Overall Aircraft Design for New Airframe Technologies, New Energy Systems, and New Operations—2nd Edition

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

Deadline for manuscript submissions: 30 June 2026 | Viewed by 32

Special Issue Editor


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Guest Editor
School of Aeronautics and Astronautics, Zhejiang University, Hangzhou 310018, 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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Special Issue Information

Dear Colleagues,

In order to achieve carbon emission goals in the aviation sector, traditional airframe technologies, energy systems, and operation strategies (ATEOs) are no longer able to meet the evolving demands made of future aircraft. Radically new ATEOs present great potential in terms of 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 gather together the latest research on aircraft design pertaining to ATEOs, such as laminar flow control, variable camber, boundary-layer ingestion for airframe technologies, lithium batteries, sustainable aviation fuels (SAFs), 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 refueling, and continuous climb/descent.

This Special Issue welcomes contributions on areas of interest that include, but are not limited to, the following:

  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, and advanced composite materials);
  5. Evaluation of new energy systems for aircraft (e.g., hybrid electric propulsion and hydrogen fuel cells);
  6. Assessment of operational strategies for aircraft (e.g., formation flight and 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
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 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. 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

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