Nonlinear resonant responses of a novel FGM sandwich cylindrical shell structure for supersonic flight vehicles based on 1:1 internal resonance between conjugate modes-Reference-Cited by-同舟云学术

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Nonlinear resonant responses of a novel FGM sandwich cylindrical shell structure for supersonic flight vehicles based on 1:1 internal resonance between conjugate modes

Published:2024-09 Issue: Volume:152 Page:109372
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Zhang Wei,Zheng Huiying^ORCID,Liu Tao^ORCID,Zheng Yan,Qian Yingjing,Su Xiaoyang

Funder

Beijing Natural Science Foundation

China Postdoctoral Science Foundation

National Natural Science Foundation of China

Beijing Institute of Graphic Communication

Publisher

Elsevier BV

Reference54 articles.

1. Cellular solids: Structure and Properties;Gibson,1997

2. Impact On Composite Structures;Abrate,2011

3. Fire Properties of Polymer Composite Materials;Mouritz,2006

4. On the low frequency acoustic properties of novel multifunctional honeycomb sandwich panels with micro-perforated faceplates;Meng;Appl. Acoust.,2019

5. Vibration behavior of metallic sandwich panels with Hourglass truss cores;Li;Mar. Struct.,2019

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