Overall Aircraft Design for New Airframe Technologies, New Energy Systems and New Operations

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

Deadline for manuscript submissions: 20 October 2024 | Viewed by 147

Special Issue Editors


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Guest Editor
School of Aeronautics and Astronautics, Zhejiang University, Hangzhou 310058, China
Interests: overall aircraft design; multidisciplinary design analysis and optimization (MDAO); electric vertical takeoff and landing (eVTOL) aircraft; high-speed aircraft; hybrid electric propulsion

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Guest Editor
School of Aeronautic Science and Engineering, Beihang University, Beijing 100191, China
Interests: aircraft conceptual design; model-based systems engineering; systems of systems engineering; digital collaboration; big data

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Guest Editor
Faculty of Engineering and Physical Sciences, University of Southampton, Southampton SO171BJ, UK
Interests: aerodynamics; structures; aeroelasticity; model reduction; control
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Special Issue Information

Dear Colleagues,

In order to achieve aviation carbon emission goals, traditional airframe technologies, energy systems, and operation strategies (ATEO) are no longer sufficient to meet the evolving demands of future aircraft. Radically novel ATEOs present great potential for reducing aviation carbon emissions but also pose numerous challenges. In the context of a growing focus on electric vertical takeoff and landing (eVTOL) aircraft for urban air mobility, a resurgence of interest in civil high-speed flight, and the increasing consensus on achieving net-zero aviation carbon emissions by 2050, this Special Issue aims to collect the latest research work in aircraft design related to ATEO, such as laminar flow control, variable camber, boundary layer ingestion for airframe technologies, lithium batteries, sustainable aviation fuels (SAF), methane, and hydrogen for energy storage systems, as well as fuel cells and electric motors for energy conversion systems, and operation strategies like formation flight (cooperative trajectories), intermediate-stop refueling, continuous climb/descent.

This Special Issue welcomes potential topics, including but not limited to:

  1. EVTOL aircraft design and optimization;
  2. Civil high-speed aircraft design and optimization;
  3. Aircraft design case studies on new configurations;
  4. Aircraft technology integration (e.g., laminar flow control, boundary layer ingestion, advanced composite materials);
  5. Evaluation of new energy systems for aircraft (e.g., hybrid electric propulsion, hydrogen with fuel cells);
  6. Assessment of operational strategies for aircraft (e.g., formation flight, trajectory optimization);
  7. Aviation emission reduction strategies, including case studies and reviews;
  8. Multidisciplinary design analysis and optimization, incorporating disciplinary methods and/or optimization strategies;
  9. Digital and model-based design approaches for new configurations;
  10. New aircraft design methods, tools, and frameworks (e.g., machine-learning-based approaches).

Dr. Yaolong Liu
Dr. Mingqiang Luo
Dr. Andrea Da-Ronch
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 100 words) can be sent to the Editorial Office for announcement on this website.

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. Aerospace is an international peer-reviewed open access monthly 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

  • overall aircraft design
  • aircraft technology integration
  • EVTOL
  • MDAO (Multidisciplinary Design Analysis and Optimization)
  • MBSE (Model-Based Systems Engineering)
  • hybrid electric propulsion
  • laminar flow control
  • formation flight
  • trajectory optimization

Published Papers

This special issue is now open for submission.
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