Flow and Heat Transfer in Solid Rocket Motors
A special issue of Aerospace (ISSN 2226-4310). This special issue belongs to the section "Astronautics & Space Science".
Deadline for manuscript submissions: 31 December 2025 | Viewed by 135
Special Issue Editor
Special Issue Information
Dear Colleagues,
Due to various advantages, such as their inherent simplicity, high reliability, and quick responses, solid rocket motors (SRMs) play an important role in space launch vehicles. As their performance can be enhanced through the fundamental mechanisms of their complex flow and heat transfer physics, there is growing interest in the issues encountered in these areas.
Indeed, an understanding of complex flow and heat transfer mechanisms, multiphase flow dynamics, and the ablation mechanism of the adiabatic layer are all technical challenges still to be faced in advanced SRM design. Building on this vision, this Special Issue aims to provide an overview of the most recent advances in the field of the flow and heat transfer of SRMs. Potential topics include, but are not limited to, complex flow and heat transfer, ablation mechanisms, multiphase flow modeling, metal droplet behavior, the prediction of SRM performance, the design of combustion chambers and nozzles, and combustion modeling.
Prof. Dr. Yang Liu
Guest Editor
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
- solid rocket motor
- complex flow and heat transfer
- ablation mechanism
- insulator
- multiphase flow modeling
- metal droplet behavior
- design of combustion chamber and nozzle
- combustion modeling
- prediction of performance
Benefits of Publishing in a Special Issue
- Ease of navigation: Grouping papers by topic helps scholars navigate broad scope journals more efficiently.
- Greater discoverability: Special Issues support the reach and impact of scientific research. Articles in Special Issues are more discoverable and cited more frequently.
- Expansion of research network: Special Issues facilitate connections among authors, fostering scientific collaborations.
- External promotion: Articles in Special Issues are often promoted through the journal's social media, increasing their visibility.
- e-Book format: Special Issues with more than 10 articles can be published as dedicated e-books, ensuring wide and rapid dissemination.
Further information on MDPI's Special Issue polices can be found here.
