Application of computational fluid dynamics to a monoplane fixed-wing missile with elliptic cross sections /

Bibliographic Details
Main Author:	Heavey, Karen R.
Corporate Author:	U.S. Army Research Laboratory
Other Authors:	Sahu, Jabaraj
Format:	Government Document eBook
Language:	English
Published:	Aberdeen Proving Ground, MD : Army Research Laboratory, [2005]
Series:	ARL-TR (Aberdeen Proving Ground, Md.) ; 3549.
Subjects:	Guided missiles > Aerodynamics > Models. Fluid dynamics > Models.
Online Access:	https://purl.fdlp.gov/GPO/gpo5721

Description
Item Description:	Title from title screen (viewed on Mar. 25, 2011). "July 2005." Electronic resource.
Physical Description:	1 online resource (vi, 30 pages) : color illustrations