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Airfoil database list (A).

AH 79-K-132/20 to AH 93-K-131/15

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(ah79k132-il) AH 79-K-132/20

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AH 79-K-132/20Althaus AH 79-K-132/20 airfoil for use with flaps (K)
Max thickness 13.2% at 40.2% chord
Max camber 3.7% at 40.2% chord
Source UIUC Airfoil Coordinates Database

(ah79k135-il) AH 79-K-135/20 B

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AH 79-K-135/20 BAlthaus AH 79-K-135/20 airfoil for use with flaps (K)
Max thickness 13.5% at 40.2% chord
Max camber 3.1% at 40.2% chord
Source UIUC Airfoil Coordinates Database

(ah79k143-il) AH 79-K-143/18

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AH 79-K-143/18Althaus AH 79-K-143/18 airfoil for use with flaps (K)
Max thickness 14.3% at 40.2% chord
Max camber 2.9% at 40.2% chord
Source UIUC Airfoil Coordinates Database

(ah80129-il) AH 80-129

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AH 80-129Althaus AH 80-129 airfoil
Max thickness 12.9% at 40.2% chord
Max camber 4.1% at 43.5% chord
Source UIUC Airfoil Coordinates Database

(ah80136-il) AH 80-136

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AH 80-136Althaus AH 80-136 airfoil
Max thickness 13.5% at 33.9% chord
Max camber 3.4% at 33.9% chord
Source UIUC Airfoil Coordinates Database

(ah80140-il) AH 80-140

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AH 80-140Althaus AH 80-140 airfoil
Max thickness 14% at 30.9% chord
Max camber 4.4% at 33.9% chord
Source UIUC Airfoil Coordinates Database

(ah81131-il) AH 81-131

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AH 81-131Althaus AH 81-131 airfoil
Max thickness 13.1% at 40.2% chord
Max camber 2.8% at 40.2% chord
Source UIUC Airfoil Coordinates Database

(ah81k144-il) AH 81-K-144/17

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AH 81-K-144/17Althaus AH 81-K-144/17 airfoil for use with flaps (K)
Max thickness 14.5% at 40.2% chord
Max camber 4.2% at 46.7% chord
Source UIUC Airfoil Coordinates Database

(ah81k144wfklappe-il) AH 81-K-144 W-F KLAPPE

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AH 81-K-144 W-F KLAPPEAlthaus AH 81-K-144 W-F KLAPPE airfoil for use with flaps (K)
Max thickness 22% at 17% chord
Max camber 1.1% at 56.5% chord
Source UIUC Airfoil Coordinates Database

(ah82150a-il) AH 82-150 A

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AH 82-150 AAlthaus AH 82-150 A airfoil
Max thickness 15% at 40.2% chord
Max camber 3.3% at 43.5% chord
Source UIUC Airfoil Coordinates Database

(ah82150f-il) AH 82-150 F

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AH 82-150 FAlthaus AH 82-150 F airfoil
Max thickness 15% at 43.5% chord
Max camber 3.6% at 46.7% chord
Source UIUC Airfoil Coordinates Database

(ah83150q-il) AH 83-150 Q

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AH 83-150 QAlthaus AH 83-150 Q airfoil
Max thickness 15% at 40.2% chord
Max camber 4.1% at 37.1% chord
Source UIUC Airfoil Coordinates Database

(ah83159-il) AH 83-159

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AH 83-159Althaus AH 83-159 airfoil
Max thickness 15.9% at 40.2% chord
Max camber 3.8% at 40.2% chord
Source UIUC Airfoil Coordinates Database

(ah85l120-il) AH 85-L-120/17

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AH 85-L-120/17Althaus AH 85-L-120/17 symmetrical airfoil
Max thickness 12.1% at 43.5% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(ah88k130-il) AH 88-K-130/20

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AH 88-K-130/20Althaus AH 88-K-130/20 airfoil for use with flaps (K)
Max thickness 13% at 43.5% chord
Max camber 3.9% at 46.7% chord
Source UIUC Airfoil Coordinates Database

(ah88k136-il) AH 88-K-136/16

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AH 88-K-136/16Althaus AH 88-K-136/16 airfoil for use with flaps (K)
Max thickness 13.5% at 44.9% chord
Max camber 3% at 41.9% chord
Source UIUC Airfoil Coordinates Database

(ah93156-il) AH 93-156

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AH 93-156Althaus AH 93-156 airfoil
Max thickness 15.7% at 39.5% chord
Max camber 3.7% at 41.5% chord
Source UIUC Airfoil Coordinates Database

(ah93157-il) AH 93-157

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AH 93-157Althaus AH 93-157 airfoil
Max thickness 15.7% at 39.6% chord
Max camber 3.5% at 41.7% chord
Source UIUC Airfoil Coordinates Database

(ah93k130-il) AH 93-K-130/15

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AH 93-K-130/15Althaus AH 93-K-130/15 airfoil for use with flaps (K)
Max thickness 13.1% at 42% chord
Max camber 3.5% at 42% chord
Source UIUC Airfoil Coordinates Database

(ah93k131-il) AH 93-K-131/15

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AH 93-K-131/15Althaus AH 93-K-131/15 airfoil for use with flaps (K)
Max thickness 13.1% at 41.3% chord
Max camber 3.6% at 41.3% chord
Source UIUC Airfoil Coordinates Database
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