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TH 25816 HALE AIRFOIL (th25816-il)

TH 25816 HALE AIRFOIL - Naval Air Development Center/Doug Hall high altitude


Airfoil th25816-il
Details Dat file Parser  
(th25816-il) TH 25816 HALE AIRFOIL
Naval Air Development Center/Doug Hall high altitude
Max thickness 25.7% at 48.3% chord.
Max camber 4% at 52.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
TH 25816 HALE AIRFOIL
       33.       29.

  0.000010 -0.000740
  0.002750  0.011590
  0.010080  0.025520
  0.021730  0.040160
  0.037800  0.054880
  0.058370  0.069480
  0.083180  0.083880
  0.111890  0.097850
  0.144150  0.111140
  0.179630  0.123520
  0.217930  0.134760
  0.258650  0.144680
  0.301370  0.153090
  0.345630  0.159820
  0.390970  0.164730
  0.436900  0.167650
  0.482910  0.168380
  0.528670  0.166630
  0.574070  0.162320
  0.618900  0.155590
  0.662880  0.146610
  0.705870  0.135610
  0.747610  0.123140
  0.787540  0.109780
  0.824940  0.095910
  0.859000  0.081630
  0.889310  0.066520
  0.916380  0.050420
  0.940920  0.034190
  0.963070  0.019490
  0.981880  0.008260
  0.995120  0.001880
  1.000000  0.000000

  0.000010 -0.000740
  0.003550 -0.010760
  0.014230 -0.019690
  0.031030 -0.028760
  0.053260 -0.037740
  0.080440 -0.046450
  0.112140 -0.054710
  0.147910 -0.062390
  0.187300 -0.069360
  0.229810 -0.075480
  0.274900 -0.080640
  0.322030 -0.084720
  0.370630 -0.087580
  0.420110 -0.089100
  0.469860 -0.089060
  0.519410 -0.087140
  0.568570 -0.083110
  0.617240 -0.077050
  0.665200 -0.069250
  0.712070 -0.060130
  0.757220 -0.049950
  0.800320 -0.038620
  0.841700 -0.026450
  0.881490 -0.014670
  0.919160 -0.005020
  0.952730  0.000520
  0.978740  0.001710
  0.994690  0.000710
  1.000000  0.000000
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Lednicer format dat file
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Polars for TH 25816 HALE AIRFOIL (th25816-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   th25816-il50,00092.4 at α=13.75°Mach=0 Ncrit=9Xfoil predictionDetails
   th25816-il50,00057.1 at α=19°Mach=0 Ncrit=5Xfoil predictionDetails
   th25816-il100,000915.1 at α=17.5°Mach=0 Ncrit=9Xfoil predictionDetails
   th25816-il100,000512.2 at α=16°Mach=0 Ncrit=5Xfoil predictionDetails
   th25816-il200,000921.5 at α=14.75°Mach=0 Ncrit=9Xfoil predictionDetails
   th25816-il200,000519.1 at α=13.5°Mach=0 Ncrit=5Xfoil predictionDetails
   th25816-il500,000954.7 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   th25816-il500,000547.9 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   th25816-il1,000,000974.9 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   th25816-il1,000,000559.6 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
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