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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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Language:英语
Document Type:会议论文
Author:岳连捷
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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
Adobe PDF(1289Kb)
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Submit date:2021/01/12
Numerical Study of Heat Transfer on Confined Under-Expanded Impinging Jet from Slot into a Plenum
会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
Authors:
Huang TL(黄庭隆)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
Adobe PDF(714Kb)
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View/Download:36/17
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Submit date:2023/03/17
Downstream pressure variation induced hysteresis in the scramjet isolator
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Huang TL(黄庭隆)
;
Yue LJ(岳连捷)
;
Ma SH
;
Jia YN(贾轶南)
;
Zhang XY(张新宇)
;
Yue, Lianjie(yuelj@imech.ac.cn)
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View/Download:275/93
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Submit date:2018/01/16
Spacecraft
The Phenomena of Sudden Change in Hypersonic Inlets Self-Starting Capability
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Jia YN(贾轶南)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
;
Jia, Yinan(yuelj@imech.ac.cn)
Adobe PDF(566Kb)
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Submit date:2018/01/16
Boundary Layer Flow
Boundary Layers
Spacecraft
Wind Tunnels
Role of wall temperature on shock train in a rectangular isolator
会议论文
52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016, Salt Lake City, UT, United states, July 25, 2016 - July 27, 2016
Authors:
Lu HB
;
Wang D
;
Chen X
;
Yue LJ(岳连捷)
;
Ji, Feng (yuelj@imech.ac.cn)
Adobe PDF(560Kb)
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Submit date:2017/05/05
Aero
Heating
Dual Mechanisms
On Flow
Shock Train
Specific Heat Ratio
Total Pressure
Total Temperatures
Wall Temperatures
Iso-contraction-ratio methodology for the design of hypersonic inward turning inlets with shape transition
会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012
Authors:
Xiao YB(肖雅彬)
;
Yue LJ(岳连捷)
;
Chen LH(陈立红)
;
Zhang XY(张新宇)
;
Xiao YB(肖雅彬)
Adobe PDF(1674Kb)
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Submit date:2014/02/24
Investigation on a truncated streamline-traced hypersonic Busemann inlet
会议论文
15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Dayton, OH, United states, April 28, 2008 - May 1, 2008
Authors:
Xiao YB(肖雅彬)
;
Yue LJ(岳连捷)
;
Gong P
;
Chang XY(张新宇)
Adobe PDF(3472Kb)
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View/Download:216/85
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Submit date:2017/06/01
Boundary Layer Corrections
Busemann Inlet
Core Flow
Correction Method
Design Points
Finite Differential Methods
Internal Contraction Ratio
Internal Flows
Mass Flow
Research on three-dimensional scramjet inlet
会议论文
14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference, 2006, Beijing, China, 20-23 April 2006
Authors:
Yue LJ(岳连捷)
;
Xiao YB(肖雅彬)
;
Chen LH(陈立红)
;
Xiang AY(向安宇)
;
Zhang XY(张新宇)
Adobe PDF(1265Kb)
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Submit date:2015/09/21
Research on three-dimensional scramiet inlet
会议论文
14th AIAA/AHI International Space Planes and Hypersonics Systems Technologies Conference, Canberra, Australia, November 6, 2006 - November 9, 2006
Authors:
Yue LJ(岳连捷)
;
Chen LH(陈立红)
;
Xiao YB
;
Gong P
;
Chang XY(张新宇)
Adobe PDF(1267Kb)
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View/Download:152/51
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Submit date:2017/06/01
Capture Ratio
Mass Flow
Surface Oil Dot Visualization
Three-dimensional Scramjet Inlet
An Experimental Study of Kerosene Combustion in a Supersonic Model Combustor Using Effervescent Atomization
会议论文
30th International Symposium on Combustion, JUL 25-30, 2004 Univ Illinois Chicago, Chicago, IL
Authors:
Yu G(俞刚)
;
Li JG(李建国)
;
Zhao JR(赵建荣)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
;
Song ZR(宋知人)
Adobe PDF(1268Kb)
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View/Download:799/239
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Submit date:2007/12/18