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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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(lwk79100-il) LWK 79-100

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LWK 79-100LWK 79-100 symmetrical airfoil
Max thickness 10% at 27.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(hq010-il) HQ 0/10 AIRFOIL

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HQ 0/10 AIRFOILQuabeck HQ 0/10 R/C sailplane airfoil
Max thickness 10% at 33.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(e230-il) E230 (9.96%)

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E230  (9.96%)Eppler E230 airfoil
Max thickness 10% at 29.3% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(sd8020-il) SD8020-010-88

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SD8020-010-88Selig/Donovan SD8020 low Reynolds number airfoil
Max thickness 10.1% at 27.5% chord
Max camber 0% at 42.1% chord
Source UIUC Airfoil Coordinates Database

(lwk80100-il) LWK 80-100

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LWK 80-100LWK 80-100 symmetrical airfoil
Max thickness 10.1% at 40.2% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(fx79l100-il) FX 79-L-100

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FX 79-L-100Wortmann FX 79-L-100 symmetrical airfoil
Max thickness 10.1% at 33.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(fx76100-il) WORTMANN FX 76-100

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WORTMANN FX 76-100Wortmann FX 76-100 symmetrical airfoil
Max thickness 10.1% at 27.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(n0011sc-il) NACA/LANGLEY SYMMETRICAL

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NACA/LANGLEY SYMMETRICALNASA/Langley 11% symmetrical supercritical airfoil
Max thickness 11% at 40% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(e297-il) EPPLER 297 AIRFOIL

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EPPLER 297 AIRFOILEppler E297 tailplane airfoil
Max thickness 11.4% at 37.7% chord
Max camber 0% at 0% 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
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