Experimental study on crashworthiness and failure mechanisms of aeronautical multi-fibers hybrid composite corrugated structures with Carbon, Glass, Kevlar-Reference-Cited by-同舟云学术

Experimental study on crashworthiness and failure mechanisms of aeronautical multi-fibers hybrid composite corrugated structures with Carbon, Glass, Kevlar

Published:2023-11 Issue: Volume:142 Page:108599
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Guo Kaijin,Liu Xuefeng,Ren Yiru^ORCID,Jiang Hongyong

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference40 articles.

1. A novel ablative material for thermal protection system: carbon fiber/polysiloxane composites;Hou;Aerosp. Sci. Technol.,2022

2. Interfacial design and flexural property of CFRP/aluminum-honeycomb sandwich with Aramid-pulp micro/nano-fiber interlays;Jiang;Compos. Struct.,2022

3. An experimental investigation on damage mechanisms of thick hybrid composite structures under flexural loading using multi-instrument measurements;Gul;Aerosp. Sci. Technol.,2021

4. Hybrid effects and interactive failure mechanisms of hybrid fiber composites under flexural loading: carbon/Kevlar, carbon/glass, carbon/glass/Kevlar;Jiang;Aerosp. Sci. Technol.,2023

5. Low-velocity impact resistance behaviors of bio-inspired helicoidal composite laminates with non-linear rotation angle based layups;Jiang;Compos. Struct.,2019

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