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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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The design and main performance of a hydrogen peroxide/kerosene coaxial-swirl injector in a lab-scale rocket engine
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 70, 页码: 636-643
Authors:
Li HX(李慧鑫)
;
Ye L(叶亮)
;
Wei XL(魏小林)
;
Li T(李腾)
;
Li S(李森)
;
Wei, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
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Submit date:2017/12/18
H2o2/kerosene Bipropellant
Coaxial-swirl Injector
Geometric Constant
Performance
Initiation characteristics of wedge-induced oblique detonation waves in a stoichiometric hydrogen-air mixture
期刊论文
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2017, 卷号: 36, 期号: 2, 页码: 2735-2742
Authors:
Teng HH(滕宏辉)
;
Ng HD
;
Jiang ZL(姜宗林)
;
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:2017/07/24
Oblique Detonation
Formation Structure
Hydrogen
Shock Wave
Detailed Chemistry
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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Submit date:2016/12/08
Detonation Wave
Detonation Instability
Shock Wave
Chemical Reaction
Experimental investigation and numerical simulation of CO oxidation with HCl addition
期刊论文
FUEL, 2016, 卷号: 179, 页码: 221-228
Authors:
Wu, Dongyin
;
Wang, Yuhao
;
Wei XL(魏小林)
;
Li S(李森)
;
Guo, Xiaofeng
;
Wei, 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:2017/12/18
Inhibition Effect
Co Oxidation
Reduced Mechanism
Hcl
Efr
Engine performance analysis and optimization of a dual-mode scramjet with varied inlet conditions
期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 1, 页码: 75-82
Authors:
Tian L
;
Chen LH(陈立红)
;
Chen Q(陈强)
;
Zhong FQ(仲峰泉)
;
Zhang XY(张新宇)
;
Chen, LH (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:2016/09/14
Dual-mode Scramjet
Engine Performance
Thrust
Optimization
Heat Release Distribution
Simulated Annealing Algorithm
Investigation on the Pinch Point Position in Heat Exchangers
期刊论文
JOURNAL OF THERMAL SCIENCE, 2016, 卷号: 25, 期号: 3, 页码: 258-265
Authors:
Pan LS(潘利生)
;
Shi Weixiu
;
Pan, LS (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
;
Shi, WX (reprint author), Beijing Univ Civil Engn & Architecture, Sch Environm & Energy Engn, Beijing 100044, Peoples R China.
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Submit date:2017/12/18
Pinch Point Position
Heat Exchanger
Heat Transfer
Phase Transition
Supercritical Condition
Skeletal mechanism modelling of n-heptane/oxygen laminar coflow flame structure at pressures
期刊论文
FUEL, 2015, 卷号: 162, 页码: 162-170
Authors:
Li S(李森)
;
Wei XL(魏小林)
;
Li, S (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
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Submit date:2016/01/08
Skeletal Mechanism
N-heptane
Flame Structure
Soot
A Slope Constrained 4th Order Multi-Moment Finite Volume Method with WENO Limiter
期刊论文
COMMUNICATIONS IN COMPUTATIONAL PHYSICS, 2015, 卷号: 18, 期号: 4, 页码: 901-930
Authors:
Sun ZY
;
Teng HH(滕宏辉)
;
Xiao F
;
Xiao, F (reprint author), Tokyo Inst Technol, Dept Energy Sci, Midori Ku, 4259 Nagatsuta, Yokohama, Kanagawa 2268502, Japan.
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Submit date:2016/01/08
Multi-moment Finite Volume Method
Weno
Flux Reconstruction
Compressible Flow
Conservative Method
Oscillation-suppressing
Numerical study of oblique detonation wave initiation in a stoichiometric hydrogen-air mixture
期刊论文
PHYSICS OF FLUIDS, 2015, 卷号: 27, 期号: 9, 页码: 96101
Authors:
Wang T
;
Zhang YN
;
Teng HH(滕宏辉)
;
Jiang ZL(姜宗林)
;
Ng HD
;
Wang, T (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
Experimental study on the effect of combustor configuration on the performance of dual-mode combustor
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 42, 页码: 169-175
Authors:
Wang ZP(王知溥)
;
Li F(李飞)
;
Gu HS
;
Yu XL(余西龙)
;
Zhang XY(张新宇)
;
Li, F (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:2015/06/12
Scramjet
Dual-mode Combustor
Divergent Angle
Cavity Location
Combustion Efficiency
Tdlas