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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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(hq09-il) HQ 0/9 AIRFOIL

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HQ 0/9 AIRFOILQuabeck HQ 0/9 R/C sailplane airfoil
Max thickness 8.1% at 33.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(nacam2-il) NACA M2

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NACA M2NACA M2 airfoil
Max thickness 8.1% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(lwk80080-il) LWK 80-080

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LWK 80-080LWK 80-080 symmetrical airfoil
Max thickness 8.1% at 40.2% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(fx71089a-il) WORTMANN FX 71-089A AIRFOIL

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WORTMANN FX 71-089A AIRFOILWortmann FX 71-089A airfoil
Max thickness 8.9% at 22.2% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(n0009sm-il) NACA-0009 9.0% smoothed

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NACA-0009 9.0% smoothedNACA 0009 airfoil (smoothed)
Max thickness 9% at 30.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(joukowsk0009-jf) Joukovsky f=0% t=9%

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Joukovsky f=0% t=9%Joukowski 9% symmetrical airfoil
Max thickness 9% at 25.5% chord
Max camber 0% at 0% chord
Source Javafoil generated

(ea61009-il) EPPLER EA 6(-1)-009 AIRFOIL

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EPPLER EA 6(-1)-009 AIRFOILEppler EA 6(-1)-009 airfoil
Max thickness 9% at 30% 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

(naca16009-il) NACA 16009

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NACA 16009NACA 16009 airfoil
Max thickness 9% at 50% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(s9032-il) S9032 (9%)

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S9032 (9%)Selig S9032 (9%) symmetrical horizontal stab airfoil used on the Blackhawk R/C sailplane
Max thickness 9% at 25% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
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