Aerodynamic and inlet-flow-field characteristics at a free-stream Mach number of 3.0 for airplanes with circular fuselage cross sections and for two engine locations

Author:	Dryer, Murray
Year:	1958
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E57K26
Link:	https://digital.library.unt.edu/ark:/67531/metadc64014/