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Transitional wave configurations between Type III and Type IV oblique shock/bow shock interactions
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 3, 页码: 96-106
Authors:
Peng J(彭俊)
;
Li S(李帅)
;
Yang F(杨帆)
;
Lin MY(林明月)
;
Han GL(韩桂来)
;
Hu ZM(胡宗民)
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Submit date:2023/04/20
Shock interactions
Transitional configuration
Aerodynamic heating
Shear layer
Mach interaction
Direct numerical simulation of impinging shock wave and turbulent boundary layer interaction over a wavy-wall
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 5, 页码: 350-363
Authors:
Tong FL(童福林)
;
Sun D(孙栋)
;
Li XL(李新亮)
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Submit date:2021/06/07
Direct numerical simulation
Low-frequency unsteadiness
Shock waves
Turbulent boundary layer
Wavy-wall
Advances in critical technologies for hypersonic and high-enthalpy wind tunnel
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038
Authors:
Jiang ZL(姜宗林)
;
Hu ZM(胡宗民)
;
Wang YP(汪运鹏)
;
Han GL(韩桂来)
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Submit date:2021/03/30
High-enthalpy flow
Hypersonic wind tunnel
Aerospace vehicle
Aerodynamic balance
Heat flux sensor
Optical measurement technique
Numerical study of convective heat transfer of a supersonic combustor with varied inlet flow conditions
期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 5, 页码: 943-953
Authors:
Fan WH(范文慧)
;
Zhong FQ(仲峰泉)
;
Ma SG(马素刚)
;
Zhang XY(张新宇)
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Submit date:2020/03/11
Wall heat flux
Numerical simulation
Ethylene
Supersonic combustor
Effects of dimensional wall temperature on velocity-temperature correlations in supersonic turbulent channel flow of thermally perfect gas
期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2019, 卷号: 62, 期号: 6, 页码: AR64711
Authors:
Chen XP
;
Li XL(李新亮)
;
Zhu ZC
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Submit date:2019/04/11
direct numerical simulation
velocity-temperature correlation
supersonic flow
channel flow
thermally perfect gas
strong Reynolds analogy
Shock oscillation in highly underexpanded jets
期刊论文
CHINESE PHYSICS B, 2018, 卷号: 27, 期号: 9, 页码: 94705
Authors:
Li XP
;
Zhou R
;
Chen XP
;
Fan XJ(范学军)
;
Xie GS
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Submit date:2018/10/30
highly underexpanded jets
shock oscillation
large eddy simulation
Effect of uniform blowing or suction on hypersonic spatially developing turbulent boundary layers
期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2016, 卷号: 59, 期号: 6, 页码: 664702
Authors:
Chen Z(陈哲)
;
Yu ZP(于长平)
;
Li L(李理)
;
Li XL(李新亮)
;
Li, XL (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Submit date:2016/09/14
Influences of affiliated components and train length on the train wind
期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 2, 页码: 191-205
Authors:
Guo DL(郭迪龙)
;
Shang KM
;
Zhang Y
;
Yang GW(杨国伟)
;
Sun ZX(孙振旭)
;
Guo, DL
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Submit date:2017/09/04
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
Improvement of Baldwin-Lomax turbulence model for supersonic complex flows
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2013, 卷号: 26, 期号: 3, 页码: 529–534
Authors:
Zhao R(赵瑞)
;
Yan C(阎超)
;
Yu J(于剑)
;
Li XL(李新亮)
;
Yan, C (reprint author), Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China.
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View/Download:918/309
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Submit date:2013/09/21
Baldwin-lomax Model
Boundary Layers
Computational Aerodynamics
Entropy
Supersonic Flows
Turbulence Models