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Airfoil database list (A).

ARA-D 20% AIRFOIL to AVISTAR

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(arad20-il) ARA-D 20% AIRFOIL

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ARA-D 20% AIRFOILAeronautical Research Association/Bocci-Dowty Rotol ARA-D 20% thick propeller airfoil
Max thickness 20% at 25% chord
Max camber 3.8% at 25% chord
Source UIUC Airfoil Coordinates Database

(arad6-il) ARA-D 6% AIRFOIL

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ARA-D 6% AIRFOILAeronautical 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

(as5045-il) AS5045 (15%)

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AS5045 (15%)AS5045 airfoil Ashok Gopalarathnam/Selig 15% airfoil
Max thickness 15% at 37.5% chord
Max camber 1% at 27.2% chord
Source UIUC Airfoil Coordinates Database

(as5046-il) AS5046 (16%)

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AS5046 (16%)AS5046 airfoil Ashok Gopalarathnam/Selig 16% airfoil
Max thickness 16% at 37.6% chord
Max camber 0.7% at 77.4% chord
Source UIUC Airfoil Coordinates Database

(as5048-il) AS5048 (18%)

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AS5048 (18%)AS5048 airfoil Ashok Gopalarathnam/Selig 18% airfoil
Max thickness 18% at 38.3% chord
Max camber 0.8% at 77.8% chord
Source UIUC Airfoil Coordinates Database

(atr72sm-il) Smoothed ATR airfoil coordinates obtained using AFSMO (Harry Morgan's NASA smoothing program)

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Smoothed ATR airfoil coordinates obtained  using AFSMO (Harry Morgan's NASA smoothing program)ATR 72 wing airfoil (from NTSB report)
Max thickness 14.5% at 25.4% chord
Max camber 2.9% at 21.4% chord
Source UIUC Airfoil Coordinates Database

(august160-il) AUGUST 160

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AUGUST 160AUGUST 160 airfoil
Max thickness 16% at 25% chord
Max camber 5.4% at 25% chord
Source UIUC Airfoil Coordinates Database

(avistar-il) AVISTAR

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AVISTARHobbico R/C Avistar trainer airfoil
Max thickness 14.5% at 34.2% chord
Max camber 2.3% at 37.9% chord
Source UIUC Airfoil Coordinates Database
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