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Polymer Composites in Aerospace Applications

A special issue of Polymers (ISSN 2073-4360). This special issue belongs to the section "Polymer Applications".

Deadline for manuscript submissions: closed (5 April 2024) | Viewed by 6069

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Guest Editor
School of Materials and Chemistry, Southwest University of Science and Technology, Mianyang, China
Interests: mechanical properties of fibre resin matrix composites
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Special Issue Information

Dear Colleagues,

Polymer composites have many prominent advantages, including high specific strength and modulus, good thermal and chemical resistance, etc., and are, thus, gradually drawing attention for industrial aerospace applications. Fiber-reinforced polymer composites and fiber-metal laminated composites are major polymer composites used as alternative materials to replace heavy metal structures for lightweight design. High-performance development remains a focus for polymer composites in aerospace to ensure structural stability and safety in use; therefore, more novel reinforcement or design methods, including polymer matrix improvement, interlaminar toughening, and bonding interface design, are desirable and required to toughen the polymer composites.

The purpose of this Special Issue is to explore the most recent research articles and reviews on the design and analysis of polymer composites in aerospace applications. A special emphasis is placed on structure design, process methods, and complex mechanical mechanisms.

Dr. Fei Cheng
Guest Editor

Manuscript Submission Information

Manuscripts should be submitted online at www.mdpi.com by registering and logging in to this website. Once you are registered, click here to go to the submission form. Manuscripts can be submitted until the deadline. All submissions that pass pre-check are peer-reviewed. Accepted papers will be published continuously in the journal (as soon as accepted) and will be listed together on the special issue website. Research articles, review articles as well as short communications are invited. For planned papers, a title and short abstract (about 100 words) can be sent to the Editorial Office for announcement on this website.

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Please visit the Instructions for Authors page before submitting a manuscript. The Article Processing Charge (APC) for publication in this open access journal is 2700 CHF (Swiss Francs). Submitted papers should be well formatted and use good English. Authors may use MDPI's English editing service prior to publication or during author revisions.

Keywords

  • high-performance polymer composites
  • fiber-reinforced polymer composites
  • fiber-metal laminated composites
  • interlaminar toughening
  • interface design
  • mechanical behavior
 

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Published Papers (2 papers)

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12 pages, 3559 KiB  
Article
Growing Carbon Nanotubes In Situ Surrounding Carbon Fiber Surface via Chemical Vapor Deposition to Reinforce Flexural Strength of Carbon Fiber Composites
by Guangming Yang, Fei Cheng, Shihao Zuo, Jinheng Zhang, Yang Xu, Yunsen Hu and Xiaozhi Hu
Polymers 2023, 15(10), 2309; https://doi.org/10.3390/polym15102309 - 15 May 2023
Cited by 28 | Viewed by 2975 | Correction
Abstract
This study employed novel joint treatments to strengthen the carbon fiber reinforced polymer (CFRP) composites. Vertically aligned carbon nanotubes (VACNTs) were prepared in situ on the catalyst-treated CF surface via the chemical vapor deposition (CVD) method, intertwining into three-dimensional fiber-nets and fully surrounding [...] Read more.
This study employed novel joint treatments to strengthen the carbon fiber reinforced polymer (CFRP) composites. Vertically aligned carbon nanotubes (VACNTs) were prepared in situ on the catalyst-treated CF surface via the chemical vapor deposition (CVD) method, intertwining into three-dimensional fiber-nets and fully surrounding CF to form an integrated structure. The resin pre-coating (RPC) technique was further used to guide diluted epoxy resin (without hardener) to flow into nanoscale and submicron spaces to eliminate void defects at the root of VACNTs. Three-point bending testing results showed the “growing CNTs and RPC”-treated CFRP composites yielded the best flexural strength, a 27.1% improvement over the specimens without treatment, while the failure modes indicated that the original delamination failure was changed into “flexural failure” with through-the-thickness crack propagation. In brief, growing VACNTs and RPC on the CF surface enabled toughening of the epoxy adhesive layer, reducing potential void defects and constructing the integrated quasi-Z-directional fiber bridging at the CF/epoxy interface for stronger CFRP composites. Therefore, the joint treatments of growing VACNTs in situ via the CVD method and RPC technique are very effective and have great potential in manufacturing high-strength CFRP composites for aerospace applications. Full article
(This article belongs to the Special Issue Polymer Composites in Aerospace Applications)
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1 pages, 149 KiB  
Correction
Correction: Yang et al. Growing Carbon Nanotubes In Situ Surrounding Carbon Fiber Surface via Chemical Vapor Deposition to Reinforce Flexural Strength of Carbon Fiber Composites. Polymers 2023, 15, 2309
by Guangming Yang, Fei Cheng, Shihao Zuo, Jinheng Zhang, Yang Xu, Yunsen Hu and Xiaozhi Hu
Polymers 2023, 15(14), 3032; https://doi.org/10.3390/polym15143032 - 13 Jul 2023
Viewed by 2203
Abstract
In the original publication [...] Full article
(This article belongs to the Special Issue Polymer Composites in Aerospace Applications)
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