An analytical study of the comparative performance of four air-induction systems for turbojet-powered airplanes designed to operate at Mach numbers up to 1.5

Author:	Blackaby, James R
Year:	1952
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A52C14
Link:	https://digital.library.unt.edu/ark:/67531/metadc59221/