Volume 10, Issue 5
Air Chemical Non-Equilibrium Effects on the Hypersonic Combustion Flow of RCS with Gaseous Ethylene Fuel

Faming Zhao, Jiangfeng Wang, Xiaofeng Fan & Tianpeng Yang

Adv. Appl. Math. Mech., 10 (2018), pp. 1261-1278.

Published online: 2018-07

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  • Abstract

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 multicomponent 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.

  • Keywords

RCS ethylene-oxygen combustion air chemical non-equilibrium effects hypersonic

  • AMS Subject Headings

76D05 76K05 80A30

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COPYRIGHT: © Global Science Press

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@Article{AAMM-10-1261, author = {Faming Zhao, Jiangfeng Wang, Xiaofeng Fan and Tianpeng Yang}, 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 = {

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 multicomponent 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.

}, issn = {2075-1354}, doi = {https://doi.org/10.4208/aamm.OA-2017-0321}, url = {http://global-sci.org/intro/article_detail/aamm/12598.html} }
TY - JOUR T1 - Air Chemical Non-Equilibrium Effects on the Hypersonic Combustion Flow of RCS with Gaseous Ethylene Fuel AU - Faming Zhao, Jiangfeng Wang, Xiaofeng Fan & Tianpeng Yang JO - Advances in Applied Mathematics and Mechanics VL - 5 SP - 1261 EP - 1278 PY - 2018 DA - 2018/07 SN - 10 DO - http://dor.org/10.4208/aamm.OA-2017-0321 UR - https://global-sci.org/intro/aamm/12598.html KW - RCS KW - ethylene-oxygen combustion KW - air chemical non-equilibrium effects KW - hypersonic AB -

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 multicomponent 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.

Faming Zhao, Jiangfeng Wang, Xiaofeng Fan & Tianpeng Yang. (1970). Air Chemical Non-Equilibrium Effects on the Hypersonic Combustion Flow of RCS with Gaseous Ethylene Fuel. Advances in Applied Mathematics and Mechanics. 10 (5). 1261-1278. doi:10.4208/aamm.OA-2017-0321
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