Advanced Aircraft Composite Structure Design

A special issue of Aerospace (ISSN 2226-4310). This special issue belongs to the section "Aeronautics".

Deadline for manuscript submissions: 31 May 2026 | Viewed by 504

Special Issue Editors

School of Aeronautics, Northwestern Polytechnical University, Xi'an, China
Interests: composite damage; composite repair; adhesive bonding; environmental durability

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Guest Editor
School of Aeronautics, Northwestern Polytechnical University, Xi'an, China
Interests: high temperature; high strain rate; ceramic matrix composites; joints; impact; dynamic damage

Special Issue Information

Dear Colleagues,

The past few decades have seen outstanding advances in the use of composite materials in the aerospace industry. Composites have revolutionized traditional design concepts and made possible an unparalleled range of new and exciting viable materials for aircraft structures.

This Special Issue, titled "Advanced Aircraft Composite Structure Design", focuses on the latest advancements and cutting-edge research that contribute to knowledge in the use of composite materials in aircraft structures. Original research papers and review articles dealing with design, research, and development studies, experimental investigations, theoretical analysis, and fabrication techniques relevant to the application of composites, ranging from individual components such as plates to complete composite structures, are welcome.

By bringing together advancements in the development, characterization, and application of composite materials, this Special Issue aims to disseminate knowledge between users, manufacturers, engineers, and researchers involved in aircraft component manufacturing using composite materials.

Dr. Wei Feng
Dr. Chao Zhang
Guest Editors

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Keywords

  • fiber-reinforced composite materials
  • functional and multi-functional composites
  • additive manufacturing of composites
  • finite modeling method
  • dynamic response of composite structures
  • composite maintenance and repair
  • hygrothermal aging
  • composite joints
  • extreme environment

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Published Papers (1 paper)

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Research

13 pages, 12736 KB  
Article
Study on the Dynamic Mechanical Behavior of 2D C/SiC Composites at Medium Strain Rates
by Xinyue Zhang, Chao Zhang, Xiaochuan Liu, Chunyu Bai, Xulong Xi and Xiaocheng Li
Aerospace 2026, 13(2), 168; https://doi.org/10.3390/aerospace13020168 - 10 Feb 2026
Viewed by 298
Abstract
Two-dimensional C/SiC are promising candidates for use in high-temperature structures in aeroengines and thermal protection systems in the aerospace industry, which will be subjected to loads in various directions during service. In this paper, the in-plane tensile, compressive, and shear mechanical properties of [...] Read more.
Two-dimensional C/SiC are promising candidates for use in high-temperature structures in aeroengines and thermal protection systems in the aerospace industry, which will be subjected to loads in various directions during service. In this paper, the in-plane tensile, compressive, and shear mechanical properties of 2D C/SiC were investigated over a strain-rate range of 10−5 s−1 to 10 s−1. The failure mechanisms of the material under different loading conditions were analyzed. The study reveals that 2D C/SiC exhibits nonlinear stress–strain relationships under tension and shear, while it displays a linear stress–strain relationship under compression similar to the quasi-static loading state. The strain-rate strengthening effect is most pronounced under compression, whereas the effect is less significant under tensile loading. The reason for the observed increase in strength is the additional energy consumed by multiple crack initiation and propagation. A rate-dependent constitutive model was fitted, which agrees well with the experimental data for both tensile and shear loading conditions. Full article
(This article belongs to the Special Issue Advanced Aircraft Composite Structure Design)
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