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Knowledge Management System of Institue of Mechanics, CAS
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Numerical investigation of free oblique detonation wave induced by non-intrusive energy deposition
期刊论文
AIP ADVANCES, 2021, 卷号: 11, 期号: 12, 页码: 17
Authors:
Zhang WS(张文硕)
;
Zhang, Zijian
;
Jiang ZL(姜宗林)
;
Han X(韩信)
;
Liu YF(刘云峰)
;
Wang C(王春)
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Submit date:2022/01/24
Direct numerical simulation of hypersonic boundary layer transition over a lifting-body model HyTRV
期刊论文
Advances in Aerodynamics, 2021, 卷号: 3, 期号: 1
Authors:
Qi H(齐涵)
;
Li XL(李新亮)
;
Yu ZP(于长平)
;
Tong FL(童福林)
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Submit date:2021/11/01
Lifting body model
Hypersonic transition
Direct numerical simulation
Numerical study on aerodynamic performance of waverider with a new bluntness method
期刊论文
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2021, 卷号: 235, 期号: 10, 页码: 1225-1233
Authors:
Qu ZP
;
Xiao HD
;
Lv MY
;
Li GL(李广利)
;
Cui K(崔凯)
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Submit date:2021/06/11
bluntness method
computational fluid dynamics
hypersonic
volume
Waverider
Theoretical, numerical and experimental study of hypersonic boundary layer transition: Blunt circular cone
期刊论文
APPLIED THERMAL ENGINEERING, 2021, 卷号: 194, 页码: 14
Authors:
Chen, Jianqiang
;
Yi, Shihe
;
Li XL(李新亮)
;
Han GL(韩桂来)
;
Zhang, Yifeng
;
Yang, Qiang
;
Yuan, Xianxu
Adobe PDF(11175Kb)
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Submit date:2021/08/03
Hypersonic boundary layer
Stability
Transition
Thermal protection
The mechanical behavior and collapse of graphene-assembled hollow nanospheres under compression
期刊论文
CARBON, 2021, 卷号: 173, 页码: 600-608
Authors:
Zhao, Yifan
;
Zhao, Yushun
;
Wu, Fan
;
Zhao, Yue
;
Wang, Yaming
;
Sui, Chao
;
He, Xiaodong
;
Wang C(王超)
;
Tan, Huifeng
;
Wang, Chao
Adobe PDF(3740Kb)
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Submit date:2021/04/19
Graphene
Hollow nanosphere
In-situ test
Compressive mechanical properties
Numerical study on supersonic boundary-layer transition and wall skin friction reduction induced by fuel wall-jet combustion
期刊论文
ACTA ASTRONAUTICA, 2020, 卷号: 174, 页码: 11-23
Authors:
Xue R
;
Zheng X
;
Yue LJ(岳连捷)
;
Zhang SK
;
Weng C
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Submit date:2020/08/26
Compressible boundary layer combustion
Skin-friction reduction
Boundary layer transition
Transition k-kl-w model
Hydrogen combustion
Modification of hypersonic waveriders by vorticity-based boundary layer displacement thickness determination method
期刊论文
Aerospace Science and Technology, 2018, 卷号: 75, 页码: 200-214
Authors:
Liu W(刘文)
;
Zhang CA(张陈安)
;
Wang FM(王发民)
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Submit date:2018/06/16
Aerothermal characteristics of bleed slot in hypersonic flows
期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2015, 卷号: 58, 期号: 10, 页码: 104703
Authors:
Yue LJ(岳连捷)
;
Lu HB
;
Xu X
;
Chang XY
;
Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Submit date:2016/01/08
Boundary Layer Control
Boundary Layer Heat Flow
Shock Wave Interactions
Separated Flows
A modified multi-objective sorting particle swarm optimization and its application to the design of the nose shape of a high-speed train
期刊论文
ENGINEERING APPLICATIONS OF COMPUTATIONAL FLUID MECHANICS, 2015, 卷号: 9, 期号: 1, 页码: 513-527
Authors:
Yao SB(姚栓宝)
;
Guo DL(郭迪龙)
;
Sun ZX(孙振旭)
;
Yang GW(杨国伟)
;
Sun, ZX
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Submit date:2018/07/06
Flow characteristics of hypersonic inlets with different cowl-lip blunting methods
期刊论文
SCIENCE CHINA-Physics, Mechanics & Astronomy, 2014, 卷号: 57, 期号: 4, 页码: 741-752
Authors:
Lu HB(卢洪波)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
;
Yue LJ(岳连捷)
Adobe PDF(1133Kb)
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Submit date:2014/04/15
Hypersonic Inlet
Cowl-lip Bluntness
Flow Characteristics
Shock Pattern
Shock Interference