A novel composite model for vibration of thin-walled layered composite panels incorporating the agglomeration of CNTs-Reference-Cited by-同舟云学术

A novel composite model for vibration of thin-walled layered composite panels incorporating the agglomeration of CNTs

Published:2021-09 Issue: Volume:116 Page:106897
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Shahmohammadi Mohammad Amin,Azhari Mojtaba,Salehipour Hamzeh,Civalek Ömer^ORCID

Funder

Iran National Science Foundation

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference84 articles.

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4. Nonlinear response and buckling analysis of eccentrically stiffened FGM toroidal shell segments in thermal environment;Vuong;Aerosp. Sci. Technol.,2018

5. Nonlinear buckling and post-buckling behavior of shear deformable sandwich toroidal shell segments with functionally graded core subjected to axial compression and thermal loads;Vuong;Aerosp. Sci. Technol.,2020

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