Aerodynamic load distribution over a 45 degree swept wing having a spoiler-slot-deflector aileron and other spoiler ailerons for Mach numbers from 0.60 to 1.03

Author:	West, F. E., Jr.
Additional Authors:	Whitcomb, Charles F.
Year:	1957
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L57J11
Link:	https://digital.library.unt.edu/ark:/67531/metadc64127/