Wind tunnel force and pressure tests of a 21% thick general aviation airfoil with 20% aileron, 25% slotted flap and 10% slot-lip spoiler

An edition of Wind tunnel force and pressure tests of a 21% thick general aviation airfoil with 20% aileron, 25% slotted flap and 10% slot-lip spoiler (1979)

Wind tunnel force and pressure tests of a 21% thick general aviation airfoil with 20% aileron, 25% slotted flap and 10% slot-lip spoiler

By W. H. Wentz

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Publish Date

1979

Publisher

Langley Research Center

Language

Pages

112

Description:

subjects: Pressure distribution, Wind tunnel tests, Force distribution