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Indexed By:EI
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Experimental Study of Kerosene Ignition and Flame Stabilization in a Supersonic Combustor
期刊论文
International Journal of Turbo & Jet-Engines, 2022, 卷号: 39, 期号: 3, 页码: 403-410
Authors:
Meng Y(孟宇)
;
Gu HB(顾洪斌)
;
Zhang XY(张新宇)
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Submit date:2021/10/29
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)
Adobe PDF(8067Kb)
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View/Download:404/71
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Submit date:2021/03/03
Unsteady pressure measurement
Pressure sensor
Pressure transmission tube
Dynamic response
Compressible flow
Numerical investigation on flow nonuniformity-induced hysteresis in scramjet isolator
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3176-3188
Authors:
Huang TL(黄庭隆)
;
Yue LJ(岳连捷)
;
Ma SH(马生虎)
;
Zhang QF(张启帆)
;
Zhang, Peng
;
Zhang XY(张新宇)
Adobe PDF(3937Kb)
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Submit date:2021/03/30
Adverse pressure gradient
Back pressure
Hysteresis effects
Non-uniform flow
Shock train
Experimental and numerical investigation on flow and heat transfer of impingement jet cooling of kerosene
期刊论文
INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER, 2020, 卷号: 116, 页码: 8
Authors:
Du MM(杜蒙蒙)
;
Zhong FQ(仲峰泉)
;
Xing YF(邢云绯)
;
Zhang XY(张新宇)
Adobe PDF(2316Kb)
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Submit date:2020/08/26
Impingement jets
Kerosene
Heat transfer coefficient
Pressure loss
Reynolds number
Numerical study of convective heat transfer of a supersonic combustor with varied inlet flow conditions
期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 5, 页码: 943-953
Authors:
Fan WH(范文慧)
;
Zhong FQ(仲峰泉)
;
Ma SG(马素刚)
;
Zhang XY(张新宇)
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Submit date:2020/03/11
Wall heat flux
Numerical simulation
Ethylene
Supersonic combustor
CH* Luminance Distribution Application and a One-Dimensional Model of the Supersonic Combustor Heat Release Quantization
期刊论文
INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2019, 卷号: 36, 期号: 1, 页码: 45-50
Authors:
Wang ZP(王知溥)
;
Gu HB(顾洪斌)
;
Cheng L W
;
Zhong FQ(仲峰泉)
;
Zhang XY(张新宇)
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Submit date:2019/04/11
supersonic combustion
one-dimensional modelling
heat release
CH* chemiluminescence
Numerical Study of Impingement Cooling of Aviation Kerosene at Supercritical Conditions
期刊论文
JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 2018, 卷号: 140, 期号: 11, 页码: Ar-112201
Authors:
Xing YF(邢云绯)
;
Zhong FQ(仲峰泉)
;
Zhang XY(张新宇)
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View/Download:333/137
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Submit date:2018/12/12
impingement cooling
supercritical condition
heat transfer
kerosene
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)
Adobe PDF(2110Kb)
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View/Download:386/138
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Submit date:2018/10/30
Inlet restart
Cowl shock
Shock wave boundary layer interactions
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
Engine performance analysis and optimization of a dual-mode scramjet with varied inlet conditions
期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 1, 页码: 75-82
Authors:
Tian L
;
Chen LH(陈立红)
;
Chen Q(陈强)
;
Zhong FQ(仲峰泉)
;
Zhang XY(张新宇)
;
Chen, LH (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:2016/09/14
Dual-mode Scramjet
Engine Performance
Thrust
Optimization
Heat Release Distribution
Simulated Annealing Algorithm