@Article{AAMM-10-1261,
author = {Zhao , FamingWang , JiangfengFan , Xiaofeng and Yang , Tianpeng},
title = {Air Chemical Non-Equilibrium Effects on the Hypersonic Combustion Flow of RCS with Gaseous Ethylene Fuel},
journal = {Advances in Applied Mathematics and Mechanics},
year = {2018},
volume = {10},
number = {5},
pages = {1261--1278},
abstract = {<p style="text-align: justify;">In this paper, air chemical non-equilibrium effects on the shock-induced
combustion flow are numerically investigated for a reaction control system (RCS) with
gaseous ethylene fuel by solving multi-component Navier-Stokes (N-S) equations. An
integrated numerical method is developed that considers two different chemical reaction
mechanisms: the high temperature air chemical non-equilibrium reactions and
ethylene-oxygen combustion reactions. The method is independently validated by
two types of reacting flow: the hypersonic air chemical non-equilibrium flow over a
sphere and supersonic ethylene-oxygen combustion flow for a dual combustion chamber.
Furthermore, the mixed reacting flow over a blunt cone with a transverse multi-component
gaseous jet is analyzed in detail. Numerical results indicate that air chemical
non-equilibrium effects could lead to a reduction of the shock detachment distance,
a decrease of the temperature behind the shock wave and a reduction of the combustion
products.</p>},
issn = {2075-1354},
doi = {https://doi.org/10.4208/aamm.OA-2017-0321},
url = {http://global-sci.org/intro/article_detail/aamm/12598.html}
}