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Experimental investigation of a hypersonic I-shaped configuration with a waverider compression surface
期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2020, 卷号: 63, 期号: 5, 页码: 3
Authors:
Li GL(李广利)
;
Cui K(崔凯)
;
Xu YZ(徐应洲)
;
Wang HX(王浩祥)
;
Yang J(杨靖)
;
Xu XG(许先贵)
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Submit date:2020/05/18
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
Hypersonic I-shaped aerodynamic configurations
期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2018, 卷号: 61, 期号: 2, 页码: 24722
Authors:
Cui K(崔凯)
;
Xiao Y(肖尧)
;
Xu YZ
;
Li GL
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Submit date:2018/10/30
Comparative study on aerodynamic heating under perfect and nonequilibrium hypersonic flows
期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2016, 卷号: 59, 期号: 2, 页码: 624701
Authors:
Wang Q(汪球)
;
Li JP(李进平)
;
Zhao W(赵伟)
;
Jiang ZL(姜宗林)
;
Li, JP (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:2016/03/21
Aerodynamic Heating
Hypersonic
Shock Tunnel
Stanton Number
Sharp Cone
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
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
Nonlinear spectral-like schemes for hybrid schemes
期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2014, 卷号: 57, 期号: 4, 页码: 753-763
Authors:
He, ZW
;
Li XL(李新亮)
;
Liang X(梁贤)
;
Li, XL (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:2014/05/09
Group Velocity Control
Hybrid
Weno
Shockwave-turbulent Boundary Layer Interaction
Direct Numerical Simulation
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)
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View/Download:899/255
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Submit date:2014/04/15
Hypersonic Inlet
Cowl-lip Bluntness
Flow Characteristics
Shock Pattern
Shock Interference
Effects of different product phases in aluminum dust detonation modeling
期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2013, 卷号: 56, 期号: 11, 页码: 2178-2185
Authors:
Teng HongHui
;
Jiang ZongLin
;
Teng, HH (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:2013/11/18
Detonation
Aluminum
Multiphase
Theoretical analysis of effects of boundary layer bleed on scramjet thrust
期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2013, 卷号: 56, 期号: 10, 页码: 1952-1961
Authors:
Yue LJ(岳连捷)
;
Xu XK(徐显坤)
;
Zhang XY(张新宇)
;
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:2013/10/23
Scramjet
Boundary Layer Bleed
Theoretical Analysis
Engine Thrust