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Airfoil database list (A).

AG35 to AH 79-100 C AIRFOIL

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(ag35-il) AG35

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AG35Drela AG35 airfoil
Max thickness 8.7% at 27.9% chord
Max camber 2.3% at 37% chord
Source UIUC Airfoil Coordinates Database

(ag36-il) AG36

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AG36Drela AG36 airfoil
Max thickness 8.2% at 27.9% chord
Max camber 2.3% at 37% chord
Source UIUC Airfoil Coordinates Database

(ag37-il) AG37

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AG37Drela AG37 airfoil
Max thickness 7.7% at 26.5% chord
Max camber 2.1% at 35.5% chord
Source UIUC Airfoil Coordinates Database

(ag38-il) AG38

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AG38Drela AG38 airfoil
Max thickness 7% at 27.7% chord
Max camber 2% at 36.7% chord
Source UIUC Airfoil Coordinates Database

(ag44ct02r-il) AG44ct -02f

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AG44ct -02fDrela AG44ct -02f airfoil
Max thickness 7.3% at 24.6% chord
Max camber 1.9% at 34.4% chord
Source UIUC Airfoil Coordinates Database

(ag455ct02r-il) AG455ct -02f rot.

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AG455ct -02f rot.Drela AG455ct -02f airfoil
Max thickness 6.5% at 23.3% chord
Max camber 1.8% at 33.1% chord
Source UIUC Airfoil Coordinates Database

(ag45c03-il) AG45c -03f

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AG45c -03fDrela AG45c -03f airfoil
Max thickness 6.9% at 23.5% chord
Max camber 2% at 31.7% chord
Source UIUC Airfoil Coordinates Database

(ag45ct02r-il) AG45ct -02f

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AG45ct -02fDrela AG45ct -02f airfoil
Max thickness 6.9% at 23.3% chord
Max camber 1.8% at 33.1% chord
Source UIUC Airfoil Coordinates Database

(ag46c03-il) AG46c -03f

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AG46c -03fDrela AG46c -03f airfoil
Max thickness 6% at 23.3% chord
Max camber 1.9% at 37.3% chord
Source UIUC Airfoil Coordinates Database

(ag46ct02r-il) AG46ct -02f rot.

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AG46ct  -02f rot.Drela AG46ct -02f airfoil
Max thickness 6.1% at 23.3% chord
Max camber 1.6% at 33% chord
Source UIUC Airfoil Coordinates Database

(ag47c03-il) AG47c -03f

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AG47c -03fDrela AG47c -03f airfoil
Max thickness 5.1% at 22.4% chord
Max camber 1.3% at 33.4% chord
Source UIUC Airfoil Coordinates Database

(ag47ct02r-il) AG47ct -02f rot.

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AG47ct  -02f rot.Drela AG47ct -02f airfoil
Max thickness 5% at 22.5% chord
Max camber 1.2% at 33.4% chord
Source UIUC Airfoil Coordinates Database

(ah21-7-il) AH21 7% version (Andrew Hollom)

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AH21 7% version (Andrew Hollom)Andrew Hollom AH 21 airfoil (7% version)
Max thickness 9% at 34.9% chord
Max camber 2.3% at 54.8% chord
Source UIUC Airfoil Coordinates Database

(ah21-9-il) AH21 9% version (Andrew Hollom)

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AH21 9% version (Andrew Hollom)Andrew Hollom AH 21 airfoil (original 9% version)
Max thickness 7% at 34.9% chord
Max camber 1.8% at 54.8% chord
Source UIUC Airfoil Coordinates Database

(ah63k127-il) AH 63-K-127/24

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AH 63-K-127/24Althaus AH 63-K-127/24 airfoil for use with flaps (K)
Max thickness 12.7% at 40.2% chord
Max camber 3.8% at 43.5% chord
Source UIUC Airfoil Coordinates Database

(ah6407-il) AH-6-40-7 AIRFOIL

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AH-6-40-7 AIRFOILAlthaus AH 6-407 airfoil
Max thickness 6.9% at 20% chord
Max camber 5.5% at 40% chord
Source UIUC Airfoil Coordinates Database

(ah7476-il) AH-7-47-6 AIRFOIL

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AH-7-47-6 AIRFOILAlthaus AH 7-476 airfoil
Max thickness 5.9% at 20% chord
Max camber 6.2% at 50% chord
Source UIUC Airfoil Coordinates Database

(ah79100a-il) AH 79-100 A AIRFOIL

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AH 79-100 A AIRFOILAlthaus AH 79-100A airfoil
Max thickness 10% at 27.9% chord
Max camber 3.6% at 56.5% chord
Source UIUC Airfoil Coordinates Database

(ah79100b-il) AH 79-100 B AIRFOIL

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AH 79-100 B AIRFOILAlthaus AH 79-100B airfoil
Max thickness 10% at 30.9% chord
Max camber 6.4% at 50% chord
Source UIUC Airfoil Coordinates Database

(ah79100c-il) AH 79-100 C AIRFOIL

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AH 79-100 C AIRFOILAlthaus AH 79-100C airfoil
Max thickness 9.9% at 30.9% chord
Max camber 6.7% at 50% chord
Source UIUC Airfoil Coordinates Database
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