Effects of wing warp on the lift, drag, and static longitudinal stability characteristics of an aircraft configuration having an arrow wing of aspect ratio 1.86 at Mach numbers from 1.1 to 1.7

Author:	Gillespie, Warren, Jr.
Year:	1957
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L57G12
Link:	https://digital.library.unt.edu/ark:/67531/metadc63619/