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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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(e171-il) (Dicke 12.28%)

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(Dicke 12.28%)Eppler E171 low Reynolds number airfoil
Max thickness 12.3% at 32.4% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(e168-il) E168 (12.45%)

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E168  (12.45%)Eppler E168 low Reynolds number airfoil
Max thickness 12.4% at 26.7% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(e836-il) EPPLER E836 HYDROFOIL AIRFOIL

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EPPLER E836 HYDROFOIL AIRFOILEppler E836 hydrofoil
Max thickness 12.6% at 42.8% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(raf30-il) RAF 30 AIRFOIL

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RAF 30 AIRFOILRAF-30 airfoil
Max thickness 12.6% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(goe409-il) GOE 409 AIRFOIL

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GOE 409 AIRFOILGottingen 409 airfoil
Max thickness 12.7% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(goe459-il) GOE 459 AIRFOIL

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GOE 459 AIRFOILGottingen 459 airfoil
Max thickness 12.7% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(ultimate-il) ULTIMATE

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ULTIMATECarl Goldberg R/C Ultimate Bipe airfoil
Max thickness 12.8% at 34.2% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(ls013-il) NASA/LANGLEY LS(1)-0013 AIRFOIL

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NASA/LANGLEY LS(1)-0013 AIRFOILNASA/Langley LS(1)-0013 general aviation airfoil
Max thickness 12.9% at 40% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(goe411-il) GOE 411 AIRFOIL

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GOE 411 AIRFOILGottingen 411 airfoil
Max thickness 13.2% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(stcyr172-il) St. CYR 172 (Royer)

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St. CYR 172 (Royer)St. CYR 172 (Royer) airfoil
Max thickness 13.6% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
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