Advances in Detonative Propulsion
A special issue of Aerospace (ISSN 2226-4310).
Deadline for manuscript submissions: closed (15 July 2024) | Viewed by 7295
Special Issue Editors
Interests: oblique detonation engine; detonative propulsion; supersonic combustion; scramjets; high-enthalpy shock tunnel; high-temperature gasdynamics; hypersonic aerodynamics and aerothermal dynamics
Interests: gasdynamics; shock waves; aerodynamic designs; oblique detonation
Interests: hypersonic air-breathing propulsion; detonation; supersonic combustion; high-speed multiphase flow; supersonic/hypersonic wind-tunnel experiment
Special Issue Information
Dear Colleagues,
Detonative propulsion represents the new generation of hypersonic propulsion techniques. Research in its field is booming and many advances have been made globally in recent years. The aim of this Special Issue is to publish these cutting-edge research results to promote the development of detonative propulsion and the cooperation of researchers in this field.
The topics for this Special Issue are broad, including (but not limited to)
- oblique detonation engines,
- rotating detonation engines,
- pulsed detonation engines,
- propulsive performance analysis of detonation engines,
- the fundamental physics of gaseous detonation and multiphase detonation,
- the design of detonation engines,
- and all other research related to detonative propulsion techniques.
We invite authors to contribute new research results to this Special Issue.
Dr. Yunfeng Liu
Prof. Dr. Yancheng You
Dr. Zijian Zhang
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 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
- oblique detonation engine
- rotating detonation engine
- pulsed detonation engine
- propulsive performance analysis
- gaseous detonation
- multiphase detonation
