Instability and Transition of Compressible Flows
A special issue of Aerospace (ISSN 2226-4310). This special issue belongs to the section "Aeronautics".
Deadline for manuscript submissions: 28 February 2026 | Viewed by 405
Special Issue Editors
Interests: flow stability, transition, turbulence modes, and aerodynamic issues in aviation engineering; turbulence mode theory; turbulence numerical simulation and application
Special Issues, Collections and Topics in MDPI journals
Interests: high-speed flow stability and transition; nonlinear instability and mode–mode interaction; stability of shock wave/boundary layer interaction; transition control; direct numerical simulation
Interests: hypersonic aerodynamics; high temperature gasdynamics; heat transfer; computational fluid dynamics; experimental fluid dynamics
Special Issue Information
Dear Colleagues,
Currently, the stability and transition of compressible flows receives extensive attention due to its significance in understanding the aerodynamics of aircrafts. State-of-the-art approaches have been increasingly developing in theoretical, computational, and experimental aspects. New physics and insights have been identified in recent years regarding the regime of compressible flows. For this Special Issue of Aerospace, we invite review and research articles on the following topics:
- Stability and/or laminar–turbulent transition of the compressible boundary layer;
- Stability and/or laminar–turbulent transition of shock wave/boundary layer interaction;
- Stability and/or laminar–turbulent transition of shear layer and interfacial flow;
- Stability and/or laminar–turbulent transition of non-ideal flow;
- Stability and/or laminar–turbulent transition of the rarefied gas;
- Theoretical, computational, or experimental methods regarding compressible flow stability and/or transition;
- Aerodynamic performance considering flow stability and/or transition around vehicles;
- Transition modeling;
- All other research related to stability and/or transition of compressible flows.
We look forward to your submissions.
Prof. Dr. Song Fu
Dr. Peixu Guo
Dr. Guilai Han
Dr. Jie Ren
Guest Editors
Manuscript Submission Information
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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
- boundary layer stability and transition
- stability of shock wave/boundary layer interaction
- stability of compressible shear layer
- stability of compressible interfacial flow
- stability of non-ideal flow
- stability of rarefied gas
- methods for stability and transition
- transition modeling
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