Supersonic Fluid Flow Process and Its Control Methods
A special issue of Processes (ISSN 2227-9717). This special issue belongs to the section "Process Control and Monitoring".
Deadline for manuscript submissions: 31 December 2024 | Viewed by 208
Special Issue Editors
Interests: compressible flow; supersonic internal flow; shock wave/boundary layer interaction; flow mechanism; flow control
Special Issue Information
Dear Colleagues,
Supersonic fluid flow refers to the phenomenon of fluid flowing at a speed exceeding the local speed of sound. Different from subsonic flow, complex phenomenon of shock wave/boundary layer interaction occurs during the flow of supersonic fluid. Shock wave, as a type of highly discontinuous flow field, cause abrupt changes in density, temperature, and velocity in the flow field before and after the shock. The boundary layer along the wall, as a typical low-speed shear layer, also exhibits significant variations in physical quantities along the normal direction to the wall. Both of them are gradient fields of physical quantities, but their strengths and directions of effects are different. It is precisely because of these similarities and differences between shock wave and boundary layer that the interaction between them becomes exceptionally complex. It is a key and challenging issue that must be considered in aircraft design. The related research involves fundamental issues such as high-speed aerodynamics, flow stability, transition, separation, turbulence, and flow control. It belongs to the forefront of aerodynamics research.
Based on this, it is planned to create a Special Issue on “Supersonic fluid flow process and its control methods”. Through this, the aim is to enhance the understanding of the flow mechanism of supersonic fluid flow process, develop flow control methods to improve the flow field quality, and promote the improvement of aerodynamic performance of air-breathing hypersonic vehicles. This Special Issue focuses on the shock wave/boundary layer interaction, shock wave/vortex coupling interference, supersonic turbulent flow for chemical equilibrium, flow controlled supersonic flow, supersonic rocket nozzle flow, and other areas.
The topics of the Special Issue include, but are not limited to:
- Shock wave/boundary layer interaction
- Shock wave/vortex coupling interference
- Supersonic turbulent flow for chemical equilibrium
- Flow controlled supersonic flow
- Supersonic rocket nozzle flow
- Supersonic impinging jet flow
- Shock wave aerothermal and drag reduction
- Shock wave/combustion interaction
- Flow control methods
- Wind tunnel experimental methods
- Numerical calculation methods
Dr. Ziao Wang
Dr. Nan 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 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. Processes 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
- shock wave/boundary layer interaction
- shock wave/vortex coupling interference
- supersonic turbulent flow for chemical equilibrium
- flow controlled supersonic flow
- supersonic rocket nozzle flow
- supersonic impinging jet flow
- shock wave aerothermal and drag reduction
- shock wave/combustion interaction
- flow control methods
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.
