The aerodynamic characteristics of a supersonic aircraft configuration with a 40 degree sweptback wing through a Mach number range from 0 to 2.4 obtained from various sources

Author:	Spearman, M. Leroy
Year:	1952
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L52A21
Link:	https://digital.library.unt.edu/ark:/67531/metadc59085/