Transonic Wind-Tunnel Investigation of Static-Pressure Fluctuations in Duct of a Scale Inlet Model of a Supersonic Fighter-Bomber Airplane

Author:	Brooks, Joseph D.
Year:	1957
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L57C17
Link:	https://digital.library.unt.edu/ark:/67531/metadc53180/