Lift, drag, and static longitudinal stability characteristics of configurations consisting of three triangular wing panels and a body of equal length at Mach numbers from 3.00 to 6.28

Author:	Savin, Raymond C.
Year:	1956
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A55K21
Link:	https://digital.library.unt.edu/ark:/67531/metadc62366/