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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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Dynamic interaction patterns of oblique detonation waves with boundary layers in hypersonic reactive flows
期刊论文
COMBUSTION AND FLAME, 2025, 卷号: 271, 页码: 113832./通讯作者:Yang PF
Authors:
Sun, Jie
;
Yang PF(杨鹏飞)
;
Chen, Zheng
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View/Download:3/0
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Submit date:2024/12/02
Oblique detonation wave
Boundary layer
Flow separation
Choked flow
On the low-frequency flapping motion in flow separation
期刊论文
JOURNAL OF FLUID MECHANICS, 2024, 卷号: 984, 页码: 17./通讯作者:Fang, Xingjun, Wang, Zhan
Authors:
Fang XJ(方兴军)
;
Wang Z(王展)
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View/Download:157/0
  |  
Submit date:2024/05/14
boundary layer separation
Mitigation of Shock-Induced Separation Using Square-Shaped Micro-Serrations-A Preliminary Study
期刊论文
AEROSPACE, 2024, 卷号: 11, 期号: 2, 页码: 16./通讯作者:Zhang, Qifan, Chen, Hao
Authors:
Yu FY(于方游)
;
Gao ZB(高占彪)
;
Zhang QF(张启帆)
;
Yue LJ(岳连捷)
;
Chen H(陈昊)
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View/Download:78/0
  |  
Submit date:2024/05/21
micro-serration
separation control
shock wave/boundary layer interaction
Numerical Study on the Aerodynamic Heating Characteristics of the Cantilevered Injection System for Oblique Detonation Engine Inlets
期刊论文
AEROSPACE, 2023, 卷号: 10, 期号: 10, 页码: 18./通讯作者:Lin, Mingyue
Authors:
Yang F(杨帆)
;
Lin MY(林明月)
;
Hu ZM(胡宗民)
;
Han GL(韩桂来)
Adobe PDF(8946Kb)
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View/Download:183/15
  |  
Submit date:2023/11/28
oblique detonation engine
cantilevered injection
localized high heat flux
boundary layer separation
reattachment
Control of shock-wave/boundary-layer interaction using abackward-facing step
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 126, 页码: 13./通讯作者:Zhai, Jian
Authors:
Zhai J
;
Zhang CA(张陈安)
;
Wang FM(王发民)
;
Zhang WW(张伟为)
Adobe PDF(4533Kb)
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Submit date:2022/12/20
Shock-wave/boundary-layer interaction
Backward-facing step
Flow separation
Hypersonic inlet
Three-dimensional structural characteristics of flow separation induced by a forward-facing step in a turbulent channel flow
期刊论文
JOURNAL OF FLUID MECHANICS, 2021, 卷号: 919, 页码: 32./通讯作者:Fang, Xingjun
Authors:
Fang, Xingjun
;
Tachie, Mark F.
;
Bergstrom, Donald J.
;
Yang ZX(杨子轩)
;
Wang, Bing-Chen
Adobe PDF(3361Kb)
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View/Download:338/69
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Submit date:2021/06/21
boundary layer separation
turbulent boundary layers
Formation of stabilized oblique detonation waves in a combustor
期刊论文
COMBUSTION AND FLAME, 2021, 卷号: 223, 页码: 423-436./通讯作者:Liu, Yunfeng
Authors:
Zhang ZJ(张子健)
;
Wen, Chihyung
;
Zhang WS(张文硕)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
Adobe PDF(3599Kb)
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View/Download:553/96
  |  
Submit date:2021/03/03
Oblique detonation wave
Combustor
Oblique detonation engine
Normal detonation wave
Boundary layer separation
A comparative study of elliptical and round scramjet combustors by Improved Delayed Detached Eddy Simulation
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Yao W(姚卫)
;
Yuan YM(袁越明)
;
Li XP(李晓鹏)
;
Wang J(王晶)
;
Fan XJ(范学军)
;
Fan, Xuejun(
[email protected]
)
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  |  
Adobe PDF(1173Kb)
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View/Download:539/250
  |  
Submit date:2018/01/16
Adiabatic Flame Temperature
Aerodynamics
Boundary Layer Flow
Boundary Layers
Chemical Analysis
Combustion
Computational Chemistry
Directed Graphs
Flow Separation
Mach Number
Principal Component Analysis
Regression Analysis
Sensitivity Analysis
Spacecraft
Supersonic Aerodynamics
Supersonic Aircraft
Transients
转捩对压缩拐角激波/边界层干扰分离泡的影响
期刊论文
航空学报, 2016, 卷号: 37, 期号: 10, 页码: 2909-2921
Authors:
童福林
;
李新亮
;
唐志共
;
朱兴坤
;
黄江涛
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  |  
Adobe PDF(1595Kb)
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View/Download:551/110
  |  
Submit date:2017/02/24
Transition
Compression Ramp
Shock Wave/boundary Layer Interaction
Separation Bubble
Direct Numerical Simulation
Vortex motion in the early stages of unsteady flow around a circular cylinder
期刊论文
Sadhana-Academy Proceedings in Engineering Sciences, 1984, 卷号: 7, 期号: 7, 页码: 119-135
Authors:
Ling GC(凌国灿)
;
Yin XY
Adobe PDF(1227Kb)
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Submit date:2009/08/03
Vortex Motion - Unsteady Flow - Circular Cylinder - Flow Structure - Boundary Layer Separation - Rear Shear Layer Separation - Viscous Vortex Core