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To study the effect of rocket mass and an intermediate mass on the critical flutter load of a free-free beam (missile-like structure).
A finite element model of beam considering shear deformation and rotary inertia, based on Hamilton's principle applied to non-conservative system.
Smaller geometric dimensions of the end rocket assist in the stability. Optimum positioning of the intermediate mass leads to stability.
The stability of free-free missile structures can be better understood.
Sheds new light on the effect of rocket mass and an intermediate mass on the critical flutter load of a free-free beam.
Dynamic instability characteristics of a free-free missile structure under a controlled follower force
Aircraft Engineering and Aerospace Technology ; 78 , 6 ; 509-514
2006-11-01
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Dynamic stability of a free-free Timoshenko beam subjected to a pulsating follower force
Online Contents | 1998
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