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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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力学所知识产出(19... [2]
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岳连捷 [10]
张新宇 [10]
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Creator:岳连捷
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Parameters for evaluating the efficiency of inlet compression
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 12, 页码: 51-56
Authors:
Chen KT(陈科挺)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
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Submit date:2022/01/12
Airbreathing engine
Compression efficiency
Compression quality
Inlet
Self-consistency
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
Experimental study of mode transition characteristics of a cavity-based scramjet combustor during acceleration
期刊论文
Aerospace Science and Technology, 2019, 卷号: 93, 期号: 10, 页码: UNSP 105316
Authors:
Meng Y(孟宇)
;
Gu HB(顾洪斌)
;
Zhuang JH(庄金衡)
;
Sun WM(孙文明)
;
Gao ZB(高占彪)
;
Lian H(连欢)
;
Yue LJ(岳连捷)
;
Chang XY(张新宇)
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Submit date:2019/10/15
Scramjet Combustor Mode Transition Liquid Kerosene Acceleration
Numerical study of a fully confined supersonic slot impinging jet from bleed system
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 90, 页码: 12-22
Authors:
Huang TL(黄庭隆)
;
Yue LJ(岳连捷)
;
Chang XY(张新宇)
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Submit date:2019/09/09
Fully confined supersonic jet
Inclined impingement
Heat transfer
Boundary layer bleed
Numerical simulation
Effect of cowl shock on restart characteristics of simple ramp type hypersonic inlets with thin boundary layers
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 74, 页码: 72-80
Authors:
Yue LJ(岳连捷)
;
Jia YN(贾轶南)
;
Xu X
;
Zhang XY(张新宇)
;
Zhang P(张鹏)
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Submit date:2018/10/30
Inlet restart
Cowl shock
Shock wave boundary layer interactions
Flow characteristics of hypersonic inlets with different cowl-lip blunting methods
期刊论文
SCIENCE CHINA-Physics, Mechanics & Astronomy, 2014, 卷号: 57, 期号: 4, 页码: 741-752
Authors:
Lu HB(卢洪波)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
;
Yue LJ(岳连捷)
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Submit date:2014/04/15
Hypersonic Inlet
Cowl-lip Bluntness
Flow Characteristics
Shock Pattern
Shock Interference
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
大内收缩比二元高超声速进气道波系配置特性
期刊论文
推进技术, 2012, 卷号: 33, 期号: 4, 页码: 505-509
Authors:
张晓嘉
;
岳连捷
;
张新宇
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Submit date:2013/01/16
超燃冲压发动机
二元高超声速进气道
波系配置
附面层抽吸
带中心支板侧压进气道流场特性研究
期刊论文
实验流体力学, 2008, 卷号: 22, 期号: 1, 页码: 31-35
Authors:
龚鹏
;
岳连捷
;
肖雅斌
;
王世芬
;
张新宇
Adobe PDF(621Kb)
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Submit date:2010/05/03
超燃冲压发动机
高超声速进气道
侧压式进气道
支板
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