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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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(sc20012-il) NASA SC(2)-0012 AIRFOIL

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NASA SC(2)-0012 AIRFOILNASA SC(2)-0012 airfoil (NASA TP-2969)
Max thickness 12% at 37% 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

(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

(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

(us1000root-il) US1000ROOT

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US1000ROOTGreat Planes R/C Ultra-Sport 1000 airfoil
Max thickness 18.6% at 27.1% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(ys900-il) YS-900

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YS-900YS900 hyrdofoil (Shen / Eppler)
Max thickness 9% at 52.5% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
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