Free Vibration Analysis of Frames Using the Transfer Dynamic Stiffness Matrix Method

Author:

Tu Tsung-Hsien1,Yu Jen-Fang2,Lien Hsin-Chung3,Tsai Go-Long4,Wang B. P.5

Affiliation:

1. Institute of Mechanical and Electrical Engineering, National Taipei University of Technology, Taiwan

2. Graduate Institute of Medical Mechatronics, Chang Gung University

3. Department of Mechanical Engineering, Northern Taiwan Institute of Science and Technology

4. Department of Vehicle Engineering, National Taipei University of Technology, Taiwan

5. Department of Mechanical and Aerospace Engineering, University of Texas at Arlington, Arlington, TX 76019

Abstract

A method for free vibration of 3D space frame structures employing transfer dynamic stiffness matrix (TDSM) method based on Euler–Bernoulli beam theory is developed in this paper. The exact TDSM of each member is assembled to obtain the system matrix that is frequency dependent. All free vibration eigensolutions including coincident roots for the characteristic equation can be obtained to any desired accuracy using the algorithm developed by Wittrick and Williams (1971, “A General Algorithm for Computing Natural Frequencies of Elastic Structures,” Q. J. Mech. Appl. Math., 24, pp. 263–284). Exact eigenfunction of structures can then be computed using the dynamic shape function and the corresponding eigenvector. The results showed good agreement with those computed by finite element method.

Publisher

ASME International

Subject

General Engineering

Reference8 articles.

1. Matrix Methods in Elastomechanics

2. Myklestad, N. O. , 1944, “A New Method of Calculating Natural Modes of Uncoupled Bending Vibration,” J. Aeronaut. Sci.0095-9812, p. 153.

3. Exact Dynamic Member Stiffnesses for a Beam on an Elastic Foundation;Williams;Earthquake Eng. Struct. Dyn.

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