Effect of a wing leading-edge flap and chord-extension on the high subsonic control characteristics of an aileron located at two spanwise positions

Author: Thompson, Robert F.
Additional Authors: Taylor, Robert T.
Year: 1955
Document Type: MAIN
SUDOC: Y 3.N21/5:15/L55B18a
Series: NACA research memorandum ;
Report Number: L55B18a
Subject: Ailerons--Performance
Link: https://hdl.handle.net/2027/mdp.39015095100874

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