Numerical investigation of aerodynamics of canard-controlled missile using planar and grid tail fins. Part II, Subsonic and transonic flow /

Bibliographic Details
Main Author:	DeSpirito, James
Corporate Author:	U.S. Army Research Laboratory
Other Authors:	Vaughn, Milton E., Jr, Washington, W. David
Format:	Government Document eBook
Language:	English
Published:	Aberdeen Proving Ground, MD : Army Research Laboratory, [2004]
Series:	ARL-TR (Aberdeen Proving Ground, Md.) ; 3162.
Subjects:	Rockets (Aeronautics) > Canard fins > Aerodynamics > Models. Rockets (Aeronautics) > Fins > Aerodynamics > Models.
Online Access:	https://purl.fdlp.gov/GPO/gpo5719

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