Cover Image

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
Description
Item Description:Title from title screen (viewed on Apr. 1, 2011).
"March 2004."
Electronic resource.
Physical Description:1 online resource (x, 92 pages) : color illustrations