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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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(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

(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

(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

(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

(lwk80120k25-il) LWK 80-120/K25

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LWK 80-120/K25LWK 80-120/K25 symmetrical airfoil
Max thickness 12.1% at 40.2% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(lwk80150k25-il) LWK 80-150/K25

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LWK 80-150/K25LWK 80-150/K25 symmetrical airfoil
Max thickness 15% at 40.2% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(m1-il) NACA-M1 AIRFOIL

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NACA-M1 AIRFOILNACA/Munk M-1 airfoil
Max thickness 6.2% at 30% 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

(m3-il) NACA M3 AIRFOIL

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NACA M3 AIRFOILNACA/Munk M-3 airfoil
Max thickness 11.9% at 30% 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
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