Mechanical Behavior of a Fuselage Stiffened Carbon-Epoxy Panel under Debonding Load-Reference-Cited by-同舟云学术

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Mechanical Behavior of a Fuselage Stiffened Carbon-Epoxy Panel under Debonding Load

Published:2018 Issue:02 Volume:07 Page:
ISSN:2168-9792
Container-title:Journal of Aeronautics & Aerospace Engineering
language:
Short-container-title:J Aeronaut Aerospace Eng

Author:

M Torres,Urquiza EA Franco,Moreno H Hernandez,Villa MA Gonzalez

Publisher

OMICS Publishing Group

Subject

General Medicine

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Successive self-nucleation and Annealing technique applied to polypropylene/butyl rubber composites: Recycling alternatives for vacuum bagging materials;Journal of Reinforced Plastics and Composites;2024-09-03

2. Innovation in Aircraft Cabin Interior Panels. Part II: Technical Assessment on Replacing Glass Fiber with Thermoplastic Polymers and Panels Fabricated Using Vacuum Forming Process;Polymers;2021-09-24

3. Innovation in Aircraft Cabin Interior Panels Part I: Technical Assessment on Replacing the Honeycomb with Structural Foams and Evaluation of Optimal Curing of Prepreg Fiberglass;Polymers;2021-09-22

4. Manufacturing Process of High Performance—Low Cost Composite Structures for Light Sport Aircrafts;Aerospace;2019-02-01

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