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: 10 February 2025 | Viewed by 1957

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

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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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Published Papers (2 papers)

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Research

37 pages, 4159 KiB  
Article
Runway Safety Assistant Foreseeing Excursions: Calculating Means
by Georgios Alogdianakis, Ioannis Katsidimas, Athanasios Kotzakolios, Anastasios Plioutsias and Vassilis Kostopoulos
Aerospace 2024, 11(9), 705; https://doi.org/10.3390/aerospace11090705 - 29 Aug 2024
Viewed by 610
Abstract
Runway Safety Assistant Foreseeing Excursions (RUNSAFE) is a complete embedded system solution, that predicts a potential runway overrun of a civil aviation aircraft during takeoff and landing. This work examines the feasibility of such a system, through the algorithms and computations that predict [...] Read more.
Runway Safety Assistant Foreseeing Excursions (RUNSAFE) is a complete embedded system solution, that predicts a potential runway overrun of a civil aviation aircraft during takeoff and landing. This work examines the feasibility of such a system, through the algorithms and computations that predict the overruns. The system executes both static and dynamic calculations, with the former being dependent on and the latter independent to the user’s inputs. Their outcomes and the runway’s length are compared in real time to assess if the process will end up in an overrun. All inputs are specifically selected to either be available to the pilots or be retrieved from the existing avionics systems of the cockpit. A performance evaluation is conducted on both static and dynamic calculations, and metrics unveil the accuracy of the predictions and the time needed to converge to a reliable result. The solution is adapted for a Boeing 737-800 aircraft with CFM56-7B engines, but the calculations also apply for similar aircraft equipped with tricycle landing gear and turbofan engines, namely the whole Boeing 737 family, the Airbus A320 family, etc. The system is aligned with current standards and certification specifications, where applicable. Full article
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35 pages, 17010 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 - 23 Jul 2024
Viewed by 783
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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