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 355

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 SO17 1BJ, UK
Interests: aerodynamics; fluid mechanics; structural dynamics; numerical analysis; cfd simulation; finite element analysis; computational fluid dynamics; numerical simulation; modeling and simulation; engineering thermodynamics
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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

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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 (1 paper)

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Research

35 pages, 17019 KiB  
Article
Flow-Based Assessment of the Impact of an All-Electric Aircraft on European Air Traffic
by Bekir Yildiz, Peter Förster, Thomas Feuerle and Peter Hecker
Aerospace 2024, 11(8), 602; https://doi.org/10.3390/aerospace11080602 (registering DOI) - 23 Jul 2024
Abstract
The consequences of new airspace entrants, such as novel aircraft concepts with innovative propulsion systems, on air traffic management operations need to be carefully identified. This paper aims to assess the impact of future aircraft with different performance envelopes on the European air [...] Read more.
The consequences of new airspace entrants, such as novel aircraft concepts with innovative propulsion systems, on air traffic management operations need to be carefully identified. This paper aims to assess the impact of future aircraft with different performance envelopes on the European air traffic network from a flow-based perspective. The underlying approach assumes that all certification-related questions concerning airworthiness have been resolved and do not take into account any economic factors related to airline operations. For example, for an innovative propulsion system, a short range all-electric aircraft is considered in this study. Aircraft trajectory calculations are based on the dataset of base of aircraft data (BADA), which are developed and maintained by EUROCONTROL. The new design concept is integrated into BADA as well, resulting in a new set of coefficients for the all-electric aircraft. In addition to the adjusted parameters which affect airborne performances, ground-related aspects are also taken into account. This includes assumptions on operational procedures, charging capacities and adaptions in infrastructure. Investigations are carried out at the trajectory level as well as at the airport and the entire network. Full article
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