Fluid Dynamic Analysis on the Adaptive Slot Method of Hypersonic Inlets
- https://doi.org/10.2991/msam-17.2017.32How to use a DOI?
- adaptive slot; hypersonic inlet; starting ability; restart; separation
To enhance the starting ability was one of the most serious issues in air propulsion system. In the present work, an adaptive slot control method was proposed to expand the working range of hypersonic inlets to a lower Mach number with weak losses, which was beneficial for engineering applications. Simulation results indicated that the starting Mach number can be decreased from 3.2 to 3.0 with five parallel slots at a width of 4mm. The flow inside the slot channel was self-driven due to the pressure gradient across of the separation shock. In case that the inlet was restart, the slot channel flow would be strongly suppressed.
- © 2017, the Authors. Published by Atlantis Press.
- Open Access
- This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).
Cite this article
TY - CONF AU - Chengxiang Zhu AU - Yancheng You PY - 2017/03 DA - 2017/03 TI - Fluid Dynamic Analysis on the Adaptive Slot Method of Hypersonic Inlets BT - Proceedings of the 2017 2nd International Conference on Modelling, Simulation and Applied Mathematics (MSAM2017) PB - Atlantis Press SP - 143 EP - 146 SN - 1951-6851 UR - https://doi.org/10.2991/msam-17.2017.32 DO - https://doi.org/10.2991/msam-17.2017.32 ID - Zhu2017/03 ER -