Exhaust nozzle plume effects on sonic boom test results for vectored nozzles /

Bibliographic Details
Main Author:	Castner, Raymond S.
Corporate Authors:	NASA Glenn Research Center, Joint Propulsion Conference and Exhibit
Format:	Government Document Conference Proceeding eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
Series:	NASA technical memorandum ; 217229.
Subjects:	Exhaust nozzles. Sonic booms. Computational fluid dynamics. Elastic waves. Plumes. F-15 aircraft. Supersonic aircraft. Pressure ratio.
Online Access:	https://purl.fdlp.gov/GPO/gpo28438

Description
Item Description:	Title from title screen (viewed on Nov. 1, 2012). "February 2012." "Prepared for the 47th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE,San Diego, California, July 31-August 3, 2011." "AIAA-2011-5974." Electronic resource.
Physical Description:	1 online resource (16 pages) : color illustrations
Bibliography:	Includes bibliographical references (pages 15-16).