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Knowledge Management System of Institue of Mechanics, CAS
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Flow characteristic of highly underexpanded jets from various nozzle geometries
期刊论文
APPLIED THERMAL ENGINEERING, 2017, 卷号: 125, 页码: 240-253
Authors:
Li XP(李晓鹏)
;
Zhou, Rui
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Fan, XJ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
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Submit date:2017/11/16
Underexpanded Jets
Noncircular Jets
Nozzle Geometry
Large Eddy Simulation
Graphene Foam: Uniaxial Tension Behavior and Fracture Mode Based on a Mesoscopic Model
期刊论文
ACS NANO, 2017, 卷号: 11, 期号: 9, 页码: 8988-8997
Authors:
Pan DX(潘斗兴)
;
Wang C(王超)
;
Wang ZQ(王自强)
;
Yao YG(姚裕贵)
;
Yao, YG (reprint author), Beijing Inst Technol, Sch Phys, Beijing Key Lab Nanophoton & Ultrafine Optoelect, Beijing 100081, Peoples R China.
;
Wang, TC (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing 100190, Peoples R China.
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Submit date:2017/11/29
Mesoscopic Model
Graphene Foam
Coarse-grained Molecular Dynamics
Multipeak Stress Strain Curve
Ductile Fracture
Power Scaling Law
Multiscale Physics Mechanics
Simulations of twisted bilayer orthorhombic black phosphorus
期刊论文
PHYSICAL REVIEW B, 2017, 卷号: 96, 期号: 4
Authors:
Pan DX(潘斗兴)
;
Wang ZQ(王自强)
;
Xiao, Wende
;
Hu, Dongmei
;
Yao YG(姚裕贵)
;
Yao, YG (reprint author), Beijing Inst Technol, Lab Quantum Funct Mat Design & Applicat, Sch Phys, Beijing 100081, Peoples R China.
;
Wang, TC (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing 100190, Peoples R China.
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Submit date:2017/11/29
Application of short time energy analysis in monitoring the stability of arc sound signal
期刊论文
MEASUREMENT, 2017, 卷号: 105, 页码: 98-105
Authors:
Yao P
;
Zhou K(周亢)
;
Zhou, K (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temperature Gas Dynam, Beijing, Peoples R China.
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Submit date:2017/07/24
Short Time Energy
Arc Sound Signal
Quantitative Evaluation
Statistical Analysis
Quantitative evaluation method of arc sound spectrum based on sample entropy
期刊论文
MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2017, 卷号: 92, 页码: 379-390
Authors:
Yao P
;
Zhou K(周亢)
;
Zhu Q
;
Zhou, K (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100864, Peoples R China.
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Submit date:2017/07/24
Arc Sound Signal
Sample Entropy
Psd
Asse
Numerical investigation of characteristic frequency excited highly underexpanded jets
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 63, 页码: 304-316
Authors:
Li XP
;
Fan E
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
;
Fan, XJ (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
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Submit date:2017/07/24
Fuel Jets
Underexpanded Jets
Jet Mixing Control
Excited Jets
Large Eddy Simulation
Research of a Multi-Frequency Waveform Control Method on Double-Wire MIG Arc Welding
期刊论文
APPLIED SCIENCES-BASEL, 2017, 卷号: 7, 期号: 2
Authors:
Yao P
;
Zhou K(周亢)
;
Zhou, K (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
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Submit date:2017/07/24
Double-wire Mig Arc Welding
Multi-frequency Modulation
Current Waveform Control
Orthogonal Experiment
高度欠膨胀声速射流的自相似特性
期刊论文
航空动力学报, 2017, 卷号: 32, 期号: 01, 页码: 177-187
Authors:
李晓鹏
;
姚卫
;
范学军
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Submit date:2017/12/22
高度欠膨胀射流
大涡模拟
自相似特性
高斯拟合
剪切层发展
A comparative study of elliptical and round scramjet combustors by Improved Delayed Detached Eddy Simulation
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Yao W(姚卫)
;
Yuan YM(袁越明)
;
Li XP(李晓鹏)
;
Wang J(王晶)
;
Fan XJ(范学军)
;
Fan, Xuejun(xfan@imech.ac.cn)
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Submit date:2018/01/16
Adiabatic Flame Temperature
Aerodynamics
Boundary Layer Flow
Boundary Layers
Chemical Analysis
Combustion
Computational Chemistry
Directed Graphs
Flow Separation
Mach Number
Principal Component Analysis
Regression Analysis
Sensitivity Analysis
Spacecraft
Supersonic Aerodynamics
Supersonic Aircraft
Transients
LES Study of Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Wu K(吴坤)
;
Zhang P(张鹏)
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Zhang, Peng(pengzhang.zhang@polyu.edu.hk)
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Submit date:2018/01/16
Combustion
Diesel Engines
Hydrogen
Large Eddy Simulation
Spacecraft
Stabilization
Supersonic Aircraft
Temperature Measurement
Wall Flow