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发表日期:2017
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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
作者:
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)
Adobe PDF(1173Kb)
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浏览/下载:440/216
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提交时间: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
Development of zone flamelet model for scramjet combustor modeling
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:
Yao W(姚卫)
;
Fan XJ(范学军)
Adobe PDF(623Kb)
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浏览/下载:259/88
  |  
提交时间:2018/01/16
Combustion
Cost Benefit Analysis
Costs
Mixtures
Spacecraft
Supersonic Aircraft
Full Scale Detached Eddy Simulation of Transverse Hydrogen Jet in Supersonic Combustion
会议论文
53rd AIAA/SAE/ASEE Joint Propulsion Conference , Atlanta, GA., 10-12 July 2017
作者:
Fan E
;
Wu K(吴坤)
;
Lee YC
;
Yao W(姚卫)
;
Fan XJ(范学军)
Adobe PDF(2297Kb)
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浏览/下载:253/108
  |  
提交时间:2018/01/16
Fast Modeling Methods for Complex System with Separable Features
会议论文
10th International Symposium on Computational Intelligence and Design (ISCID), Hangzhou, PEOPLES R CHINA, DEC 09-10, 2017
作者:
Chen C(陈辰)
;
Luo ZT(罗长童)
;
Jiang ZL(姜宗林)
Adobe PDF(249Kb)
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浏览/下载:242/81
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提交时间:2018/06/06
Data-driven Modeling
Genetic Programming
Generalized Separable Model
Multi-level Block Search
Development of zone flamelet modelfor scramjet combustor modeling
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, March 6, 2017 - March 9, 2017
作者:
Yao W(姚卫)
;
Fan XJ(范学军)
Adobe PDF(832Kb)
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浏览/下载:274/81
  |  
提交时间:2018/11/08
Combustion
Cost benefit analysis
Costs
Mixtures
Ramjet engines
Supersonic aircraft
Computational costs
Equivalence ratios
Local flow conditions
Scramjet combustors
Statistics approaches
Supersonic combustion
Supersonic combustors
Turbulent combustion
Direct numerical simulation of supersonic turbulent boundary layer subjected to a curved compression ramp
会议论文
Meeting of the Institute-of-Non-Newtonian-Fluid-Mechanics (INNFM), Llanwddyn, WALES, 2017
作者:
Tong FL(童福林)
;
Li XL(李新亮)
;
Duan, Yanhui
;
Yu ZP(于长平)
;
Yu, CP (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
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Adobe PDF(3818Kb)
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浏览/下载:295/117
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提交时间:2018/01/16
Concave Surface Curvature
Adverse Pressure-gradient
Large-eddy Simulation
Reynolds-number
Near-wall
Flows
Separation
Vortices
Models
Numerical simulations of sessile droplet evaporating on heated substrate
会议论文
8th Meeting of the International-Marangoni-Association (IMA), Bad Honnef, GERMANY, 2016
作者:
Chen X(陈雪)
;
Chen, Paul G.
;
Ouazzani, Jalil
;
Liu QS(刘秋生)
;
Chen, PG (reprint author), Aix Marseille Univ, CNRS, Cent Marseille, M2P2, Marseille, France.
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Adobe PDF(659Kb)
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浏览/下载:260/73
  |  
提交时间:2018/01/16
Microdroplets
Surfaces
Water
New method to differentiate between matrix and micro-fractures using diffusion data in gas shale
会议论文
51st US Rock Mechanics / Geomechanics Symposium 2017, San Francisco, CA, United states, June 25, 2017 - June 28, 2017
作者:
Yang L(杨柳)
;
Shi X
;
Zhang KH
;
Ge HK
;
Gao J
;
Tan XQ
;
Xu P
;
Li LD
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Adobe PDF(895Kb)
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浏览/下载:330/47
  |  
提交时间:2018/11/08
Diffusion in liquids
Fracture
Ions
Matrix algebra
Rock mechanics
Shale
Shale gas
Diffusion experiments
Diffusion rate
Fracture matrix
Fracturing operations
Ion
diffusion rate
Low probability
Mineral composition
Reservoir characteristic
EXPERIMENTAL AND NUMERICAL STUDY OF THE CLOUD CAVITATING FLOW AROUND A SLENDER CYLINDER WITH A PETALS-SHAPED SECTION
会议论文
ASME Fluids Engineering Division Summer Meeting, Waikoloa, HI, JUL 30-AUG 03, 2017
作者:
Wang YW(王一伟)
;
Huang J(黄荐)
;
Xu C(徐畅)
;
Yu C(余超)
;
Huang CG(黄晨光)
;
Wu XC(吴小翠)
;
Wang, YW (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Mech Fluid Solid Coupling Syst, Beijing, Peoples R China.
;
Wang, YW (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
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Adobe PDF(1600Kb)
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浏览/下载:338/68
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提交时间:2018/01/16
Large-eddy Simulation
Hydrofoil
Propeller
Surface
Probability Distribution Evolution Algorithm to Inertial Parameters Identification for Space Target
会议论文
4th International Conference on Systems and Informatics (ICSAI), Hangzhou, PEOPLES R CHINA, NOV 11-13, 2017
作者:
Feng GH
;
Li WH(李文皓)
;
Zhang H(张珩)
;
Xiao XX(肖歆昕)
;
Zhang J(章杰)
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Adobe PDF(249Kb)
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浏览/下载:356/82
  |  
提交时间:2018/06/06
Probability Distribution Evolution Algorithm (Pde)
Inertial Parameters Identification
Space Target
Pseudo-inverse Solution Consistency