Numerical Study of Chemical Non-equilibrium Flow in Hydrocarbon Scramjet Nozzle
- 10.2991/mems.2012.184How to use a DOI?
- scramjet nozzle; chemical non-equilibrium effects; nozzle performance
The non-equilibrium flow and frozen flow of hydrocarbon scramjet nozzle were numerically simulated to research the non-equilibrium effects on the nozzle performance. The numerical results show the recombination occurs during the expansion in the scramjet nozzle, which is helpful to the nozzle performance. The calculation results suggest the influence of the inlet mach and the fuel equivalence ratio to the non-equilibrium effects on nozzle performance is visible.
- © 2012, 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 - ZHANG Xiao-yuan AU - QIN Li-zi AU - LIU Yu PY - 2012/12 DA - 2012/12 TI - Numerical Study of Chemical Non-equilibrium Flow in Hydrocarbon Scramjet Nozzle BT - Proceedings of the 1st International Conference on Mechanical Engineering and Material Science (MEMS 2012) PB - Atlantis Press SP - 702 EP - 705 SN - 1951-6851 UR - https://doi.org/10.2991/mems.2012.184 DO - 10.2991/mems.2012.184 ID - Xiao-yuan2012/12 ER -