Nonlinear thermal flutter of variable angle tow composite laminates in supersonic airflow-Reference-Cited by-同舟云学术

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Nonlinear thermal flutter of variable angle tow composite laminates in supersonic airflow

Published:2024-07-31 Issue: Volume: Page:1-18
ISSN:1537-6494
Container-title:Mechanics of Advanced Materials and Structures
language:en
Short-container-title:Mechanics of Advanced Materials and Structures

Author:

Li Huizhong¹^ORCID,Nie Guojun¹²^ORCID,Chen Xiaodong³^ORCID

Affiliation:

1. School of Aerospace Engineering and Applied Mechanics, Tongji University, Shanghai, China

2. Shanghai Institute of Aircraft Mechanics and Control, Shanghai, China

3. School of Civil and Transportation Engineering, Henan University of Urban Construction, Pingdingshan, China

Funder

National Natural Science Foundation of China

Shanghai Gaofeng Project for University Academic Program Development

Youth Backbone Teacher Programme

Henan University of Urban Construction, China

Publisher

Informa UK Limited

Link

https://www.tandfonline.com/doi/pdf/10.1080/15376494.2024.2380087

Reference42 articles.

1. Vibration and flutter analysis of damaged composite plates under thermal environment and its passive control using piezoelectric patches

2. Overview of Computational Methods to Predict Flutter in Aircraft

3. Flutter of Rectangular Simply Supported Panels at High Supersonic Speeds

4. Theoretical considerations of panel flutter at high supersonic Mach numbers.

5. Nonlinear oscillations of a fluttering plate.

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