Vibration Characteristics and Aeroelastic Stability Behavior of Foam-Filled Composite Corrugated Sandwich Panels Considering Mass Reduction-Reference-Cited by-同舟云学术

Vibration Characteristics and Aeroelastic Stability Behavior of Foam-Filled Composite Corrugated Sandwich Panels Considering Mass Reduction

Published:2024-03 Issue:2 Volume:37 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Zhou Jian¹,Tian Zheng²^ORCID,Zhou Jie³,Zhang Zhijia⁴,Xu Minglong⁵

Affiliation:

1. Associate Professor, State Key Laboratory for Strength and Vibration of Mechanical Structures, School of Aerospace Engineering, Xi’an Jiaotong Univ., Xi’an 710049, China (corresponding author).

2. Ph.D. Student, School of Aerospace Engineering, Xi’an Jiaotong Univ., Xi’an 710049, China. ORCID: .

3. Senior Engineer, Intelligent Control Research Dept., Shanghai Aerospace System Engineering Institute, Shanghai 201109, China.

4. Associate Professor, School of Aerospace Engineering, Xi’an Jiaotong Univ., Xi’an 710049, China.

5. Professor, School of Aerospace Engineering, Xi’an Jiaotong Univ., Xi’an 710049, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

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

Link

https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-5298

Reference36 articles.

1. Nonlinear Flutter of Composite Panels Under Yawed Supersonic Flow Using Finite Elements

2. Review of composite sandwich structure in aeronautic applications

3. Nonlinear Flutter Suppression and Thermal Buckling Elimination for Composite Lattice Sandwich Panels

4. Nonlinear vibrations, bifurcations and chaos of lattice sandwich composite panels on Winkler–Pasternak elastic foundations with thermal effects in supersonic airflow

5. Investigations on the influences of elastic foundations on the aerothermoelastic flutter and thermal buckling properties of lattice sandwich panels in supersonic airflow