Panel flutter analysis of nano-hybrid laminated composite quadrilateral plates presuming curvilinear fibers-Reference-Cited by-同舟云学术

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Panel flutter analysis of nano-hybrid laminated composite quadrilateral plates presuming curvilinear fibers

Published:2024-02-22 Issue: Volume: Page:1-18
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:

Fazilati Jamshid¹,Khalafi Vahid²,Jalalvand Meisam³

Affiliation:

1. Aeronautical Science and Technology Department, Aerospace Research Institute, Tehran, Iran

2. Aerospace Engineering Department, Shahid Sattari Aeronautical University of Science and Technology, Tehran, Iran

3. Engineering Materials, School of Engineering, University of Southampton, Southampton, UK

Publisher

Informa UK Limited

Link

https://www.tandfonline.com/doi/pdf/10.1080/15397734.2024.2316870

Reference36 articles.

1. Flutter of geometrical imperfect functionally graded carbon nanotubes doubly curved shells

2. Isogeometric analysis of the effect of CNT orientation on the static and vibration behaviors of CNT-reinforced skew composite plates

3. Enhancing flutter stability in nanocomposite thin panels by harnessing CNT/polymer dissipation

4. Linear aeroelastic analysis of cantilever hybrid composite laminated plates with curvilinear fibres and carbon nanotubes

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