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Flow, Combustion, and Thermal-Structure of Advanced Aerospace Propulsion
This special issue belongs to the section “J: Thermal Management“.
Special Issue Information
Dear Colleagues,
Advanced aerospace propulsion systems, such as turbofan engines and rocket engines, form the foundation of aerospace transportation in modern society. However, beyond the traditional fields of aviation and space transportation, new demands such as green aviation, urban air mobility, sub-orbital flight, etc., have given rise to new requirements for advanced aerospace propulsion systems. To meet these emerging needs, the field of aerospace propulsion needs to develop innovative, advanced propulsion concepts, including aspects related to the working processes of propulsion systems such as fluid flow, combustion and structure design.
This Special Issue aims to highlight the most recent advances related to the concept, design, modeling, application and the flow, combustion and structure of all types of advanced aerospace propulsion systems.
Topics of interest include, but are not limited to, the following research areas:
- Advancement in traditional aviation engines like turbofan, turboprop or turboshaft engines, etc.;
- Electric or hybrid propulsion systems;
- Variable cycle engines;
- Combined cycles like TBCC, RBCC, SABRE, etc.;
- Other new aerospace propulsion systems;
- Propulsion system design, modeling, simulation, control and application analysis;
- Combustion organization and simulation of aerospace engines;
- Flow control, simulation and resistance reduction in aerospace engines;
- Structure cooling and design of aerospace engines.
Dr. Xuanfei Yu
Dr. Duo Zhang
Dr. Wenqiang Li
Guest 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 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. Energies is an international peer-reviewed open access semimonthly 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 2600 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
- aerospace propulsion
- modeling
- flow
- combustion
- structure
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