Aerothermoelastic flutter analysis and active vibration suppression of nonlinear composite laminated panels with time-dependent boundary conditions in supersonic airflow-Reference-Cited by-同舟云学术

Aerothermoelastic flutter analysis and active vibration suppression of nonlinear composite laminated panels with time-dependent boundary conditions in supersonic airflow

Published:2017-07-28 Issue:4 Volume:29 Page:653-668
ISSN:1045-389X
Container-title:Journal of Intelligent Material Systems and Structures
language:en
Short-container-title:Journal of Intelligent Material Systems and Structures

Author:

Chai Yuyang¹,Li Fengming¹²³,Song Zhiguang⁴,Zhang Chuanzeng³

Affiliation:

1. School of Astronautics, Harbin Institute of Technology, Harbin, China

2. College of Aerospace and Civil Engineering, Harbin Engineering University, Harbin, China

3. Department of Civil Engineering, University of Siegen, Siegen, Germany

4. Dynamics and Vibrations Group, Institute of Numerical Methods in Mechanical Engineering, Technische Universität Darmstadt, Darmstadt, Germany

Funder

National Natural Science Foundation of China

Publisher

SAGE Publications

Subject

Mechanical Engineering,General Materials Science

Link

http://journals.sagepub.com/doi/pdf/10.1177/1045389X17721027

Reference41 articles.

1. Nonlinear Vibration Behaviors of Composite Laminated Plates with Time-Dependent Base Excitation and Boundary Conditions

2. Mixing Rules for the Piezoelectric Properties of Macro Fiber Composites

3. Aeroelastic behavior of composite laminated shells with embedded SMA wires under supersonic flow

4. Nonlinear oscillations of a fluttering plate.

5. Active control of panel flutter with piezoelectric transducers

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