Gnani, F., Zare-Behtash, H. , White, C. and Kontis, K. (2019) Shock Train Structures in Rectangular Ducts. In: 31st International Symposium on Shock Waves, Nagoya, Japan, 09-14 Jul 2017, pp. 769-776. ISBN 9783319910161 (doi: 10.1007/978-3-319-91017-8_96)
Full text not currently available from Enlighten.
Abstract
The deceleration of a supersonic flow to subsonic velocity inside a high-speed engine occurs through a series of shock waves, known as a shock train. The generation of such a flow structure is due to the interaction between the shock waves and the boundary layer inside a long duct. This phenomenon is frequently encountered in a variety of internal flow fields where a shock wave interacts with the boundary layer including air-breathing engines, high-speed wind tunnel diffusers, and supersonic compressors and ejectors. The present study investigates the complex SBLI phenomenon encountered in a Mach 2 shock train through numerical analysis.
| Item Type: | Conference Proceedings |
|---|---|
| Status: | Published |
| Refereed: | Yes |
| Glasgow Author(s) Enlighten ID: | Gnani, Francesca and Zare-Behtash, Dr Hossein and White, Dr Craig and Kontis, Professor Konstantinos |
| Authors: | Gnani, F., Zare-Behtash, H., White, C., and Kontis, K. |
| Subjects: | Q Science > Q Science (General) Q Science > QC Physics T Technology > T Technology (General) |
| College/School: | College of Science and Engineering > School of Engineering > Autonomous Systems and Connectivity |
| ISBN: | 9783319910161 |
| Published Online: | 03 April 2019 |
University Staff: Request a correction | Enlighten Editors: Update this record
Deposit and Record Details
Deposit and Record Details