An approximate method for pitch-damping prediction /

A simple method of estimating the pitch-damping coefficients for axisymmetric flight bodies has been developed. The method is suitable for preliminary design and parametric studies. The procedure is based on concepts from slender body theory, but the method significantly improves the accuracy of the...

Full description

Bibliographic Details
Main Author:	Danberg, James E.
Corporate Author:	U.S. Army Research Laboratory
Other Authors:	Weinacht, P.
Format:	Government Document eBook
Language:	English
Published:	Aberdeen Proving Ground, MD : Army Research Laboratory, [2003]
Series:	ARL-TR (Aberdeen Proving Ground, Md.) ; 3007.
Subjects:	Axial flow. Angle of attack (Aerodynamics) Flight control. Mechanics. Ammunition and Explosives. Pitch(inclination) Damping. Computational fluid dynamics. Data bases. Aerodynamic configurations. Flight testing. Parametric analysis. Slender bodies. Predictions. Validation. Projectiles. Theory. Accuracy. Correlation. Coefficients. Length. Axisymmetric. Mach number. Noses. Functions(mathematics)
Online Access:	https://purl.fdlp.gov/GPO/gpo1394

Internet

https://purl.fdlp.gov/GPO/gpo1394

Available Online

Holdings details from Available Online
Call Number	Status	Get It
Call Number:		D 101.133:3007

D 101.133:3007	Available