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Plasma properties measurements of parallel-plane electrodes in Argon by coupling OES and PLIF 会议论文
Global Intelligent Industry Conference, 中国上海, 2020/10/28-30
Authors:  Wang FY(王方仪);  Zhang SH(张少华);  Yu XL(余西龙)
Adobe PDF(975Kb)  |  Favorite  |  View/Download：438/48  |  Submit date：2021/02/01
Application of dynamic zone flamelet model to a GH2/GO2 rocket combustor 会议论文
AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019
Authors:  Yao W(姚卫);  Li B(李波)
Adobe PDF(1665Kb)  |  Favorite  |  View/Download：173/51  |  Submit date：2020/11/20
Dynamic zone flamelet model  GH2/GO2  Large Eddy Simulation (LES)  Rocket combustor  Turbulence-chemistry interaction  
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
Authors:  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.
Adobe PDF(3818Kb)  |  Favorite  |  View/Download：328/128  |  Submit date：2018/01/16
Concave Surface Curvature  Adverse Pressure-gradient  Large-eddy Simulation  Reynolds-number  Near-wall  Flows  Separation  Vortices  Models  
Plasma Assisted Low Temperature Combustion 会议论文
22nd International Symposium on Plasma Chemistry (ISPC 22), Antwerp, BELGIUM, JUL 05-10, 2015
Authors:  Ju YG;  Lefkowitz JK;  Reuter CB;  Won SH;  Yang XL;  Yang S;  Sun WT;  Jiang ZL(姜宗林);  Chen Q;  Ju, YG (reprint author), Princeton Univ, Dept Mech & Aerosp Engn, Princeton, NJ 08544 USA.
Adobe PDF(2568Kb)  |  Favorite  |  View/Download：308/112  |  Submit date：2017/05/04
Plasma Assisted Combustion  Low Temperature Chemistry  Kinetics  Cool Flames  S-curve Transition  Nonequilibrium Plasma  Saturated-hydrocarbons  Diffusion Flames  Pulsed Discharge  Ignition  Mixtures  Oxidation  Kinetics  Enhancement  
Measurement of heat flux distribution of supercritical kerosene fueled supersonic combustor 会议论文
32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2016, Washington, DC, United states, June 13, 2016 - June 17, 2016
Authors:  Cheng D(程迪);  Wang J(王晶);  Gong J;  Lu Y(陆阳);  Yao W(姚卫);  Li L(李龙);  Fan XJ(范学军);  Fan, Xuejun (xfan@imech.ac.cn)
View  |  Adobe PDF(2131Kb)  |  Favorite  |  View/Download：352/128  |  Submit date：2017/05/05
Equivalence Ratios  Heat Flux Distributions  Heat Transfer Characteristics  Scramjet  Supercritical Kerosenes  Supersonic Combustion  Supersonic Combustors  Total Temperatures  
Three-dimensional numerical study of the acoustic properities of a highly underexpanded jet 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:  Wu K(吴坤);  Li XP(李晓鹏);  Yao W(姚卫);  Fan XJ(范学军)
View  |  Adobe PDF(590Kb)  |  Favorite  |  View/Download：414/100  |  Submit date：2017/05/05
Frequency Spectrum Analysis  High Temporal Resolution  Instantaneous Flow  Noise Generation Mechanisms  Theoretical Modeling  Three  Dimensional Numerical Studies  Transport Mechanism  Under  Expanded Jets  
Evaluation of BGK-type Models of the Boltzmann Equation 会议论文
the 29th International Symposium on Rarefied Gas Dynamics, Xi'an, China, July13-18，2014
Authors:  Gao W(高巍);  Sun QH(孙泉华)
View  |  Adobe PDF(656Kb)  |  Favorite  |  View/Download：978/288  |  Submit date：2015/01/01
The applicability of Mach number independence principle in case of hypersonic thermo-chemical nonequilibrium flow 会议论文
First International Conference on High Temperature Gas Dynamics, Beijing, 2012
Authors:  Li K(李康);  Li JP(李进平);  Jiang ZL(姜宗林)
View  |  Adobe PDF(1755Kb)  |  Favorite  |  View/Download：643/148  |  Submit date：2015/03/02
Keywords: Mach Number Independence  Oswatitsch  Nonequilibrium Flow  Real-gas Effect  Expansion Effect  
Splitting the Fast and Slow Motions in Molecular Dynamics Simulations Based on the Change of Cold Potential Well Bottom 会议论文
2nd International Symposium on Computational Mechanics, Hong Kong, PEOPLES R CHINA, NOV 30-DEC 03, 2009
Authors:  Zheng ZJ;  Bai YL(白以龙)
Adobe PDF(314Kb)  |  Favorite  |  View/Download：745/191  |  Submit date：2009/07/23
Molecular Simulations  Multiple-time Scale Problem  Cold Potential Well  
Numerical analyses of discrete gust response for a flexible aircraft 会议论文
21st AIAA Applied Aerodynamics Conference 2003, Orlando, FL, United states, June 23, 2003 - June 26, 2003
Authors:  Yang GW(杨国伟);  Obayashi S
View  |  Adobe PDF(1991Kb)  |  Favorite  |  View/Download：207/87  |  Submit date：2017/06/01
Direct-coupling Method  Dynamic Equations Of Motion  Flexible Aircraft  Flexible Airplane  Freedom Of Motion  One-minus-cosine Gust  Quasi-steady Model  Supersonic Transport