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ARA-D 6% AIRFOIL (arad6-il)

ARA-D 6% AIRFOIL - Aeronautical Research Association/Bocci-Dowty Rotol ARA-D 6% thick propeller airfoil


Airfoil arad6-il
Details Dat file Parser  
(arad6-il) ARA-D 6% AIRFOIL
Aeronautical Research Association/Bocci-Dowty Rotol ARA-D 6% thick propeller airfoil
Max thickness 6% at 20% chord.
Max camber 5% at 45% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 ARA-D 6% AIRFOIL
26.        26.
 
 0.00000   0.00000
  .00300    .009099
  .01000    .017152
  .02000    .024678
  .04000    .035135
  .07000    .045809
  .10000    .053377
  .15000    .062118
  .20000    .068235
  .25000    .072750
  .30000    .076067
  .35000    .078178
  .40000    .079022
  .45000    .078668
  .50000    .077173
  .55000    .074566
  .60000    .070912
  .65000    .066260
  .70000    .060628
  .75000    .054022
  .80000    .046416
  .85000    .037752
  .90000    .028002
  .95000    .017193
  .97500    .011484
 1.00000    .005500
 
 0.00000   0.00000
  .00300   -.004658
  .01000   -.007411
  .02000   -.008934
  .04000   -.009318
  .07000   -.007339
  .10000   -.004076
  .15000    .002198
  .20000    .007996
  .25000    .012750
  .30000    .016295
  .35000    .018834
  .40000    .020553
  .45000    .021539
  .50000    .021827
  .55000    .021435
  .60000    .020401
  .65000    .018750
  .70000    .016501
  .75000    .013723
  .80000    .010504
  .85000    .006940
  .90000    .003084
  .95000   -.001015
  .97500   -.003184
 1.00000   -.005500
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Lednicer format dat file
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Polars for ARA-D 6% AIRFOIL (arad6-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   arad6-il50,000946 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   arad6-il50,000545.8 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   arad6-il100,000968.9 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   arad6-il100,000566.6 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   arad6-il200,000993 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   arad6-il200,000586 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   arad6-il500,0009122.5 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   arad6-il500,0005105.6 at α=1.75°Mach=0 Ncrit=5Xfoil predictionDetails
   arad6-il1,000,0009139.7 at α=2°Mach=0 Ncrit=9Xfoil predictionDetails
   arad6-il1,000,0005106 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
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