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

Description
Item Description:	Title from title screen (viewed on Apr. 17, 2012). "November 2011." "Prepared for the 29th Applied Aerodynamics Conference sponsored by the American Institute of Aeronautics, Honolulu, Hawaii, June 27-30, 2011." "AIAA-2011-3801." Electronic resource.
Physical Description:	1 online resource (14 pages) : color illustrations
Bibliography:	Includes bibliographical references (pages 13-14).