Numerical prediction of supersonic shock-boundary layer interaction /

Bibliographic Details
Main Author:	Bhagwandin, Vishal A.
Corporate Author:	U.S. Army Research Laboratory
Other Authors:	DeSpirito, James
Format:	Government Document eBook
Language:	English
Published:	Aberdeen Proving Ground, MD : Army Research Laboratory, [2011]
Series:	ARL-TR (Aberdeen Proving Ground, Md.) ; 5602.
Subjects:	Shock waves > Research. Aerospace engineering > Research.
Online Access:	https://purl.fdlp.gov/GPO/gpo11650

Description
Item Description:	Title from title screen (viewed on Aug. 19, 2011). "July 2011." Electronic resource.
Physical Description:	1 online resource (viii, 36 pages) : color illustrations
Bibliography:	Includes bibliographical references (pages 32-33).