Nonlinear Dynamic Modeling for a Flexible Laminated Composite Appendage Attached to a Spacecraft Body Undergoing Deployment and Locking Motions-Reference-Cited by-同舟云学术

Nonlinear Dynamic Modeling for a Flexible Laminated Composite Appendage Attached to a Spacecraft Body Undergoing Deployment and Locking Motions

Published:2016-09 Issue:5 Volume:29 Page:04016018
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

You Bin Di¹,Wen Jian Min²,Zhang Guang Yu³,Zhao Yang⁴

Affiliation:

1. Associate Professor, School of Naval Architecture and Ocean Engineering, Harbin Institute of Technology, Weihai, Shandong 264209, China.

2. Associate Professor, School of Naval Architecture and Ocean Engineering, Harbin Institute of Technology, Weihai, Shandong 264209, China (corresponding author).

3. Professor, School of Mechanical and Electrical Engineering, Harbin Institute of Technology, Harbin, Heilongjiang 150001, China.

4. Professor, School of Astronautics Engineering, Harbin Institute of Technology, Harbin, Heilongjiang 150001, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000570

Reference31 articles.

1. NON-LINEAR VIBRATION CHARACTERISTICS OF CLAMPED LAMINATED SHALLOW SHELLS

2. Nonlinear dynamic behaviors of clamped laminated shallow shells with one-to-one internal resonance

3. Anantharaman M. (1987). “The dynamic analysis of flexible mechanisms using finite element methods.” Ph.D. dissertation Univ. of Stuttgart Stuttgart Germany.

4. Nonlinear elastic deformations of moderately thick laminated shells subjected to large and rapid rigid-body motion

5. Vibration control of rotating beams with active constrained layer damping

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