A \((3,2)\) reduced degree-of-freedom unified zigzag laminated beam theory
From MaRDI portal
Publication:1988786
DOI10.1016/J.APM.2019.09.041zbMath1481.74449OpenAlexW2975199282WikidataQ127214918 ScholiaQ127214918MaRDI QIDQ1988786
Publication date: 24 April 2020
Published in: Applied Mathematical Modelling (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.apm.2019.09.041
Cites Work
- Unnamed Item
- Refined zigzag theory for homogeneous, laminated composite, and sandwich beams derived from Reissner's mixed variational principle
- Recent advances in analysis of laminated beams and plates. Part I - Sheareffects and buckling.
- Recent Advances in Analysis of Laminated Beams and Plates, Part II: Vibrations and Wave Propagation
- Thick beam theory and finite element model with zig-zag sublaminate approximations
- Analysis of thick sandwich construction by a \(\{3,2\}\)-order theory.
This page was built for publication: A \((3,2)\) reduced degree-of-freedom unified zigzag laminated beam theory