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Knowledge Management System of Institue of Mechanics, CAS
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Source Publication:SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY
Community:高温气体动力学国家重点实验室
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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)
Adobe PDF(661Kb)
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View/Download:387/93
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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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View/Download:319/101
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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
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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View/Download:543/230
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Submit date:2016/03/21
Aerodynamic Heating
Hypersonic
Shock Tunnel
Stanton Number
Sharp Cone
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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View/Download:380/99
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Submit date:2016/01/08
Boundary Layer Control
Boundary Layer Heat Flow
Shock Wave Interactions
Separated Flows
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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View/Download:739/255
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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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View/Download:887/262
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Submit date:2013/10/23
Scramjet
Boundary Layer Bleed
Theoretical Analysis
Engine Thrust
Towards an entropy-based detached-eddy simulation
期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2013, 卷号: 56, 期号: 10, 页码: 1970-1980
Authors:
Zhao R(赵瑞)
;
Yan C(阎超)
;
Li XL(李新亮)
;
Kong WX
;
Zhao, R (reprint author), Beijing Univ Aeronaut & Astronaut, Natl Lab Computat Fluid Dynam, Beijing 100191, Peoples R China.
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Submit date:2013/10/23
Hybrid Rans/les
Detached-eddy Simulation
Turbulence
Compressible Flows
Entropy
DNS of a spatially evolving hypersonic turbulent boundary layer at Mach 8
期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2013, 卷号: 56, 期号: 7, 页码: 1408-1418
Authors:
Liang Xian
;
Li XinLiang
;
Liang X(梁贤)
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View/Download:914/327
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Submit date:2013/06/13
Dns
Compressibility Effects
Turbulent Boundary Layer
Shock tube study of kerosene ignition delay at high pressures
期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2012, 卷号: 55, 期号: 6, 页码: 947-954
Authors:
Liang JH(梁金虎)
;
Wang S(王苏)
;
Hu HH(胡弘浩)
;
Zhang ST
;
Fan BC(范秉诚)
;
Cui JP(崔季平)
;
Wang, S
;
Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Submit date:2013/01/18
Ignition Delay Time
Kerosene
Shock Tube
High Pressure
Mixtures
Autoignition
Temperatures
Times