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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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State Key ... [5]
力学所知识产出(19... [2]
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岳连捷 [7]
张新宇 [7]
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张启帆 [3]
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Indexed By:SCI
Creator:岳连捷
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Document Type:期刊论文
Author:张新宇
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Flow structure of pressure transmission tube and its influence on unsteady pressure measuring results in compressible flow
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 108, 页码: 22
Authors:
Tong XT(仝晓通)
;
Zhang QF(张启帆)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
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Submit date:2021/03/03
Unsteady pressure measurement
Pressure sensor
Pressure transmission tube
Dynamic response
Compressible flow
Numerical study on the shock/combustion interaction of oblique detonation waves
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 13
Authors:
Yang L
;
Yue LJ(岳连捷)
;
Zhang QF(张启帆)
;
Zhang XY(张新宇)
Adobe PDF(5176Kb)
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Submit date:2020/11/30
Oblique detonation wave
Shock/combustion interaction
Shock polar analysis
High-resolution simulation
Numerical investigation of mode transition and hysteresis in a cavity-based dual-mode scramjet combustor
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 94, 页码: 10
Authors:
Zhang X(张旭)
;
Yue LJ(岳连捷)
;
Huang TL(黄庭隆)
;
Zhang QF(张启帆)
;
Zhang XY(张新宇)
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Submit date:2020/03/21
Hysteresis
Dual-mode scramjet
Supersonic combustion
Mode transition
Flame stabilization
Combustion oscillation
The vitiation effects of water vapor and carbon dioxide on the autoignition characteristics of kerosene
期刊论文
Acta Mechanica Sinica, 2014, 卷号: 30, 期号: 4, 页码: 485-494
Authors:
Liang JH(梁金虎)
;
Wang S(王苏)
;
Zhang ST(张胜涛)
;
Yue LJ(岳连捷)
;
Fan BC(范秉诚)
;
Zhang XY(张新宇)
;
Cui JP(崔季平)
;
Wang S(王苏)
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Submit date:2014/08/14
Ignition Delay
Vitiation Effect
Kerosene
Water
Carbon Dioxide
Shock Tube
Theoretical analysis of effects of boundary layer bleed on scramjet thrust
期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2013, 卷号: 56, 期号: 10, 页码: 1952-1961
Authors:
Yue LJ(岳连捷)
;
Xu XK(徐显坤)
;
Zhang XY(张新宇)
;
Yue, LJ (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:2013/10/23
Scramjet
Boundary Layer Bleed
Theoretical Analysis
Engine Thrust
Effects of entry conditions on cracked kerosene-fueled supersonic combustor performance
期刊论文
Combustion Science and Technology, 2007, 卷号: 179, 期号: 10, 页码: 2199-2217
Authors:
Fan XJ(范学军)
;
Yu G(俞刚)
;
Li JG(李建国)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
;
Sung CJ
;
Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100080, Peoples R China.
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Submit date:2009/08/03
Entry Conditions
Kerosene
Supersonic Combustion
Thermal Cracking
Model Combustor
Propulsion
Injection
An Experimental Study of Kerosene Combustion in a Supersonic Model Combustor Using Effervescent Atomization
期刊论文
Proceedings of the Combustion Institute, 2005
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)
;
Sung CJ
;
Yu, G (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100080, Peoples R China.
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Submit date:2007/06/15