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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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姜宗林 [14]
胡宗民 [6]
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Creator:姜宗林
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JF12复现风洞平板边界层转捩研究
会议论文
中国力学大会, 中国浙江杭州, 2019年8月25-28日
Authors:
刘美宽
;
韩桂来
;
姜宗林
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Submit date:2019/11/21
激波风洞
边界层
转捩
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
Authors:
Chen C(陈辰)
;
Luo ZT(罗长童)
;
Jiang ZL(姜宗林)
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Submit date:2018/06/06
Data-driven Modeling
Genetic Programming
Generalized Separable Model
Multi-level Block Search
高超声速下三维侧压进气道激波干扰的研究
会议论文
中国航天第三专业信息网第三十七届技术交流会暨第一届空天动力联合会议, 中国陕西西安, 2016-08-17
Authors:
项高翔
;
王春
;
姜宗林
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Submit date:2017/09/27
高超声速流动
体-翼激波干扰
波系结构
流场区域
Starting Process in a Large-Scale Shock Tunnel
会议论文
22nd AIAA Computational Fluid Dynamics Conference, Dallas, TX, JUN 22-26, 2015
Authors:
Wang YP
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
;
Wang, YP (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:2016/06/28
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.
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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
Numerical investigation of the starting process in a long-test-duration hypersonic shock tunnel
会议论文
22nd AIAA Computational Fluid Dynamics Conference, 2015, Dallas, TX, United states, June 22, 2015 - June 26, 2015
Authors:
Wang YP(汪运鹏)
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
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Submit date:2017/05/05
Inviscid Flows
Numerical Investigations
Outlet Diameters
Reflected Shock Waves
Simulated Results
Starting Process
Transmitted Shock
Unsteady Nozzle Flow
A New Flux Splitting Scheme for Euler Equations of Gas Dynamics
会议论文
International Conference on Numerical Analysis and Applied Mathematics, Rhodes GREECE, SEP 22-28 2014
Authors:
Li XD(李馨东)
;
Hu ZM(胡宗民)
;
Jiang ZL(姜宗林)
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Submit date:2015/09/29
Flux Splitting
Hybrid Upwind Method
Ausm Scheme
K-cusp Scheme
超声速圆柱尾流及其稳定性的数值模拟
会议论文
LHD2013夏季学术研讨会, 河北平山, 2013
Authors:
李馨东
;
胡宗民
;
滕宏辉
;
姜宗林
Adobe PDF(309Kb)
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Submit date:2014/01/23
超声速
分离流动
尾流
不稳定性
数值模拟
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)
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Submit date:2015/03/02
Keywords: Mach Number Independence
Oswatitsch
Nonequilibrium Flow
Real-gas Effect
Expansion Effect
JF16 膨胀管运行条件分析的数值问题
会议论文
LHD2012夏季学术研讨会, 吉林延吉, 2012
Authors:
胡宗民
;
李进平
;
姜宗林
Adobe PDF(909Kb)
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Submit date:2014/01/23
高焓
膨胀管
爆轰驱动
接触间断
数值振荡