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仲峰泉 [13]
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Indexed By:SCI
Creator:仲峰泉
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Document Type:期刊论文
Author:张新宇
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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)
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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
Experimental study of flame characteristics of ethylene and its mixture with methane and hydrogen in supersonic combustor
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 86, 页码: 775-781
Authors:
Zhong FQ(仲峰泉)
;
Cheng LW(程柳维)
;
Gu HB(顾洪斌)
;
Zhang XY(张新宇)
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Submit date:2019/05/29
Supersonic combustor
Hydrocarbon
Mixture fuel
Flame structure
Ignition
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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Submit date:2018/12/12
impingement cooling
supercritical condition
heat transfer
kerosene
Numerical study on supersonic combustion of hydrogen and its mixture with Ethylene and methane with strut injection
期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2018, 卷号: 43, 期号: 15, 页码: 7591-7599
Authors:
Ma SG(马素刚)
;
Zhong FQ(仲峰泉)
;
Zhang XY(张新宇)
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Submit date:2018/07/17
Detached Eddy Simulation
Reduced Kinetic Mechanism
Supersonic Combustion
Hydrogen
Hydrocarbon
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
Numerical study of combustion and convective heat transfer of a Mach 2.5 supersonic combustor
期刊论文
APPLIED THERMAL ENGINEERING, 2015, 卷号: 89, 页码: 883-896
Authors:
Wang X
;
Zhong FQ(仲峰泉)
;
Gu HB(顾宏斌)
;
Zhang XY(张新宇)
;
Zhong, FQ (reprint author), 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
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Submit date:2016/01/08
Supersonic Combustor
Convective Heat Transfer
Numerical Study
Wall Heat Flux
Numerical study of heat transfer deterioration of turbulent supercritical kerosene flow in heated circular tube
期刊论文
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2015, 卷号: 85, 页码: 1003-1011
Authors:
Dang GX
;
Zhong FQ(仲峰泉)
;
Zhang YJ
;
Zhang XY(张新宇)
;
Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Bei Si Huan Xi Rd 15, Beijing 100190, Peoples R China.
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Submit date:2015/06/12
Supercritical Kerosene
Convective Heat Transfer
Turbulent Flow
Numerical Study
Numerical analysis on the heat transfer of three types of nozzles for the hypersonic long-run wind tunnel
期刊论文
Science China-Technological Sciences, 2015, 卷号: 58, 期号: 3, 页码: 470-475
Authors:
Xing YF(邢云绯)
;
Zhong FQ(仲峰泉)
;
Li DX(李东霞)
;
Zhang XY(张新宇)
;
Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Natl Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Submit date:2015/04/28
Hypersonic Scramjet Test Tunnel
Nozzle
Aerodynamic Heating
Convective Heat Transfer