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 [5]
工程热物理研究所 [5]
采集方式
OAI收割 [10]
内容类型
期刊论文 [10]
发表日期
2022 [1]
2020 [1]
2016 [1]
2014 [1]
2013 [1]
2005 [2]
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学科主题
流体力学::计算流体... [1]
高超声速气体动力学 [1]
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Control of shock-wave/boundary-layer interaction using abackward-facing step
期刊论文
OAI收割
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 126, 页码: 13
作者:
Zhai J
;
Zhang CA(张陈安)
;
Wang FM(王发民)
;
Zhang WW(张伟为)
  |  
收藏
  |  
浏览/下载:29/0
  |  
提交时间:2022/12/20
Shock-wave/boundary-layer interaction
Backward-facing step
Flow separation
Hypersonic inlet
Alleviation of lateral spillage of two-dimensional hypersonic inlet using waverider-configuration chines
期刊论文
OAI收割
INTERNATIONAL JOURNAL OF MODERN PHYSICS B, 2020, 卷号: 34, 期号: 14-16, 页码: 5
作者:
Zhai J
;
Zhang CA(张陈安)
;
Wang FM(王发民)
;
Zhang WW
  |  
收藏
  |  
浏览/下载:33/0
  |  
提交时间:2020/08/26
Hypersonic inlet
lateral spillage
waverider design method
streamline tracing technology
mass-flow ratio
Design methodology for shape transition inlets based on constant contraction of discrete streamtubes
期刊论文
OAI收割
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2016, 卷号: 230, 期号: 8, 页码: 1496-1506
作者:
Xiao YB(肖雅斌)
;
Yue LJ(岳连捷)
;
Ma SH
;
Zhang XY(张新宇)
收藏
  |  
浏览/下载:42/0
  |  
提交时间:2016/09/14
Hypersonic inlet
shape transition
inward turning
scramjet
design method
Flow characteristics of hypersonic inlets with different cowl-lip blunting methods
期刊论文
OAI收割
SCIENCE CHINA-Physics, Mechanics & Astronomy, 2014, 卷号: 57, 期号: 4, 页码: 741-752
作者:
Lu HB(卢洪波)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
;
Yue LJ(岳连捷)
收藏
  |  
浏览/下载:52/0
  |  
提交时间:2014/04/15
hypersonic inlet
cowl-lip bluntness
flow characteristics
shock pattern
shock interference
Conceptual design and aerodynamic evaluation of hypersonic airplane with double flanking air inlets
期刊论文
OAI收割
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2013, 卷号: 56, 期号: 8, 页码: 1980-1988
作者:
Cui K(崔凯)
;
Hu SC(胡守超)
;
Li GL(李广利)
;
Qu ZP(屈志朋)
;
Situ M
收藏
  |  
浏览/下载:38/0
  |  
提交时间:2013/09/27
hypersonic
flanking air inlet
waverider
computational fluid dynamics(CFD)
The Research of Laminar-Turbulent Transition in Hypersonic Three-Dimensional Boundary Layer
期刊论文
OAI收割
JOURNAL OF THERMAL SCIENCE, 2005, 卷号: 14, 期号: 2, 页码: 103,107
Marat A. GOLDFELD
;
Evgeniy V. ORLIK
收藏
  |  
浏览/下载:17/0
  |  
提交时间:2013/03/11
hypersonic boundary layer
transition
convergent inlet
adverse pressure gradient
The Research of Laminar-Turbulent Transition in Hypersonic Three-Dimensional Boundary Layer
期刊论文
OAI收割
JOURNAL OF THERMAL SCIENCE, 2005, 卷号: 14, 期号: 2, 页码: 103,107
作者:
Marat A. GOLDFELD
;
Evgeniy V. ORLIK
  |  
收藏
  |  
浏览/下载:15/0
  |  
提交时间:2013/03/11
Hypersonic Boundary Layer
Transition
Convergent Inlet
Adverse Pressure Gradient
Numerical and Experimental Studies of 3D Hypersonic Inlet
期刊论文
OAI收割
JOURNAL OF THERMAL SCIENCE, 2002, 卷号: 11, 期号: 3, 页码: 198,206
Marat A. Goldfeld
;
Roman V. Nestoulia
收藏
  |  
浏览/下载:25/0
  |  
提交时间:2013/03/12
hypersonic inlet
convergent inlet
boundary layer.
Preliminary Investigation of Full Model of Two-Mode Scramjet
期刊论文
OAI收割
JOURNAL OF THERMAL SCIENCE, 2001, 卷号: 10, 期号: 2, 页码: 97,102
J.L. Le
;
Z.C. Zhang
;
H.C. Bai1
;
M.A. Goldfeld
;
R.V. Nestoulia
;
A.V. Starov2
收藏
  |  
浏览/下载:22/0
  |  
提交时间:2013/03/12
full engine
hypersonic flow
fuel
inlet
combustion
wind tunnel
experiment.
Preliminary Investigation of Full Model of Two-Mode Scramjet
期刊论文
OAI收割
JOURNAL OF THERMAL SCIENCE, 2001, 卷号: 10, 期号: 2, 页码: 97,102
作者:
J.L. Le
;
Z.C. Zhang
;
H.C. Bai1
;
M.A. Goldfeld
;
R.V. Nestoulia
  |  
收藏
  |  
浏览/下载:24/0
  |  
提交时间:2013/03/12
Full Engine
Hypersonic Flow
Fuel
Inlet
Combustion
Wind Tunnel
Experiment.