An approximate approach on the buckling analysis of a composite lattice cylindrical panel
Author:
Affiliation:
1. The 4th R&D Institute - 5th Directorate, Agency for Defense Development , Deajeon 34186, South Korea
2. Department of Aerospace and Mechanical Engineering, Korea Aerospace University , Goyang-si 10540, South Korea
Funder
Development of the Composite Lattice Structure
Institute of Civil Military Technology Cooperation
Publisher
Informa UK Limited
Subject
Mechanical Engineering,Mechanics of Materials,Ceramics and Composites
Link
https://www.tandfonline.com/doi/pdf/10.1080/09243046.2020.1755100
Reference21 articles.
1. Anisogrid composite lattice structures – Development and aerospace applications
2. Zhang Y , Xue Z , Chen L , et al. Deformation and failure mechanisms of lattice cylindrical shells under axial loading. J Mech Sci. 1993;51(3):213–221.
3. Finite-element modelling and buckling analysis of anisogrid composite lattice cylindrical shells
4. Study of filament wound grid-stiffened composite cylindrical structures
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