Investigating Interlaminar Stresses in Stress Concentration Zones of Laminated Composite Shells of Revolution Using Quasi-3D Theory with the Transverse Stress Recovery-Reference-Cited by-同舟云学术

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Investigating Interlaminar Stresses in Stress Concentration Zones of Laminated Composite Shells of Revolution Using Quasi-3D Theory with the Transverse Stress Recovery

Published:2024-11 Issue:6 Volume:37 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Thien Pham Vinh¹^ORCID,Vasilyevich Firsanov Valery²,Doan Tran Ngoc³^ORCID

Affiliation:

1. Researcher, Aircraft Technology Dept., Institute of Technology, Hanoi 125993, Vietnam. ORCID: .

2. Lead Scientist, Faculty of Mechanical Engineering, Moscow Aviation Institute, Moscow 125993, Russian Federation.

3. Lead Scientist, Faculty of Aerospace Engineering, Le Quy Don Technical Univ., Hanoi 122300, Vietnam (corresponding author). ORCID: .

Publisher

American Society of Civil Engineers (ASCE)

Link

https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-5577

Reference52 articles.

1. Application of chebyshev polynomials to the analysis of laminated axisymmetric spherical shells

2. Analysis of laminated orthotropic spherical shells subjected to asymmetric loads

3. Ambartsumyan, S. A. 1970. Theory of anisotropic plates. Lancaster, PA: Technomic.

4. Static analysis of thick laminated shells with different boundary conditions using GDQ

5. Three-dimensional elasticity solution for static response of orthotropic doubly curved shallow shells on rectangular planform

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