An analytical study of the comparative performance of six air-induction systems for turbojet-powered airplanes designed to operate at Mach numbers up to 2.0

Author:	Watson, Earl C.
Year:	1953
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A53H03
Link:	https://digital.library.unt.edu/ark:/67531/metadc59804/