Aviation Sustainability

A special issue of Aerospace (ISSN 2226-4310). This special issue belongs to the section "Air Traffic and Transportation".

Deadline for manuscript submissions: closed (30 June 2022) | Viewed by 12958

Special Issue Editors


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Collection Editor
Faculty of Aeronautics and Astronautics, Eskisehir Technical University, 2 Eylul Campus, 26470 Eskisehir, Turkey
Interests: aircraft engine; airports; energy; environment

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Collection Editor
Suleyman Demirel University, School of Civil Aviation, Department of Airframe and Powerplant Maintenance, Isparta, Turkey
Interests: gas turbine engine measurements; combustion and fuels; energy and exergy analyses of thermal systems; sustainable aviation; aviation and environment

Special Issue Information

Dear Colleagues,

To use existing resources effectively in the future, a basic understanding of sustainability should be included in R&D. Although sustainability is examined under the three main pillars of economic, environmental, and social, these three parameters should be examined in an integrated manner.

In the first years of aviation research, only studies on system performance and improvement were carried out. Then, energy-efficient system designs and applications were carried out. In recent decades, economic and environmentally friendly aviation applications have emerged as research topics. Aviation applications can be divided into two subgroups, airside and landside. While the effects of aircraft can be examined separately both on the airside and on the landside, airport studies can be limited to landside applications. To achieve sustainable aviation, we need to carry out aviation studies on environmentally friendly (e.g., producing low emission, carbon neutral), respecting equalities (e.g.; genetics, gender, disability), ecosystem friendly (protecting biodiversity), and using alternative sources (e.g., electricity–heating–cooling with solar, wind, heat pump).

This journal is inviting work concerning sustainable aviation studies. In particular, the collection will focus on eco-friendly aircraft engines, sustainable aircraft materials, aircraft life cycle analysis, alternative energy sources for aircraft, propulsion analysis (e.g., sub-sonic, hypersonic), more electrical aircraft, airport sustainability (e.g, science and social applications), and sustainable airport management (e.g., energy, noise, environmental).

Prof. Dr. Onder Altuntas 
Prof. Dr. Yasin Şöhret
Collection 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

  • Eco-friendly aircraft engine
  • aircraft life cycle analysis
  • airport sustainability

Published Papers (2 papers)

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Research

19 pages, 3394 KiB  
Article
Feasibility Study of Electrified Light-Sport Aircraft Powertrains
by Madeline McQueen, Ahmet E. Karataş, Götz Bramesfeld, Eda Demir and Osvaldo Arenas
Aerospace 2022, 9(4), 224; https://0-doi-org.brum.beds.ac.uk/10.3390/aerospace9040224 - 17 Apr 2022
Cited by 3 | Viewed by 2694
Abstract
A theory-based aerodynamic model developed and applied to electrified powertrain configurations was intended to analyze the feasibility of implementing fully electric and serial hybrid electric propulsion in light-sport aircraft. The range was selected as the primary indicator of feasibility. A MATLAB/Simulink environment was [...] Read more.
A theory-based aerodynamic model developed and applied to electrified powertrain configurations was intended to analyze the feasibility of implementing fully electric and serial hybrid electric propulsion in light-sport aircraft. The range was selected as the primary indicator of feasibility. A MATLAB/Simulink environment was utilized to create the models, involving the combination of proportional-integral-derivative controllers, aerodynamic properties of a reference aircraft, and powertrain limitations taken from off-the-shelf components. Simulations conducted by varying missions, batteries, fuel mass, and energy distribution methods provided results showcasing the feasibility of electrified propulsion with current technology. Results showed that the fully electric aircraft range was only 5% of a traditionally powered aircraft with current battery technology. Hybrid electric aircraft could achieve 44% of the range of a traditionally powered aircraft, but this result was found to be almost wholly related to fuel mass. Hybrid electric powertrains utilizing an energy distribution with their optimal degree of hybridization can achieve ranges up to 3% more than the same powertrain utilizing a different energy distribution. Results suggest that improvements in the power-to-weight ratio of the existing battery technology are required before electrified propulsion becomes a contender in the light-sport aircraft segment. Full article
(This article belongs to the Special Issue Aviation Sustainability)
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24 pages, 94378 KiB  
Article
Accuracy of Noise-Power-Distance Definition on Results of Single Aircraft Noise Event Calculation
by Oleksandr Zaporozhets and Larisa Levchenko
Aerospace 2021, 8(5), 121; https://0-doi-org.brum.beds.ac.uk/10.3390/aerospace8050121 - 21 Apr 2021
Cited by 5 | Viewed by 4292
Abstract
Aircraft performance and noise database together with operational weights (depending on flight distances) and operational procedures (including low noise procedures) significantly influence results of noise exposure contour maps assessment in conditions of real atmosphere. Current recommendations of the Standard SAE-AIR1845A allow the definition [...] Read more.
Aircraft performance and noise database together with operational weights (depending on flight distances) and operational procedures (including low noise procedures) significantly influence results of noise exposure contour maps assessment in conditions of real atmosphere. Current recommendations of the Standard SAE-AIR1845A allow the definition of flight profiles via solutions of balanced motion equations. However, differences are still supervised between the measured sound level data and calculated ones, especially in assessing the single flight noise events. Some of them are well explained by differences between balanced flight parameters (thrust and velocity first of all) and monitored ones by the traffic control system. Statistical data were gathered to make more general view on these differences and some proposal to use them in calculations has been proven. Besides, the real meteorological parameters provide inhomogeneous atmosphere conditions always, which are quite different from the main assumptions of the SAE-AIR1845A, stipulating inaccuracies of sound level calculations. Full article
(This article belongs to the Special Issue Aviation Sustainability)
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