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AQUILA 9.3% smoothed (aquilasm-il)

AQUILA 9.3% smoothed - AQUILA R/C sailplane airfoil


Airfoil aquilasm-il
Details Dat file Parser  
(aquilasm-il) AQUILA 9.3% smoothed
AQUILA R/C sailplane airfoil
Max thickness 9.4% at 31.3% chord.
Max camber 4% at 34.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
  AQUILA 9.3% smoothed
  1.00000   0.0
  0.99667   0.00057
  0.99333   0.00114
  0.99000   0.00171
  0.98667   0.00228
  0.98000   0.00340
  0.92667   0.01240
  0.87333   0.02150
  0.82000   0.03065
  0.76000   0.04077
  0.70667   0.04945
  0.65333   0.05768
  0.60000   0.06530
  0.54667   0.07214
  0.49333   0.07799
  0.44000   0.08263
  0.39333   0.08551
  0.34667   0.08710
  0.31333   0.08735
  0.27333   0.08655
  0.23333   0.08438
  0.19333   0.08055
  0.16000   0.07577
  0.12667   0.06914
  0.09333   0.06012
  0.06000   0.04786
  0.04667   0.04171
  0.03333   0.03454
  0.02667   0.03045
  0.02000   0.02587
  0.01333   0.02052
  0.01000   0.01739
  0.00667   0.01377
  0.00333   0.00929
  0.0       0.0
  0.00333  -0.00572
  0.00667  -0.00725
  0.01000  -0.00810
  0.01333  -0.00862
  0.02000  -0.00917
  0.02667  -0.00940
  0.03333  -0.00947
  0.04667  -0.00939
  0.06000  -0.00920
  0.09333  -0.00866
  0.12667  -0.00821
  0.16000  -0.00787
  0.19333  -0.00758
  0.23333  -0.00724
  0.27333  -0.00688
  0.31333  -0.00650
  0.34667  -0.00618
  0.39333  -0.00574
  0.44000  -0.00530
  0.49333  -0.00480
  0.54667  -0.00430
  0.60000  -0.00380
  0.65333  -0.00330
  0.70667  -0.00279
  0.76000  -0.00229
  0.82000  -0.00173
  0.87333  -0.00122
  0.92667  -0.00070
  0.98000  -0.00019
  0.98667  -0.00013
  0.99000  -0.00009
  0.99333  -0.00006
  0.99667  -0.00003
  1.00000   0.0
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Polars for AQUILA 9.3% smoothed (aquilasm-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   aquilasm-il50,000925.3 at α=11.75°Mach=0 Ncrit=9Xfoil predictionDetails
   aquilasm-il50,000537 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   aquilasm-il100,000951.6 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   aquilasm-il100,000556.4 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   aquilasm-il200,000974.7 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   aquilasm-il200,000575 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   aquilasm-il500,0009104.8 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   aquilasm-il500,000599.6 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   aquilasm-il1,000,0009127.1 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   aquilasm-il1,000,0005118.5 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
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