Exhaust nozzle plume and shock wave interaction /

Bibliographic Details
Main Authors:	Castner, Raymond S. (Author), Elmiligui, Alaa (Author), Cliff, Susan (Author)
Corporate Authors:	Fundamental Aeronautics Program (U.S.), United States. National Aeronautics and Space Administration (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2013.
Series:	NASA technical memorandum ; 217838.
Subjects:	Computational fluid dynamics. Shock wave interaction. Convergent-divergent nozzles. Sonic booms.
Online Access:	https://purl.fdlp.gov/GPO/gpo51485 http://purl.fdlp.gov/GPO/gpo51485

Description
Item Description:	Title from title screen (viewed on Aug. 21, 2014). "February 2013." "Prepared for the 51st Aerospace Science Conference sponsored by the American Institute of Aeronautics and Astronautics, Grapevine, Texas, January 7-10, 2013."
Physical Description:	1 online resource (21 pages) : illustrations.
Bibliography:	Includes bibliographical references (pages 20-21).