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Airfoil database search

Search the 1638 airfoils available in the databases filtering by name, thickness and camber. Click on an airfoil image to display a larger preview picture. There are links to the original airfoil source and dat file and the details page with polar diagrams for a range of Reynolds numbers.

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(m17-il) NACA M17 AIRFOIL

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NACA M17 AIRFOILNACA/Munk M-17 airfoil
Max thickness 8.1% at 40% chord
Max camber 4.1% at 30% chord
Max Cl/Cd 74.2 at Re# 200,000
Source UIUC Airfoil Coordinates Database

(goe308-il) GOE 308 (MVA H.40) AIRFOIL

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GOE 308 (MVA H.40) AIRFOILGottingen 308 (MVA H.40) airfoil
Max thickness 8.1% at 29.9% chord
Max camber 5% at 29.9% chord
Max Cl/Cd 74.2 at Re# 200,000
Source UIUC Airfoil Coordinates Database

(mh18-il) MH 18 11.16%

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MH 18  11.16%Martin Hepperle MH 18 for F3D Pylon Racing
Max thickness 11.1% at 36.8% chord
Max camber 2.7% at 42.1% chord
Max Cl/Cd 74.2 at Re# 200,000
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
Max Cl/Cd 74.2 at Re# 200,000
Source UIUC Airfoil Coordinates Database

(goe324-il) GOE 324 (HANSA-BRANDENBURG) AIRFOIL

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GOE 324 (HANSA-BRANDENBURG) AIRFOILGottingen 324 (Hansa-Brandenburg) airfoil
Max thickness 13.1% at 29.8% chord
Max camber 5.9% at 29.8% chord
Max Cl/Cd 74.2 at Re# 200,000
Source UIUC Airfoil Coordinates Database

(goe142-il) GOE 142 (MVA H.19) AIRFOIL

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GOE 142 (MVA H.19) AIRFOILGottingen 142 (MVA H.19) airfoil
Max thickness 6.2% at 24.9% chord
Max camber 3.8% at 34.9% chord
Max Cl/Cd 74.2 at Re# 200,000
Source UIUC Airfoil Coordinates Database

(m13-il) NACA M13 AIRFOIL

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NACA M13 AIRFOILNACA/Munk M-13 airfoil
Max thickness 6.2% at 30% chord
Max camber 3.8% at 30% chord
Max Cl/Cd 74.1 at Re# 200,000
Source UIUC Airfoil Coordinates Database

(goe401-il) GOE 401 AIRFOIL

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GOE 401 AIRFOILGottingen 401 airfoil
Max thickness 7.1% at 29.9% chord
Max camber 4.9% at 29.9% chord
Max Cl/Cd 74.1 at Re# 200,000
Source UIUC Airfoil Coordinates Database

(e561-il) EPPLER 561 AIRFOIL

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EPPLER 561 AIRFOILEppler E561 general aviation airfoil
Max thickness 16.9% at 27.9% chord
Max camber 5.1% at 45.8% chord
Max Cl/Cd 74.1 at Re# 200,000
Source UIUC Airfoil Coordinates Database

(usa25-il) USA 25 AIRFOIL

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USA 25 AIRFOILUSA-25 airfoil
Max thickness 8.3% at 19.9% chord
Max camber 5.2% at 29.9% chord
Max Cl/Cd 74.1 at Re# 200,000
Source UIUC Airfoil Coordinates Database
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