Effect of a wing leading-edge flap and chord-extension on the high subsonic control characteristics of an aileron located at two spanwise positions /
by Robert F. Thompson and Robert T. Taylor.

Description

Main Author

Thompson, Robert F.

Related Names

Taylor, Robert T.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, 1955.

Subjects

Ailerons > Ailerons / Performance.

Note

On front cover: "Classification Changed to Unclassified, Authority: NACA Research Abstract No. 119. Effective Date; August 16, 1957 WHL."
On front cover: "May 10, 1955."

Physical Description

59 pages : illustrations ; 27 cm.

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