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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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Indexed By:EI
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Optimized sixth-order monotonicity-preserving scheme by nonlinear spectral analysis
期刊论文
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS, 2013, 卷号: 73, 期号: 6, 页码: 560–577
Authors:
Li XL(李新亮)
;
Leng Y(冷岩)
;
He ZW(何志伟)
;
Li, XL (reprint author), Chinese Acad Sci, LHD Inst Mech, Beijing 100190, Peoples R China
Adobe PDF(1159Kb)
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View/Download:1109/432
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Submit date:2013/09/21
Nonlinear Spectral Analysis
Monotonicity-preserving
Optimization
Shock-capturing Schemes
Dissipation
Dispersion
Interaction of isentropic compression waves with a bow shock
期刊论文
AIAA JOURNAL, 2013, 卷号: 51, 期号: 10, 页码: 2474-2484
Authors:
Lu HB(卢洪波)
;
Yue LJ(岳连捷)
;
Xiao YB(肖雅彬)
;
Zhang XY(张新宇)
;
Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temperature Gas Dynam, Beijing 100190, Peoples R China.
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View/Download:763/286
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Submit date:2014/01/17
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:889/263
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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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View/Download:1157/253
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Submit date:2013/10/23
Hybrid Rans/les
Detached-eddy Simulation
Turbulence
Compressible Flows
Entropy
Conceptual design and aerodynamic evaluation of hypersonic airplane with double flanking air inlets
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2013, 卷号: 56, 期号: 8, 页码: 1980-1988
Authors:
Cui K(崔凯)
;
Hu SC(胡守超)
;
Li GL(李广利)
;
Qu ZP(屈志朋)
;
Situ M
;
Cui, K (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:892/296
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Submit date:2013/09/27
Hypersonic
Flanking Air Inlet
Waverider
Computational Fluid Dynamics(Cfd)
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:887/291
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Submit date:2013/09/21
Baldwin-lomax Model
Boundary Layers
Computational Aerodynamics
Entropy
Supersonic Flows
Turbulence Models
Direct Numerical Simulation of Chemical Non-equilibrium Turbulent Flow
期刊论文
Chinese Physics Letters, 2013, 卷号: 30, 期号: 6, 页码: 064702/1-064702/5
Authors:
Chen XP(陈小平)
;
Li XL(李新亮)
;
Li, XL (reprint author), Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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View/Download:868/375
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Submit date:2013/09/21
Channel Flows
Turbulent Flows
Non-equilibrium Turbulent Flow
Chemical Reactions
Direct Numerical Simulation
Numerical simulation of ignition and combustion of ethylene in a supersonic model combustor with a reduced kinetic mechanism
期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2013, 卷号: 185, 期号: 4, 页码: 548-563
Authors:
Zhong FQ(仲峰泉)
;
Chen LH(陈立红)
;
Li F(李飞)
;
Zhang XY(张新宇)
;
Sung CJ
;
Zhong, FQ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
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View/Download:1432/487
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Submit date:2013/05/03
Ethylene
Ignition
Numerical Simulation
Reduced Kinetic Mechanism
Supersonic Combustion
Approximate analytic solution of heat conduction in hollow semi-spheres flying at hypersonic speed
期刊论文
INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER, 2013, 卷号: 43, 页码: 46-52
Authors:
Han GL(韩桂来)
;
Jiang ZL(姜宗林)
;
Han, GL (reprint author), Chinese Acad Sci, Stake Key Lab High Temp Gas Dynam LHD, Inst Mech, Beijing 100190, Peoples R China.
Adobe PDF(548Kb)
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View/Download:1111/331
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Submit date:2013/05/31
Heat Conduction
Theoretical Investigation
Approximate Solution
Hypersonic
Fracture toughness and toughening mechanisms in a (ZrB2-SiC) composite reinforced with boron nitride nanotubes and boron nitride nanoplatelets
期刊论文
SCRIPTA MATERIALIA, 2013, 卷号: 68, 期号: 8, 页码: 579-582
Authors:
Yue CG
;
Liu WW
;
Zhang L
;
Zhang TH(张泰华)
;
Chen Y
;
Chen, Y (reprint author), Soochow Univ, Sch Mech & Elect Engn, 178 East Ganjiang Rd, Suzhou 215021, Peoples R China.
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View/Download:918/294
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Submit date:2013/04/07
Ceramic Matrix Composites
Boron Nitride Nanotubes
Toughness
Spark Plasma Sintering