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Airfoil database search (Symmetrical)

Search the 1629 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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(ht05-il) HT05

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HT05Drela HT05 airfoil
Max thickness 4.8% at 17.1% chord
Max camber 0% at 63.3% chord
Source UIUC Airfoil Coordinates Database

(goe443-il) GOE 443 AIRFOIL

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GOE 443 AIRFOILGottingen 443 airfoil
Max thickness 5% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(ht08-il) HT08

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HT08Drela HT08 airfoil
Max thickness 5% at 20.2% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(ht12-il) HT12

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HT12Drela HT12 airfoil
Max thickness 5% at 18.6% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(goe444-il) GOE 444 AIRFOIL

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GOE 444 AIRFOILGottingen 444 airfoil
Max thickness 5.6% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(ea81006-il) EPPLER EA 8(-1)-006 AIRFOIL

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EPPLER EA 8(-1)-006 AIRFOILEppler EA 8(-1)-006 airfoil
Max thickness 6% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(naca0006-il) NACA 0006

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NACA 0006NACA 0006 airfoil
Max thickness 6% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(naca16006-il) NACA 16-006

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NACA 16-006NACA 16-006 airfoil
Max thickness 6% at 50% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(s1010-il) S1010 HPV airfoil

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S1010 HPV airfoilSelig S1010 HPV airfoil
Max thickness 6% at 23.3% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(m1-il) NACA-M1 AIRFOIL

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NACA-M1 AIRFOILNACA/Munk M-1 airfoil
Max thickness 6.2% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
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