A Transonic Investigation of Changing Indentation Design Mach Number on the Aerodynamic Characteristics of a 45 Degree Sweptback-Wing-Body Combination Designed for High Performance

Author:	Loving, Donald L.
Year:	1956
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L55J07
Link:	https://digital.library.unt.edu/ark:/67531/metadc62013/