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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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(fxlv152-il) WORTMANN FX L V-152 AIRFOIL

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WORTMANN FX L V-152 AIRFOILWortmann FX L V-152 airfoil
Max thickness 15.3% at 33.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(e837-il) EPPLER E837 HYDROFOIL AIRFOIL

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EPPLER E837 HYDROFOIL AIRFOILEppler E837 hydrofoil
Max thickness 16.1% at 36.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(goe410-il) GOE 410 AIRFOIL

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GOE 410 AIRFOILGottingen 410 airfoil
Max thickness 16.1% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(e473-il) EPPLER 473 AIRFOIL

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EPPLER 473 AIRFOILEppler E473 aerobatic aircraft airfoil
Max thickness 16.2% at 21.2% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(s1014-il) S1014

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S1014Selig S1014 HPV airfoil
Max thickness 16.5% at 42.2% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(e479-il) EPPLER 479 AIRFOIL

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EPPLER 479 AIRFOILEppler E479 aerobatic aircraft airfoil
Max thickness 16.6% at 25.7% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(s1046-il) S1046 17% (Danny Howell)

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S1046 17% (Danny Howell)Selig S1046 airfoil
Max thickness 17% at 30.8% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(s1016-il) S1016

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S1016Selig S1016 HPV airfoil
Max thickness 17.5% at 41.8% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(naca16018-il) NACA 16-018

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NACA 16-018NACA 16-018 airfoil
Max thickness 18% at 50% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(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
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