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西北工业大学 国内
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Influence of hydrogen equivalence ratios on supersonic combustion based on large eddy simulations
Bing Liu
, Jia chen Xu,
Fei Qin
,
Guo qiang He
, Duo Zhang, Lei Shi
航天学院
Northwestern Polytechnical University Xian
科研成果
:
期刊稿件
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同行评审
16
引用 （Scopus）
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探究 'Influence of hydrogen equivalence ratios on supersonic combustion based on large eddy simulations' 的科研主题。它们共同构成独一无二的指纹。
分类
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Engineering
Supersonic Combustion
100%
Equivalence Ratio
100%
Heat Release Rate
50%
Flow Distribution
33%
Autoignition
33%
Mach Number
16%
Simulation Result
16%
Good Agreement
16%
Realization
16%
Combustor
16%
Boundary Layer
16%
Numerical Method
16%
Specific Impulse
16%
Combustion Chamber
16%
Propulsion System
16%
Wall-Pressure
16%
Supersonic Flow
16%
Hypersonic Flows
16%
Combustion Mode
16%
Shockwave
16%
Material Science
Large Eddy Simulation
100%
Boundary Layer
50%
Hypersonic Flows
50%
Supersonic Flow
50%
Mach Number
50%
Physics
Spontaneous Combustion
50%