A geometric modeling method for an integrally stiffened panel with three-dimensional woven composites-Reference-Cited by-同舟云学术

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A geometric modeling method for an integrally stiffened panel with three-dimensional woven composites

Published:2023-07-02 Issue: Volume: Page:1-14
ISSN:1537-6494
Container-title:Mechanics of Advanced Materials and Structures
language:en
Short-container-title:Mechanics of Advanced Materials and Structures

Author:

Kim Hiyeop¹^ORCID,Kim Yoenhi²,Park Jungsun²,Byun Joonhyung³

Affiliation:

1. Advanced Technology R&D Center, Hanwha Aerospace, Seongnam, South Korea

2. Department of Aerospace and Mechanical Engineering, Korea Aerospace University, Goyang, South Korea

3. Composites Research Division, Korea Institute of Materials Science, Changwon, South Korea

Funder

National Research Foundation of 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/10.1080/15376494.2023.2226137

Reference34 articles.

1. Buckling behavior of stiffened composite panels with variable thickness skin under compression

2. Analysis of skin-stringer debonding in composite panels through a two-way global-local method

3. A robust numerical approach for the simulation of skin–stringer debonding growth in stiffened composite panels under compression

4. Debonding monitoring of CFRP T-joint using optical acoustic emission sensor

5. 3D woven preforms for E-textiles and composites reinforcements

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