Numerical and experimental investigation on dynamics of deployable space telescope experiencing deployment and attitude adjustment motions coupled with laminated composite shell-Reference-Cited by-同舟云学术

Numerical and experimental investigation on dynamics of deployable space telescope experiencing deployment and attitude adjustment motions coupled with laminated composite shell

Published:2020-01-24 Issue:1 Volume:50 Page:268-287
ISSN:1539-7734
Container-title:Mechanics Based Design of Structures and Machines
language:en
Short-container-title:Mechanics Based Design of Structures and Machines

Author:

You Bindi¹,Yu Xiangjie¹,Liang Dong¹,Liu Xiaomeng¹,Yang Xujian¹

Affiliation:

1. School of Naval Architecture and Ocean Engineering, Harbin Institute of Technology, Weihai, China

Funder

National Natural Science Foundation of China

Publisher

Informa UK Limited

Subject

Mechanical Engineering,Mechanics of Materials,Ocean Engineering,Condensed Matter Physics,Aerospace Engineering,Automotive Engineering,General Mathematics,Civil and Structural Engineering

Link

https://www.tandfonline.com/doi/pdf/10.1080/15397734.2020.1717341

Reference22 articles.

1. Novel shear deformation model for moderately thick and deep laminated composite conoidal shell

2. Geometrically nonlinear transient analysis of composite laminated plate and shells subjected to low-velocity impact

3. THERMAL–DYNAMIC COUPLING ANALYSIS OF LARGE SPACE STRUCTURES CONSIDERING GEOMETRIC NONLINEARITY

4. Analysis of Stress and Strain in the Absolute Nodal Coordinate Formulation

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