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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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High-order simulation solving Navier-Stokes equations with Spalart–Allmaras turbulence model
会议论文
4th International Conference on Fluid Mechanics and Industrial Applications, FMIA 2020,, Asian Union of Information Technology, June 27, 2020 - June 28, 2020
Authors:
Yang L
;
岳连捷
;
张启帆
;
张新宇
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Submit date:2021/01/12
Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, PEOPLES R CHINA, MAR 06-09, 2017
Authors:
Yao W(姚卫)
;
Yuan YM(袁越明)
;
Li XP(李晓鹏)
;
Wang J(王晶)
;
Wu K(吴坤)
;
Fan XJ(范学军)
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Submit date:2018/06/06
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
Experimental and Modeling Investigation of CO2 Dissociation in Mars Entry Condition
会议论文
18th International Conference on the Methods of Aerophysical Research (ICMAR), Perm Natl Res Polytechn Univ, Perm, RUSSIA, JUN 27-JUL 03, 2016
Authors:
Lin X
;
Chen LZ
;
Peng JL
;
Li JP(李进平)
;
Li F(李飞)
;
Yu XL(余西龙)
Adobe PDF(1399Kb)
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Submit date:2017/05/12
Nonequilibrium
Concept of non-ablative thermal protection system for hypersonic vehicles
会议论文
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, CA, APR 11-14, 2011
Authors:
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
;
Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temperature Gas Dynam, Beijing 100190, Peoples R China.
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Submit date:2013/12/12
Research progress on high-enthalpy and hypersonic flows
会议论文
5th International Conference on Fluid Mechanics, Shanghai, PEOPLES R CHINA, AUG 15-19, 2007
Authors:
Jiang ZL(姜宗林)
;
Yu HR(俞鸿儒)
;
Lin ZB(林贞彬)
;
Jiang Z
Adobe PDF(690Kb)
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Submit date:2009/07/23
Hypersonic Flows
Detonation Driver
Shock-reflected Tunnels
Shock-expanded Tube
Heat Transfer
Integration property of a wedge-elliptic cone waverider with scramjet engine
会议论文
24th International Symposium on Shock Waves, JUL 11-16, 2004 Beijing, PEOPLES R CHINA, Beijing, PEOPLES R CHINA, JUL 11-16, 2004
Authors:
Liu H(刘宏)
;
Wang FM(王发民)
;
Li LW(李立伟)
;
Geng YB
;
Wang FM(王发民)
Adobe PDF(906Kb)
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Submit date:2007/12/18