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Document Type:会议论文
Community:高温气体动力学国家重点实验室
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Modeling Analysis on Cavity-based Flame Stabilization in Scramjet Combustor
会议论文
12th Asia-Pacific Conference on Combustion, ASPACC 2019, Fukuoka, Japan, July 1, 2019 - July 5, 2019
Authors:
Wu K(吴坤)
;
Zhang P(张鹏)
;
Fan XJ(范学军)
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Submit date:2019/11/20
Combustion chemistry
Combustion dynamics
Dual
mode scramjet
Flame stabilization
Improved delayed detached eddy simulations
Overall reactions
Scramjet combustors
Shock
wave structures
Measurements of CO concentration distribution for Mars atmospheric entry by combining OES and TDLAS
会议论文
3rd International Symposium on Laser Interaction with Matter, Nanjing PEOPLES R CHINA, NOV 02-05 2014
Authors:
Lin X(林鑫)
;
Chen LZ
;
Ou DB
;
Li F(李飞)
;
Yu XL(余西龙)
;
oudongbin@sina.com
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Submit date:2015/09/29
Optical Emission Spectroscopy Tunable Diode Laser Absorption Spectroscopy Shock Wave
Temperature
Concentration
Multi-step Weighted Essentially Non-oscillatory Scheme
会议论文
2013 International Workshop on Numerical Methods and Modelling for Compressible Multimaterial Flows and Mixing, 中国北京, 2013-08-12
Authors:
Shen YQ(申义庆)
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Submit date:2015/09/10
Numerical Method
Weighted Essentially Non-oscillatory Scheme
Shock Wave
Complex Flowfield Simulation.
Combined TDLAS and OES technique for CO concentration measurement in shock-heated Martian atmosphere
会议论文
2nd International Symposium on Laser Interaction with Matter (LIMIS), Xian, PEOPLES R CHINA, SEP 09-12, 2012
Authors:
Lin X(林鑫)
;
Yu XL(余西龙)
;
Li F(李飞)
;
Zhang SH(张少华)
;
Xin JG
;
Zhang XY(张新宇)
;
Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Submit date:2013/12/12
Optical Emission Spectroscopy (Oes)
Tunable Diode Laser Absorption Spectroscopy (Tdlas)
Shock Wave
Temperature
Concentration
New Constructing Method for WENO Schemes
会议论文
7th Asian-Pacific Conference on Aerospace Technology and Science, 7th APCATS 2013, Taiwan, China, MAY 23-26, 2013
Authors:
Shen YQ(申义庆)
;
Liu L(刘利)
;
Yang Y(杨焱)
;
Gao Z(高智)
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Submit date:2014/03/11
Numerical Method
Weighted Essentially Non-oscillatory Scheme
Shock Wave
Complex Flowfield
A New Non-ablative TPS for Hypersonic Vehicles
会议论文
第十五届全国激波与激波管学术会议(上册), 中国浙江杭州, 2012-07-13
Authors:
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
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Submit date:2015/09/10
Hypersonic Flow
Tps
Shock Wave
Drag Reduction