Transient Analysis of Forced Vibrations of Complex Structural-Mechanical Systems
- 1 February 1962
- journal article
- research article
- Published by Cambridge University Press (CUP) in Journal of the Royal Aeronautical Society
- Vol. 66 (619), 457-460
- https://doi.org/10.1017/s0368393100076999
Abstract
This paper presents a numerical method, derived directly from the basic differential equations of motion and expressed in the form of recurrence-matrix of finite differences, that can be generally applied to all multi-degree-of-freedom structures subjected to dynamic forces or forced displacements on any masses at any instants of time. The movements of the system may be described by any form of generalised co-ordinates.Keywords
This publication has 3 references indexed in Scilit:
- Vibration of MissilesAircraft Engineering and Aerospace Technology, 1961
- A Method of Computation for Structural DynamicsJournal of the Engineering Mechanics Division, 1959
- A Recurrence Matrix Solution for the Dynamic Response of Elastic AircraftJournal of the Aeronautical Sciences, 1950