3-Dnumerical simulation for supersonic hydrogen combustion was performed by solving the compressible Navier-Stokes equation and composition equations using implicit finite volume methods.Meanwhile
the effect of hydrogen injection pressure on combustion was analyzed and studied.The results show that
owing to the heat release from combustion and the influences of hydrogen's injection pressure
the flow field changes greatly
leading to enhanced streamwise vortex and stronger interaction between waves in the combustor and hydrogen flow
and also facilitating the mixing of hydrogen and air for improved hydrogen combustion performance.
3-D numerical investigation on supersonic combustion of hydrogen in two different type of scramjet combustors
Numerical study on flow field in three supersonic combustors
Effect of turbulent combustion model on simulation of hydrogen supersonic combustion
Applications of anisotropic unstructured mesh adaption insupersonic combustion simulations
Three-dimensional combustion numerical simulation of scramjet internal and external flow fields
Related Author
CHEN Mei-ning
LIU Zhao-shu
YANG Yang
XING Jian-wen
LE Jia-ling
WANG Jin-nuo
ZOU Jian-feng
SHENG Dong
Related Institution
Institute of Mechanical Engineering, Southwest Jiaotong University
China Aerodynamics Research and Development Center
School of Aeronautics and Astronautics, Zhejiang University
Research and Development Center, China Acedamy of Luanch Vehicle Technology, China Aerospace Science and Technology Corporation
Science and Technology on Scramjet Laboratory, Beijing Power Machinery Research Institute,the Third Research Academy, China Aerospace Science and Industry Corporation