Composite Materials and Aircraft Structural Design

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

Deadline for manuscript submissions: 20 December 2025 | Viewed by 757

Special Issue Editor


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Guest Editor
Faculty of Technology, Amsterdam University of Applied Sciences, 1091 GC Amsterdam, The Netherlands
Interests: aircraft/automobile structural design

Special Issue Information

Dear Colleagues,

Structural and material innovations are inherent parts of the future aviation industry, especially when approaching the defined goals for zero emissions and more sustainable flights. Composite and hybrid materials have proven to possess exceptional properties such as low weight, high strength, and reliable damage tolerance. However, they need to comply with the novel and advanced designs of aircrafts. As we move toward more environmentally friendly designs, advancements in properties and structural design of such components are necessary. This may include the use of thermoset-based and thermoplastic-based composites and fiber–metal laminates. For instance, clean aviation requires hydrogen tanks to be carried in the aeroplane, which needs support from composite tanks to carry the loads. Additionally, recyclability and biodegradability are becoming more favorable in different industries to achieve a more sustainable design-manufacturing process. Therefore, new procedures for modeling such innovative material concepts are welcome for this Special Issue, especially if supported by experimental characterizations and validations. Furthermore, investigations on the feasibility of innovative composites and hybrid materials will enrich the current Special Issue. Novel aircraft configurations for clean aviation purposes are are also welcome for submission to this Special Issue (e.g., novel configurations accommodating hydrogen and electric powered commercial aircrafts targeting climate neutral aviation).

I look forward to your submissions.

Dr. Morteza Abouhamzeh
Guest Editor

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Keywords

  • aircraft design
  • aviation/aeronautical
  • composite, hybrid
  • biomaterials
  • optimization
  • novel aircraft structures
  • functional composites
  • modeling
  • optimizations

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Published Papers (1 paper)

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Research

22 pages, 8402 KB  
Article
Analysis of the Compressive Buckling and Post-Buckling Behaviour of Wood-Based Sandwich Panels Used in Light Aviation
by Hajer Hadiji, Joel Serra, Remi Curti and Bruno Castanié
Aerospace 2025, 12(9), 782; https://doi.org/10.3390/aerospace12090782 - 29 Aug 2025
Viewed by 481
Abstract
This work aims to investigate the buckling and post-buckling behaviour of wood-based sandwich structures with and without a manufacturing defect, under compressive loading. The specimens were made by gluing birch veneers to a balsa wood core. The defect consisted of a central zone [...] Read more.
This work aims to investigate the buckling and post-buckling behaviour of wood-based sandwich structures with and without a manufacturing defect, under compressive loading. The specimens were made by gluing birch veneers to a balsa wood core. The defect consisted of a central zone where glue was lacking between the skin and the core. A compression load was applied to the plate using the VERTEX test rig, with the plate placed on the upper surface of a rectangular box and bolted at its borders. The upper surface of the plate was monitored using optical and infrared cameras. The stereo digital image correlation method was used to capture the in-plane and out-of-plane deformations of the specimen, and to calculate the strains and stresses. The infrared camera enabled the failure scenario to be identified. The buckling behaviour of pristine specimens showed small local debonding in the post-buckling range, which was not detrimental to overall performance. In the presence of a manufacturing defect, the decrease in buckling load was only about 15%, but final failure occurred at lower compressive loads. Full article
(This article belongs to the Special Issue Composite Materials and Aircraft Structural Design)
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