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Airfoil database search (Symmetrical)

Search the 1636 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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(hq09-il) HQ 0/9 AIRFOIL

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HQ 0/9 AIRFOILQuabeck HQ 0/9 R/C sailplane airfoil
Max thickness 8.1% at 33.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(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

(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

(j5012-il) J5012 12%

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J5012   12%Jef Raskin (originator of the Apple Macintosh Project) J5012 airfoil
Max thickness 12% at 34.5% chord
Max camber 0% at 83.5% chord
Source UIUC Airfoil Coordinates Database

(joukowsk-il) 12% JOUKOWSKI AIRFOIL

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12% JOUKOWSKI AIRFOIL12% Joukowski airfoil
Max thickness 11.8% at 25% chord
Max camber 0% at 9.5% chord
Source UIUC Airfoil Coordinates Database

(joukowsk0009-jf) Joukovsky f=0% t=9%

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Joukovsky f=0% t=9%Joukowski 9% symmetrical airfoil
Max thickness 9% at 25.5% chord
Max camber 0% at 0% chord
Source Javafoil generated

(joukowsk0015-jf) Joukovsky f=0% t=15%

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Joukovsky f=0% t=15%Joukowski 15% symmetrical airfoil
Max thickness 15% at 24.6% chord
Max camber 0% at 0% chord
Source Javafoil generated

(joukowsk0018-jf) Joukovsky f=0% t=18%

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Joukovsky f=0% t=18%Joukowski 18% symmetrical airfoil
Max thickness 18% at 27.1% chord
Max camber 0% at 0% chord
Source Javafoil generated

(joukowsk0021-jf) Joukovsky f=0% t=21%

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Joukovsky f=0% t=21%Joukowski 21% symmetrical airfoil
Max thickness 21% at 26.6% chord
Max camber 0% at 0% chord
Source Javafoil generated
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