RAMJET

作品数：16被引量：41H指数：4
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相关领域：航空宇航科学技术更多>>
相关作者：于达仁鲍文唐井峰杨晟博更多>>
相关机构：哈尔滨工业大学南京理工大学南京航空航天大学更多>>
相关期刊：《Journal of Hydrodynamics》《推进技术》《宇航学报》《Science China(Technological Sciences)》更多>>
相关基金：国家自然科学基金国家高技术研究发展计划航天支撑技术基金航天科技创新基金更多>>
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Drag reduction characteristics of recirculation flow at rocket base in an RBCC engine under ramjet/scramjet mode
《Chinese Journal of Aeronautics》2024年第3期104-115,共12页Menglei LI Mingbo SUN Peibo LI Daoning YANG Bin AN Yizhi YAO Jikai CHEN Taiyu WANG Jiaoru WANG 
supported by the National Natural Science Foundation of China(Nos.11925207 and 92252206);the Hunan Province Graduate Innovation Project,China(No.XJCX2023059)。
To reduce the drag generated by the recirculation flow at the rocket base in a RocketBased Combined Cycle(RBCC)engine operating in the ramjet/scramjet mode,a novel annular rocket RBCC engine based on a central plug co...
关键词：Rocket-based combined cycle Ramjet/scramjet mode Plug cone Drag reduction k-x SST turbulent model 
Effect of mixing section configurations on combustion efficiency of Mg-CO_(2)Martian ramjet
《Chinese Journal of Aeronautics》2023年第4期165-173,共9页Xu WANG Yanpeng BU Xu XU Qingchun YANG 
supported by the Fund of Advance Research Projects of Manned Spaceflight,China(No.050303).
Experiments were conducted to determine the effects of the mixing section configurations on the Mg-CO_(2)Martian ramjet combustion efficiency.It was carried out at a mainstream mass flow rate of 110 g/s and a temperat...
关键词：Combustion efficiency Magnesium-base fuel Martian ramjet Mars exploration Structural configurations 
Research progress on solid-fueled Scramjet被引量：7
《Chinese Journal of Aeronautics》2022年第1期398-415,共18页Xiang ZHAO Zhixun XIA Likun MA Chaolong LI Chuanbo FANG Benveniste NATAN Alon GANY 
supported by the China Scholarship Council and the National Natural Science Foundation of China(Nos.2020JJ4665,51706241).
The solid-fueled Scramjet is an interesting option for supersonic combustion ramjet.It shows significant advantages such as simple fuel supply and compactness,avoiding the complex system of tanks and pipelines that en...
关键词：Combustor performance Flame stabilization SELF-IGNITION Solid-fueled Scramjet Supersonic combustion ramjet 
Self-ignition characteristics of the high-speed ramjet kinetic energy projectile in the launch process被引量：1
《Chinese Journal of Aeronautics》2019年第4期851-860,共10页Changfei ZHUO Haotian CHEN Wenjin YAO Xiaoming WANG 
supported by the National Natural Science Foundation of China(No.11602109);the Jiangsu Province Natural Science Foundation of China(No.BK20160836);the Fundamental Research Funds for the Central Universities(No.309171B8807)
To research the self-ignition characteristics of high-speed ramjet kinetic energy projectile in the launch process, the self-ignition process based on the solid fuel of polyethylene was numerically simulated by using ...
关键词：Dynamic grid Kinetic energy projectile Muzzle velocity SELF-IGNITION Solid fuel ramjet 
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