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姜宗林 [2]
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Date Issued:2023
Community:高温气体动力学国家重点实验室
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Thermochemical non-equilibrium flow characteristics of high Mach number inlet in a wide operation range
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 12, 页码: 164-184
Authors:
Dai, Chunliang
;
Sun, Bo
;
Yue LJ(岳连捷)
;
Zhou, Shengbing
;
Zhuo, Changfei
;
Zhou, Changsheng
;
Yu, Jianyi
Adobe PDF(5674Kb)
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View/Download:67/10
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Submit date:2024/02/19
Scramjet inlet
Starting ability
Thermochemical
Work performance
Standing oblique detonation for hypersonic propulsion: A review
期刊论文
PROGRESS IN AEROSPACE SCIENCES, 2023, 卷号: 143, 页码: 17
Authors:
Jiang ZL(姜宗林)
Adobe PDF(10386Kb)
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View/Download:62/7
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Submit date:2024/02/26
Standing oblique detonation
Scramjet engine
Oblique detonation engine
Shock wave
Supersonic combustion
Hypersonic ramjet propulsion
Self-sustained catalytic combustion of CO enhanced by micro fluidized bed: stability operation, fluidization state and CFD simulation
期刊论文
FRONTIERS OF ENVIRONMENTAL SCIENCE & ENGINEERING, 2023, 卷号: 17, 期号: 9, 页码: 109
Authors:
Zhang, Zirui
;
Zhang, Chenhang
;
Liu, Huan
;
Bin F(宾峰)
;
Wei XL(魏小林)
;
Kang RN(康润宁)
;
Wu, Shaohua
;
Yang, Wenming
;
Xu, Hongpeng
Adobe PDF(5148Kb)
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Submit date:2023/06/15
Self-sustained catalytic combustion
Carbon monoxide
Cu1-xCexOy
Fluidized bed
Computational fluid dynamics
基于 CO2 的飞行器降温减阻技术优化方法及特性
学位论文
硕士论文,北京: 中国科学院大学, 2023
Authors:
姚子康
Adobe PDF(7335Kb)
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Submit date:2023/07/10
飞行器热管理,仿生分形结构,优化,CO2 射流,降温减阻
二元进气道正攻角不起动现象影响规律研究
学位论文
硕士论文,北京: 中国科学院大学, 2023
Authors:
李育凌
Adobe PDF(6578Kb)
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Submit date:2023/06/25
超燃冲压发动机进气道
不起动
内压缩段设计
攻角
三维效应
Linear calibration-free wavelength modulation spectroscopy
期刊论文
MICROWAVE AND OPTICAL TECHNOLOGY LETTERS, 2023, 卷号: 65, 期号: 5, 页码: 1024-1030
Authors:
Li RJ(李仁杰)
;
Li F(李飞)
;
Lin X(林鑫)
;
Yu XL(余西龙)
Adobe PDF(2095Kb)
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Submit date:2021/11/01
calibration-free
laser spectroscopy
linear
tunable diode laser absorption spectroscopy
wavelength modulation spectroscopy
Numerical Investigation on Longitudinal Stage Separation of Spiked Two-Stage-to-Orbit Vehicle
期刊论文
Journal of Spacecraft and Rockets, 2023, 卷号: 60, 期号: 1, 页码: 215-229
Authors:
Wang Y(王粤)
;
Wang YP(汪运鹏)
;
Wang C(王春)
;
Jiang ZL(姜宗林)
Adobe PDF(5479Kb)
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Submit date:2022/08/24
Multistage Launch Vehicle
Aerodynamic Characteristics
Shock Wave Interaction
Angle of Attack
Waverider
Boundary Layer Flow
Total Variation Diminishing
Adverse Pressure Gradient
Hypersonic Flows
Hypersonic Wind Tunnels