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WHITCOMB INTEGRAL SUPERCRITICAL AIRFOIL (whitcomb-il)

WHITCOMB INTEGRAL SUPERCRITICAL AIRFOIL - NASA/Langley Whitcomb integral supercritical airfoil


Airfoil whitcomb-il
Details Dat file Parser  
(whitcomb-il) WHITCOMB INTEGRAL SUPERCRITICAL AIRFOIL
NASA/Langley Whitcomb integral supercritical airfoil
Max thickness 11% at 35% chord.
Max camber 2.4% at 82.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 WHITCOMB INTEGRAL SUPERCRITICAL AIRFOIL
 37.        37.
 
 0.0      0.0
  .0075    .0176
  .0125    .0215
  .0250    .0276
  .0375    .0316
  .0500    .0347
  .0750    .0394
  .1000    .0428
  .1250    .0455
  .1500    .0476
  .1750    .0493
  .2000    .0507
  .2500    .0528
  .3000    .0540
  .3500    .0547
  .4000    .0550
  .4500    .0548
  .5000    .0543
  .5500    .0533
  .5750    .0527
  .6000    .0519
  .6250    .0511
  .6500    .0501
  .6750    .0489
  .7000    .0476
  .7250    .0460
  .7500    .0442
  .7750    .0422
  .8000    .0398
  .8250    .0370
  .8500    .0337
  .8750    .0300
  .9000    .0255
  .9250    .0204
  .9500    .0144
  .9750    .0074
 1.0000   -.0008
 
 0.0      0.0
  .0075   -.0176
  .0125   -.0216
  .0250   -.0281
  .0375   -.0324
  .0500   -.0358
  .0750   -.0408
  .1000   -.0444
  .1250   -.0472
  .1500   -.0493
  .1750   -.0510
  .2000   -.0522
  .2500   -.0540
  .3000   -.0548
  .3500   -.0549
  .4000   -.0541
  .4500   -.0524
  .5000   -.0497
  .5500   -.0455
  .5750   -.0426
  .6000   -.0389
  .6250   -.0342
  .6500   -.0282
  .6750   -.0215
  .7000   -.0149
  .7250   -.0090
  .7500   -.0036
  .7750    .0012
  .8000    .0053
  .8250    .0088
  .8500    .0114
  .8750    .0132
  .9000    .0138
  .9250    .0131
  .9500    .0106
  .9750    .0060
 1.0000   -.0013
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Lednicer format dat file
Selig format dat file

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Polars for WHITCOMB INTEGRAL SUPERCRITICAL AIRFOIL (whitcomb-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   whitcomb-il50,000922.1 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   whitcomb-il50,000519.9 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   whitcomb-il100,000922.9 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   whitcomb-il100,000527.8 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   whitcomb-il200,000930.1 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   whitcomb-il200,000539.2 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   whitcomb-il500,000949.1 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   whitcomb-il500,000559.6 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   whitcomb-il1,000,000969 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   whitcomb-il1,000,000576.9 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
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