Flight Investigation of the Supersonic Area Rule for a Straight Wing-Body Configuration at Mach Numbers Between 0.8 and 1.5

Author:	Hoffman, Sherwood
Additional Authors:	Wolff, Austin L.
Year:	1955
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L55C09
Link:	https://digital.library.unt.edu/ark:/67531/metadc61224/