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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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(ch10sm-il) CH10 (smoothed)

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CH10 (smoothed)Chuch Hollinger CH 10-48-13 high lift low Reynolds number airfoil
Max thickness 12.8% at 30.6% chord
Max camber 10.2% at 49.3% chord
Max Cl/Cd 135.4 at Re# 500,000
Source UIUC Airfoil Coordinates Database

(ch10sm-il) CH10 (smoothed)

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CH10 (smoothed)Chuch Hollinger CH 10-48-13 high lift low Reynolds number airfoil
Max thickness 12.8% at 30.6% chord
Max camber 10.2% at 49.3% chord
Max Cl/Cd 132.4 at Re# 500,000
Source UIUC Airfoil Coordinates Database

(fx72ls160-il) FX 72-LS-160

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FX 72-LS-160Wortmann FX 72-LS-160 airfoil
Max thickness 16% at 37.1% chord
Max camber 8.2% at 43.5% chord
Max Cl/Cd 125.7 at Re# 500,000
Source UIUC Airfoil Coordinates Database

(e423-il) E423

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E423Eppler E423 high lift airfoil
Max thickness 12.5% at 23.7% chord
Max camber 9.5% at 41.4% chord
Max Cl/Cd 123.4 at Re# 500,000
Source UIUC Airfoil Coordinates Database

(fx72150a-il) WORTMANN FX 72-MS-150A AIRFOIL

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WORTMANN FX 72-MS-150A AIRFOILWortmann FX 72-MS-150A airfoil
Max thickness 15% at 37.1% chord
Max camber 8.3% at 46.7% chord
Max Cl/Cd 123.1 at Re# 500,000
Source UIUC Airfoil Coordinates Database

(fx72ls160-il) FX 72-LS-160

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FX 72-LS-160Wortmann FX 72-LS-160 airfoil
Max thickness 16% at 37.1% chord
Max camber 8.2% at 43.5% chord
Max Cl/Cd 121.2 at Re# 500,000
Source UIUC Airfoil Coordinates Database

(fx72150a-il) WORTMANN FX 72-MS-150A AIRFOIL

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WORTMANN FX 72-MS-150A AIRFOILWortmann FX 72-MS-150A airfoil
Max thickness 15% at 37.1% chord
Max camber 8.3% at 46.7% chord
Max Cl/Cd 121.1 at Re# 500,000
Source UIUC Airfoil Coordinates Database

(e423-il) E423

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E423Eppler E423 high lift airfoil
Max thickness 12.5% at 23.7% chord
Max camber 9.5% at 41.4% chord
Max Cl/Cd 120.6 at Re# 500,000
Source UIUC Airfoil Coordinates Database

(fx74modsm-il) FX 74-Cl5-140 MOD (smoothed)

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FX 74-Cl5-140 MOD  (smoothed)Modified Wortmann FX 74-CL5-140 high lift airfoil
Max thickness 13.1% at 27.1% chord
Max camber 9.7% at 41.6% chord
Max Cl/Cd 119.7 at Re# 500,000
Source UIUC Airfoil Coordinates Database

(goe448-il) GOE 448 AIRFOIL

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GOE 448 AIRFOILGottingen 448 airfoil
Max thickness 12.9% at 29.8% chord
Max camber 10.5% at 39.8% chord
Max Cl/Cd 119.3 at Re# 500,000
Source UIUC Airfoil Coordinates Database
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