A structural optimization of laminated composite curved structure for an elastic shock absorber of UAV based on a novel theory-Reference-Cited by-同舟云学术

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A structural optimization of laminated composite curved structure for an elastic shock absorber of UAV based on a novel theory

Published:2020-12-07 Issue: Volume: Page:1-20
ISSN:1537-6494
Container-title:Mechanics of Advanced Materials and Structures
language:en
Short-container-title:Mechanics of Advanced Materials and Structures

Author:

Kim Yongha¹^ORCID,Lee Jungjin²,Park Jungsun³

Affiliation:

1. The 4th R&D Institute, Agency for Defense Development, Deajeon, South Korea

2. UAV Research Group, Korea Aerospace Research Institute, Deajeon, South Korea

3. Department of Aerospace and Mechanical Engineering, Korea Aerospace University, Goyang-si, South Korea

Publisher

Informa UK Limited

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science,General Mathematics,Civil and Structural Engineering

Link

https://www.tandfonline.com/doi/pdf/10.1080/15376494.2020.1855489

Reference33 articles.

1. Experimental and numerical study on residual strength of aircraft carbon/epoxy composite after lightning strike

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1. Experimental study on the free and constrained vibration performance of composite wave springs;Mechanics of Advanced Materials and Structures;2024-09-14

2. A mathematical method for the vibration analysis of composite lattice plates under In-plane compressive loads;Advanced Composite Materials;2024-03-15

3. Thermo-structural optimization of multiple composite layers with variable elliptical cross-sections;Composite Structures;2021-08

4. A Novel Algorithm for Dynamic Control System of Hysteretic Power of Shock Absorber;International Journal of Circuits, Systems and Signal Processing;2021-03-30

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