Dynamic characteristics of a two-stage variable-mass flexible missile with internal flow /

Dynamic characteristics of a two-stage variable-mass flexible missile with internal flow / Leonard Meirovitch and John Bankovskis.

A general formulation of the dynamical problems associated with powered flight of a two stage flexible, variable-mass missile with internal flow, discrete masses, and aerodynamic forces is presented. The formulation comprises six ordinary differential equations for the rigid body motion, 3n ordinary...

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Main Author: Meirovitch, Leonard
Corporate Authors: University of Cincinnati, Langley Research Center, United States. National Aeronautics and Space Administration
Other Authors: Bankovskis, John
Format: Government Document Book
Language:English
Published: Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service [distributor], 1972.
Series:NASA contractor report ; NASA CR-2076.
Subjects:
Rockets (Aeronautics) > Aerodynamics > Computer simulation.
Aeroelasticity.
Dynamic structural analysis.
Missile structures.
Residual stress.
Flexible bodies.
Internal combustion engines.
Thrust loads.
Transient response.
Variable mass systems.

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Norlin Library - Government Information - US

Holdings details from Norlin Library - Government Information - US
Call Number: NAS 1.26:2076
NAS 1.26:2076 Available Place a Hold

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