Reduced-Order Models for a Shallow Curved Beam Under Combined Loading-Reference-Cited by-同舟云学术

Reduced-Order Models for a Shallow Curved Beam Under Combined Loading

Published:2010-01 Issue:1 Volume:48 Page:47-55
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Spottswood S. Michael¹,Hollkamp Joseph J.¹,Eason Thomas G.¹

Affiliation:

1. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.38707

Reference19 articles.

1. A FINITE ELEMENT TIME DOMAIN MODAL FORMULATION FOR LARGE AMPLITUDE FREE VIBRATIONS OF BEAMS AND PLATES

2. A COMBINED MODAL/FINITE ELEMENT ANALYSIS TECHNIQUE FOR THE DYNAMIC RESPONSE OF A NON-LINEAR BEAM TO HARMONIC EXCITATION

3. McEwan, M. I. "A Combined Modal/Finite Element Technique for the Non-Linear Dynamic Simulation of Aerospace Structures," Ph.D. Dissertation, School of Engineering,Univ. of Manchester, Manchester,England, 2001.

4. Determination of nonlinear stiffness with application to random vibration of geometrically nonlinear structures

5. Nonlinear modal models for sonic fatigue response prediction: a comparison of methods

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