04678
  .65000   -.04265
  .67500   -.03830
  .70000   -.03383
  .72500   -.02930
  .75000   -.02461
  .77500   -.02030
  .80000   -.01587
  .82500   -.01191
  .85000   -.00852
  .87500   -.00565
  .90000   -.00352
  .92500   -.00248
  .95000   -.00257
  .97500   -.00396
 1.00000   -.00783
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Lednicer format dat file
Selig format dat file

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Polars for NASA/LANGLEY LS(1)-0417 (GA(W)-1) AIRFOIL (ls417-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   ls417-il50,000929.7 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   ls417-il50,000525 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ls417-il100,000942.9 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ls417-il100,000541 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ls417-il200,000961 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ls417-il200,000561.7 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ls417-il500,000992.9 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ls417-il500,000582.1 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
   ls417-il1,000,0009112.6 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ls417-il1,000,000591.3 at α=1°Mach=0 Ncrit=5Xfoil predictionDetails
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