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

Author:	Thompson, Robert F.
Year:	1954
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L54I09
Link:	https://digital.library.unt.edu/ark:/67531/metadc60920/