Special Issue "Electric Aircraft"
A special issue of Aerospace (ISSN 2226-4310).
Deadline for manuscript submissions: 30 April 2018
Dr. Ranjan Vepa
Senior Lecturer in Aerospace Engineering, Division of Engineering Science, School of Engineering and Material Science, Queen Mary, University of London, 327 Mile End Road, London E1 4NS, UK
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Phone: +44 (0)20 7882 5193
Fax: +44 (0)20 7882 5532
Interests: Dynamics and Control of Electric Aircraft; Aerospace Vehicles; Robotics; UAVs & Energy Systems
Ever-increasing energy demand and rising fuel prices have motivated aircraft industries to develop alternative power sources for future aircraft. In the aviation sector, the requirements of flight reliability, low noise-emission levels, reduction in the dependence on fossil fuels, requirements of lower costs and lower weight, and longer life cycles, increase the complexity of the overall system and lead manufacturers to introduce major breakthroughs and innovations. Hybrid electric propulsion and all-electric propulsion for future aircraft are currently popular fields in the aircraft industry and are forming the basis for future commercial aircraft designs. Hybrid electric propulsion systems are composed of a networked set of gas turbines and batteries, while in all electric propulsion systems batteries are the only source of propulsive power on aircraft. Current battery technologies pose the most serious limitations to the development of all-electric and more-electric aircraft. However, rapid strides are being made in the evolution of battery technology and, for this reason, most aircraft industries are planning to introduce either more-electric or all-electric powered aircraft within the next two decades. Electric aircraft will pose new problems related to the general aircraft architecture, geometry and shape, battery, motor, and propulsion system design, aerodynamics, drag reduction and boundary layer control, aircraft performance, stability and control, the design of flight controllers, optimum structural design, and a host of other issues. In this Special Issue, we hope bring together a number of current aspects of electric aircraft that are being extensively researched within the aerospace community.
Dr. Ranjan Vepa
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 papers will be 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 quarterly journal published by MDPI.
Please visit the Instructions for Authors page before submitting a manuscript. The Article Processing Charge (APC) is waived for well-prepared manuscripts submitted to this issue. 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.
- Electric Aircraft
- Electric Propulsion
- Metal Air Batteries
- Battery Simulation
- State of Charge Estimation
- High Temperature Superconductors (HTS)
- HTS Electric Machines
- All Electric Propulsion
- Hybrid Electric Propulsion
- Distributed Electric Propulsion
- Dynamics and Control
- Fault Tolerant Control