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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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Hypersonic shock wave and turbulent boundary layer interaction in a sharp cone/flare model
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 3, 页码: 80-95
Authors:
Tong FL(童福林)
;
Duan JY(段俊亦)
;
Lai, Jiang
;
Sun, Dong
;
Yuan, Xianxu
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View/Download:42/0
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Submit date:2023/04/20
Shock wave
Hypersonic turbulent
boundary layer
Heat transfer
Skin friction decomposition
Direct numerical simulation
Criteria for hypersonic airbreathing propulsion and its experimental verification
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
Authors:
Jiang ZL(姜宗林)
;
Zhang ZJ(张子健)
;
Liu YF(刘云峰)
;
Wang C(王春)
;
Luo ZT(罗长童)
Adobe PDF(1806Kb)
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View/Download:269/49
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Submit date:2021/05/17
Concept demonstration
Hypersonic propulsion
Oblique detonation engine
Scramjet
Shock wave
Supersonic combustion
Wind tunnel test
Shock/shock interactions between bodies and wings
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2018, 卷号: 31, 期号: 2, 页码: 255-261
Authors:
Xiang GX(项高翔)
;
Wang C(王春)
;
Teng HH(腾宏辉)
;
Jiang ZL(姜宗林)
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View/Download:295/71
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Submit date:2018/10/30
Body And Wing
Flow Field
Hypersonic Flow
Shock/shock Interaction
Wave Configurations
Shock relations in gases of heterogeneous thermodynamic properties
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2017, 卷号: 60, 期号: 7, 页码: 1050-1057
Authors:
Hu ZM(胡宗民)
;
Zhou K(周凯)
;
Peng J(彭俊)
;
Li JP(李进平)
;
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:2017/10/25
Shock Wave
Imperfect Gas
Heterogeneous
Theoretical Solution
Theoretical approach to one-dimensional detonation instability
期刊论文
APPLIED MATHEMATICS AND MECHANICS-ENGLISH EDITION, 2016, 卷号: 37, 期号: 9, 页码: 1231-1238
Authors:
Wang C(王春)
;
Xiang GX(项高翔)
;
Jiang ZL(姜宗林)
;
Wang, C (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Adobe PDF(514Kb)
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View/Download:387/83
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Submit date:2016/12/08
Detonation Wave
Detonation Instability
Shock Wave
Chemical Reaction
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:412/70
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Submit date:2017/02/24
Transition
Compression Ramp
Shock Wave/boundary Layer Interaction
Separation Bubble
Direct Numerical Simulation
利用锤击试验及数值反演获取岩体平行结构面接触刚度的可行性研究
期刊论文
岩土工程学报, 2016, 卷号: 38, 期号: 10, 页码: 1911-1916
Authors:
郭汝坤
;
冯春
;
唐德泓
;
乔继延
;
李世海
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Adobe PDF(1128Kb)
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View/Download:289/53
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Submit date:2017/02/24
Structural Plane Stiffness
Field Test
Hammer Shock
Stress Wave
Linear Contact Hypothesis
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:364/96
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Submit date:2016/01/08
Boundary Layer Control
Boundary Layer Heat Flow
Shock Wave Interactions
Separated Flows
Transmission characteristics of EM wave in a finite thickness plasma
期刊论文
ACTA MECHANICA SINICA, 2013, 卷号: 29, 期号: 2, 页码: 189-195
Authors:
Zhu NY(竺乃宜)
;
Huang LS(黄立舜)
;
Wu B(吴彬)
;
Yu XL(余西龙)
;
Wu RH
;
Meng G
;
Ren AM
;
Hu XT
;
Wu B(吴彬)
Adobe PDF(770Kb)
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Submit date:2013/06/13
Plasma
Electromagnetic Wave
Shock Tube
Numerical Simulation
Measurements of non-equilibrium and equilibrium temperature behind a strong shock wave in simulated martian atmosphere
期刊论文
ACTA MECHANICA SINICA, 2012, 卷号: 28, 期号: 5, 页码: 1296-1302
Authors:
Lin X
;
Yu XL(余西龙)
;
Li F(李飞)
;
Zhang SH(张少华)
;
Xin JG
;
Zhang XY(张新宇)
;
Yu, XL
;
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
Radiation Measurements
Shock Wave
Mars Re-entry
Rotational Temperature
Vibrational Temperature
Radiation Measurements
Cn
Entry
Tube
Mixtures
Model