Computational analysis of a low-boom supersonic inlet /

Bibliographic Details

Main Author:	Chima, Rodrick V.
Corporate Authors:	NASA Glenn Research Center, AIAA Applied Aerodynamics Conference
Format:	Government Document Conference Proceeding eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2011]
Series:	NASA technical memorandum ; 2011-217223.
Subjects:	Computational fluid dynamics. Engine inlets. Supersonic aircraft. Supersonic inlets. Inlet airframe configurations. Overpressure. Supersonic flow. Sonic booms. Wind tunnel tests.
Online Access:	https://purl.fdlp.gov/GPO/gpo21529