An Enhanced Global–Local Higher-Order Model for Thermal Expansion Analysis of Laminated Panels Reinforced by Carbon Nanotubes-Reference-Cited by-同舟云学术

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An Enhanced Global–Local Higher-Order Model for Thermal Expansion Analysis of Laminated Panels Reinforced by Carbon Nanotubes

Published:2024-07 Issue:4 Volume:37 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Ling Shengbo¹,Wu Zhen²^ORCID,Mei Jie¹,Ren Xiaohui³

Affiliation:

1. Ph.D. Student, School of Aeronautics, Northwestern Polytechnical Univ., Xi'an 710072, China.

2. Professor, School of Aeronautics, Northwestern Polytechnical Univ., Xi'an 710072, China (corresponding author). ORCID: .

3. Professor, School of Mechanical Engineering, Xi'an Aeronautical Univ., Xi'an 710065, China.

Publisher

American Society of Civil Engineers (ASCE)

Link

https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-5357

Reference39 articles.

1. Non-linear stability analysis of CNT reinforced composite cylindrical shell panel subjected to thermomechanical loading

2. Bending analysis of laminated SWCNT Reinforced functionally graded plate Using FEM

3. Free vibration analysis of hybrid laminated plates containing multilayer functionally graded carbon nanotube-reinforced composite plies using a layer-wise formulation

4. Higher order zig-zag theory for fully coupled thermo-electric–mechanical smart composite plates

5. Bending and free vibration analysis of functionally graded sandwich plates: An assessment of the Refined Zigzag Theory

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