Nonlinear thermo-elastic stability of variable stiffness curvilinear fibres based layered composite beams by shear deformable trigonometric beam model coupled with modified constitutive equations-Reference-Cited by-同舟云学术

Nonlinear thermo-elastic stability of variable stiffness curvilinear fibres based layered composite beams by shear deformable trigonometric beam model coupled with modified constitutive equations

Published:2023-01 Issue: Volume:148 Page:104303
ISSN:0020-7462
Container-title:International Journal of Non-Linear Mechanics
language:en
Short-container-title:International Journal of Non-Linear Mechanics

Author:

Manickam Ganapathi,Haboussi Mohamed,D’Ottavio Michele,Kulkarni Vedang,Chettiar Alfred,Gunasekaran Vijay

Publisher

Elsevier BV

Subject

Applied Mathematics,Mechanical Engineering,Mechanics of Materials

Reference73 articles.

1. Recent advances in analysis of laminated beams and plates. Part I - Shear effects and buckling;Kapania;AIAA J.,1989

2. Non-linear free periodic vibrations of variable stiffness composite laminated plates;Ribeiro;Nonlinear Dynam.,2012

3. Analysis of tow-placed, variable-stiffness laminates;Waldhart,1996

4. The use of curvilinear fiber format to improve buckling resistance of composite plates with central circular holes;Hyer;Compos. Struct.,1991

5. Thermal buckling load optimization of laminated skew plates;Topal;Mater. Des.,2009

Cited by 9 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Generalized model for eigenfrequency analysis of bolted variable-stiffness flanged-cylindrical shells;International Journal of Mechanical Sciences;2024-11

2. Frequency trajectory and modal analysis of variable stiffness composite cylindrical shells with flange;Composite Structures;2024-09

3. Influence of thermo-mechanical loads on variable stiffness composite beams: a comprehensive study using semi-analytical and finite element approaches;Mechanics Based Design of Structures and Machines;2024-05-29

4. Dynamics control of L-shaped composite structure in electric aircraft: Theoretical analysis and experimental validation;Composite Structures;2024-04

5. New Approach of Normal and Shear Stress Components for Multiple Curvilinear Holes Which Weakened a Flexible Plate;Symmetry;2024-03-16