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Knowledge Management System of Institue of Mechanics, CAS
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Funding Organization:Fund of Key Laboratory of Defense Science and Technology
Funding Organization:National Natural Science Foundation of China
Funding Project:National Key Research and Development Program of Chinahttp://dx.doi.org/10.13039/501100012166[2021YFA0719204]
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Nonequilibrium Heating/Cooling Effects in a Mach Number 10 Hydrogen-Fueled Scramjet
期刊论文
JOURNAL OF PROPULSION AND POWER, 2024, 页码: 17
Authors:
Liu H(刘杭)
;
Yao W(姚卫)
;
Zhang X(张旭)
;
Zhang XY(张晓源)
;
Liu, Jianwen
;
Yue LJ(岳连捷)
;
Sun QH(孙泉华)
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Submit date:2024/03/11
Scramjet
Dynamic Zone Flamelet Model
High Enthalpy Shock Tunnel
Combustors
Improved Delayed Detached Eddy Simulation
Vibrational Energy
nonequilibrium heating
cooling effects
thermal nonequilibrium
chemical nonequilibrium
hydrogen