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Airfoil database list (A).

AH 93-K-132/15 to ARA-D 13% AIRFOIL

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(ah93k132-il) AH 93-K-132/15

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AH 93-K-132/15Althaus AH 93-K-132/15 airfoil for use with flaps (K)
Max thickness 13.2% at 41.2% chord
Max camber 3.5% at 41.2% chord
Source UIUC Airfoil Coordinates Database

(ah93w145-il) AH 93-W-145

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AH 93-W-145Althaus AH 93-W-145 airfoil for use on wind turbines (W)
Max thickness 14.5% at 33.9% chord
Max camber 3.9% at 37.1% chord
Source UIUC Airfoil Coordinates Database

(ah93w174-il) AH 93-W-174

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AH 93-W-174Althaus AH 93-W-174 airfoil for use on wind turbines (W)
Max thickness 17.4% at 33.9% chord
Max camber 3.9% at 37.1% chord
Source UIUC Airfoil Coordinates Database

(ah93w215-il) AH 93-W-215

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AH 93-W-215Althaus AH 93-W-215 airfoil for use on wind turbines (W)
Max thickness 21.2% at 33.9% chord
Max camber 3.1% at 40.2% chord
Source UIUC Airfoil Coordinates Database

(ah93w257-il) AH 93-W-257

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AH 93-W-257Althaus AH 93-W-257 airfoil for use on wind turbines (W)
Max thickness 25.7% at 30.9% chord
Max camber 2.1% at 77.8% chord
Source UIUC Airfoil Coordinates Database

(ah93w300-il) AH 93-W-300

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AH 93-W-300Althaus AH 93-W-300 airfoil for use on wind turbines (W)
Max thickness 30% at 27.9% chord
Max camber 1.6% at 72.1% chord
Source UIUC Airfoil Coordinates Database

(ah93w480b-il) AH 93-W-480B

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AH 93-W-480BAlthaus AH 93-W-480B airfoil for use on wind turbines (W)
Max thickness 47.8% at 44.1% chord
Max camber 3.6% at 44.1% chord
Source UIUC Airfoil Coordinates Database

(ah94145-il) AH 94-145

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AH 94-145Althaus AH 94-145 airfoil
Max thickness 14.6% at 38.9% chord
Max camber 5.6% at 44.6% chord
Source UIUC Airfoil Coordinates Database

(ah94156-il) AH 94-156

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AH 94-156Althaus AH 94-156 airfoil
Max thickness 15.6% at 39.6% chord
Max camber 3.6% at 41.5% chord
Source UIUC Airfoil Coordinates Database

(ah94w301-il) AH 94-W-301

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AH 94-W-301Althaus AH 94-W-301 airfoil for use on wind turbines (W)
Max thickness 30.1% at 30.9% chord
Max camber 1.3% at 80.4% chord
Source UIUC Airfoil Coordinates Database

(ah95160-il) AH 95-160

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AH 95-160Althaus AH 95-160 airfoil
Max thickness 16% at 38.9% chord
Max camber 5.6% at 44.6% chord
Source UIUC Airfoil Coordinates Database

(ames01-il) NASA/AMES A-01 AIRFOIL

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NASA/AMES A-01 AIRFOILNASA/AMES/Hicks A-01 transonic rotorcraft airfoil
Max thickness 10.3% at 35% chord
Max camber 1.4% at 15% chord
Source UIUC Airfoil Coordinates Database

(ames02-il) NASA/AMES A-02 AIRFOIL

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NASA/AMES A-02 AIRFOILNASA/AMES/Hicks A-02 transonic rotorcraft airfoil
Max thickness 7.7% at 30% chord
Max camber 0.5% at 12.5% chord
Source UIUC Airfoil Coordinates Database

(ames03-il) NASA/AMES A-03 AIRFOIL

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NASA/AMES A-03 AIRFOILNASA/AMES/Kennelly A-03 transonic rotorcraft airfoil
Max thickness 10% at 37.5% chord
Max camber 1.2% at 17.5% chord
Source UIUC Airfoil Coordinates Database

(amsoil1-il) RUTAN CANARD AIRFOIL

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RUTAN CANARD AIRFOILRutan AMSOIL racer canard airfoil
Max thickness 11.6% at 39% chord
Max camber 2.1% at 42% chord
Source UIUC Airfoil Coordinates Database

(amsoil2-il) RUTAN WING AIRFOIL

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RUTAN WING AIRFOILRutan AMSOIL racer wing airfoil
Max thickness 11.8% at 39% chord
Max camber 1% at 48% chord
Source UIUC Airfoil Coordinates Database

(apex16-il) Apex 16 (normalized using XFOIL date021206)

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Apex 16 (normalized using XFOIL date021206)Drela Apex 16 low Reynolds number transonic research airfoil
Max thickness 12.9% at 38.6% chord
Max camber 2.4% at 59.6% chord
Source UIUC Airfoil Coordinates Database

(aquilasm-il) AQUILA 9.3% smoothed

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AQUILA 9.3% smoothedAQUILA R/C sailplane airfoil
Max thickness 9.4% at 31.3% chord
Max camber 4% at 34.7% chord
Source UIUC Airfoil Coordinates Database

(arad10-il) ARA-D 10% AIRFOIL

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ARA-D 10% AIRFOILAeronautical Research Association/Bocci-Dowty Rotol ARA-D 10% thick propeller airfoil
Max thickness 10% at 25% chord
Max camber 4% at 35% chord
Source UIUC Airfoil Coordinates Database

(arad13-il) ARA-D 13% AIRFOIL

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ARA-D 13% AIRFOILAeronautical Research Association/Bocci-Dowty Rotol ARA-D 13% thick propeller airfoil
Max thickness 13% at 25% chord
Max camber 3.6% at 30% chord
Source UIUC Airfoil Coordinates Database
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