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Advances in Aerostructural Analysis, Design, and Optimization

A special issue of Applied Sciences (ISSN 2076-3417). This special issue belongs to the section "Aerospace Science and Engineering".

Deadline for manuscript submissions: closed (20 November 2025) | Viewed by 1060

Special Issue Editors


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Guest Editor
Adaptive Structures Operative Unit, The Italian Aerospace Research Centre (CIRA), 81043 Capua, Italy
Interests: aerostructural analysis; aeroelasticity; morphing systems; design optimization; adaptive structures
Special Issues, Collections and Topics in MDPI journals

Special Issue Information

Dear Colleagues,

This Special Issue, entitled “Advances in Aerostructural Analysis, Design, and Optimization”, aims to contribute to the progression of aerostructural engineering by addressing critical challenges and innovations in the analysis, design, and optimization of aerospace structures. These advancements are essential to improve performance, reduce costs, and enhance sustainability in the aerospace sector. The integration of advanced computational techniques, aeroelastic tailoring, novel materials, and optimization strategies has enabled significant progress in aerostructural design. However, further research is required to address complex issues such as multidisciplinary optimization and the incorporation of emerging technologies like morphing systems. This collection seeks to explore these topics while also emphasizing practical applications across the aerospace industry.

We invite contributions that span a wide range of topics including, but not limited to, the following:

  • Advanced computational methods for aerostructural analysis;
  • Aeroelastic tailored design for flutter mitigation;
  • Multidisciplinary design optimization (MDO) techniques;
  • The integration of novel materials into aerostructures;
  • Machine learning applications in aerostructural analysis and optimization;
  • Morphing systems.

This Special Issue aims to provide a platform for experimental, numerical, and theoretical studies that advance the state-of-the-art in aerostructural engineering. By bringing together researchers from academia and industry, we hope to foster collaboration and innovation in this critical field.

We welcome original research articles, review papers, and case studies that align with these themes.

Dr. Maria Noviello
Dr. Rosario Pecora
Guest Editors

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 250 words) can be sent to the Editorial Office for assessment.

Submitted manuscripts should not have been published previously, nor be under consideration for publication elsewhere (except conference proceedings papers). All manuscripts are thoroughly refereed through a single-blind peer-review process. A guide for authors and other relevant information for submission of manuscripts is available on the Instructions for Authors page. Applied Sciences is an international peer-reviewed open access semimonthly journal published by MDPI.

Please visit the Instructions for Authors page before submitting a manuscript. The Article Processing Charge (APC) for publication in this open access journal is 2400 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

  • aerostructural analysis
  • aeroelastic tailoring
  • multidisciplinary design optimization
  • aerostructural design
  • morphing systems

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Published Papers (1 paper)

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Research

28 pages, 60690 KB  
Article
A Modeling Approach for Assessing Vibration Immunity in Hydrogen Fuel Cell Stack for Aeronautical Applications
by Giovanni Fasulo, Simone Gallas, Hervé Denayer, Oskar Ekblad, Giancarlo Kosova and Mattia Barbarino
Appl. Sci. 2026, 16(1), 69; https://doi.org/10.3390/app16010069 - 20 Dec 2025
Viewed by 695
Abstract
Fuel cells offer a promising route to eliminating in-flight emissions from regional aviation, but certification requires proof that stacks can withstand the vibration and shock environment of turboprop aircraft. As part of the EU-funded NEWBORN project, we combined detailed finite element modeling with [...] Read more.
Fuel cells offer a promising route to eliminating in-flight emissions from regional aviation, but certification requires proof that stacks can withstand the vibration and shock environment of turboprop aircraft. As part of the EU-funded NEWBORN project, we combined detailed finite element modeling with shaker tests to evaluate the vibration immunity of PowerCell Group’s prototype stack. The numerical model combined an orthotropic, two-zone 3D mesh of the cell package with reduced-order representations of plates, compression bands, disc springs and the mounting cage. The assembled stack was excited between 10 and 300 Hz using pseudo-random and sine-sweep inputs up to 2.0 g, from which 54 frequency response functions were obtained. The tuned model accurately reproduced the first global modes and captured the overall dynamic behavior with good, though not perfect, agreement. The combined numerical–experimental methodology therefore offers a framework for refining test campaigns and delivering early, qualitative evidence of vibration immunity in fuel cell stacks destined for flight. Full article
(This article belongs to the Special Issue Advances in Aerostructural Analysis, Design, and Optimization)
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