Experimental investigation at Mach numbers from 0 to 1.9 of trapezoidal and circular side inlets for a fighter-type airplane

Author:	Mossman, Emmett A.
Additional Authors:	Pfyl, Frank A.
Year:	1955
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A55D27
Link:	https://digital.library.unt.edu/ark:/67531/metadc61314/