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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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(goe445-il) GOE 445 AIRFOIL

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GOE 445 AIRFOILGottingen 445 airfoil
Max thickness 6.4% at 40% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(hq07-il) HQ 0/7 AIRFOIL

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HQ 0/7 AIRFOILQuabeck HQ 0/7 R/C sailplane airfoil
Max thickness 7% at 33.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(s9033-il) S9033 (7.5%)

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S9033 (7.5%)Selig S9033 (7.5%) symmetrical vertical stab airfoil used on the Blackhawk R/C sailplane
Max thickness 7.5% at 22.8% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(raf30md-il) RAF 30 MOD AIRFOIL

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RAF 30 MOD AIRFOILRAF-30 MOD airfoil
Max thickness 7.6% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(naca000834-il) NACA 0008-34

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NACA 0008-34NACA 0008-34 airfoil
Max thickness 8% at 40% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(fx77080-il) WORTMANN FX 77-080

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WORTMANN FX 77-080Wortmann FX 77-080 symmetrical airfoil
Max thickness 8% at 27.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(s9027-il) S9027 (8%)

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S9027 (8%)Selig S9027 (8%) symmetrical vertical stab airfoil used on the Opus R/C sailplane
Max thickness 8% at 22.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(naca0008-il) NACA 0008

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NACA 0008NACA 0008 airfoil
Max thickness 8% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(n64008a-il) NACA 64-008A AIRFOIL

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NACA 64-008A AIRFOILNACA 64-008A airfoil
Max thickness 8% at 40% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(m2-il) NACA M2 AIRFOIL

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NACA M2 AIRFOILNACA/Munk M-2 airfoil
Max thickness 8% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
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