中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
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CAS IR Grid
机构
力学研究所 [25]
工程热物理研究所 [3]
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OAI收割 [28]
内容类型
期刊论文 [28]
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2024 [4]
2022 [2]
2021 [1]
2020 [5]
2019 [2]
2018 [2]
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力学::流体力学::... [2]
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浏览/检索结果:
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On the determination of the standing oblique detonation wave in an engine combustor using laser absorption spectroscopy of hydroxyl radical
期刊论文
OAI收割
AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 卷号: 152, 页码: 11
作者:
Zhang WS(张文硕)
;
Zhang, Zijian
;
Han X(韩信)
;
Yuan CK(苑朝凯)
;
Liu YF(刘云峰)
  |  
收藏
  |  
浏览/下载:25/0
  |  
提交时间:2024/08/19
Standing oblique detonation ramjet
OH radical
Laser absorption spectroscopy
Shock tunnel
Freejet experiment
Nonequilibrium Heating/Cooling Effects in a Mach Number 10 Hydrogen-Fueled Scramjet
期刊论文
OAI收割
JOURNAL OF PROPULSION AND POWER, 2024, 页码: 17
作者:
Liu, Hang
;
Yao, Wei
;
Zhang, Xu
;
Zhang, Xiaoyuan
;
Liu, Jianwen
  |  
收藏
  |  
浏览/下载:16/0
  |  
提交时间: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
Investigation of Burst Pressure of Flat-Scored Metal Diaphragms in Hypersonic Impulse Facilities
期刊论文
OAI收割
AIAA JOURNAL, 2024, 页码: 8
作者:
Wang WT(王文韬)
;
Wang Q(汪球)
;
Li JP(李进平)
;
Zhao W(赵伟)
;
Gao, Liangjie
  |  
收藏
  |  
浏览/下载:21/0
  |  
提交时间:2024/02/26
Finite Element Method
Hypersonic
Shock Tube/Tunnel
Diaphragm
Burst Pressure
Experimental and numerical investigation on the unsteady interaction in longitudinal stage separation for parallel-staged two-body configuration
期刊论文
OAI收割
Physics of Fluids, 2024, 卷号: 36, 页码: 016116
作者:
Wang Y(王粤)
;
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
  |  
收藏
  |  
浏览/下载:20/0
  |  
提交时间:2024/01/15
Two-stage-to-orbit
Wind tunnel test
Numerical simulation
Stage separation
Hypersonic
Shock waves
Experimental Study of Longitudinal Stage Separation of Two-Body Configuration in Shock Tunnel
期刊论文
OAI收割
AIAA Journal, 2022, 卷号: Articles in Advance, 页码: 1-7
作者:
Wang Y(王粤)
;
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
  |  
收藏
  |  
浏览/下载:44/0
  |  
提交时间:2022/08/23
Two-stage-to-orbit
Multibody separation
Dynamic test
Aerodynamic interference
Shock Tunnel
Numerical and Experimental Study on the Duration of Nozzle Starting of the Reflected High-Enthalpy Shock Tunnel
期刊论文
OAI收割
APPLIED SCIENCES-BASEL, 2022, 卷号: 12, 期号: 6, 页码: 16
作者:
Yu, Jiangpeng
;
Li, Jinping
;
Wang, Qiu
;
Zhang, Xiaoyuan
;
Zhang, Shizhong
  |  
收藏
  |  
浏览/下载:65/0
  |  
提交时间:2022/05/17
nozzle starting
high-enthalpy shock tunnel
center startup
complete startup
Criteria for hypersonic airbreathing propulsion and its experimental verification
期刊论文
OAI收割
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
作者:
Jiang ZL(姜宗林)
;
Zhang ZJ(张子健)
;
Liu YF(刘云峰)
;
Wang C(王春)
;
Luo ZT(罗长童)
  |  
收藏
  |  
浏览/下载:25/0
  |  
提交时间:2021/05/17
Concept demonstration
Hypersonic propulsion
Oblique detonation engine
Scramjet
Shock wave
Supersonic combustion
Wind tunnel test
Impulse force-measurement system
期刊论文
OAI收割
SHOCK WAVES, 2020, 页码: 11
作者:
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
  |  
收藏
  |  
浏览/下载:32/0
  |  
提交时间:2020/11/30
Shock tunnel
High enthalpy
Aerodynamic force measurement
Strain gauge balance
A Fast-Response Calorimeter with Dynamic Corrections for Transient Heat Transfer Measurements
期刊论文
OAI收割
APPLIED SCIENCES-BASEL, 2020, 卷号: 10, 期号: 17, 页码: 22
作者:
Zhang SZ(张仕忠)
;
Wang Q(汪球)
;
Li JP(李进平)
;
Zhang XY(张晓源)
;
Chen H(陈宏)
  |  
收藏
  |  
浏览/下载:66/0
  |  
提交时间:2020/11/30
calorimeter
shock tunnel
heat transfer measurement
hypersonic
Numerical modeling of a high-enthalpy shock tunnel driven by gaseous detonation
期刊论文
OAI收割
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 8
作者:
Luo K(罗凯)
;
Wang Q(汪球)
;
Li JW(栗继伟)
;
Li JP(李进平)
;
Zhao W(赵伟)
  |  
收藏
  |  
浏览/下载:34/0
  |  
提交时间:2020/11/30
Quasi-one-dimensional
Detonation
Shock tunnel
Shock speed