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Document Type:期刊论文
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基于主动射流控制的高超声速进气道再起动性能研究(英文)
期刊论文
Transactions of Nanjing University of Aeronautics and Astronautics, 2022, 卷号: 39, 期号: 06, 页码: 651-662
Authors:
靳一超
;
姚卫
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Submit date:2023/02/09
高超声速进气道
不起动
再起动
主动射流
流动控制
Design of a new supersonic biplane
期刊论文
Acta Astronautica, 2020, 卷号: 175, 期号: 10, 页码: 216-233
Authors:
Zhai J
;
Zhang CA(张陈安)
;
Wang FM(王发民)
;
Zhang WW
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Submit date:2020/06/08
An Ensemble Convolutional Neural Networks for Bearing Fault Diagnosis Using Multi-Sensor Data
期刊论文
Sensors, 2019, 卷号: 19, 期号: 23, 页码: 5300
Authors:
Liu Y(刘洋)
;
Yan XS
;
Zhang CA(张陈安)
;
Liu W(刘文)
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Submit date:2020/01/02
Rotating Machinery
Fault Diagnosis
Multi-sensor Fusion
Convolutional Neural Network
Ensemble Model
An Experimental Study of Chilton-Colburn Analogy Between Turbulent Flow and Convective Heat Transfer of Supercritical Kerosene
期刊论文
JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 2017, 卷号: 139, 期号: 6
Authors:
Zhang YJ(张永江)
;
Zhong FQ(仲峰泉)
;
Xing YF(邢云绯)
;
张新宇 Xinyu
;
Zhong, FQ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Bei Si Huan Xi Rd 15, Beijing 100190, Peoples R China.
;
Zhong, FQ (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
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Submit date:2017/07/24
Aviation Kerosene
Supercritical
Skin Friction Coefficient
Convective Heat Transfer
Chilton-colburn Analogy
Local Piston Theory with Viscous Correction and Its Application
期刊论文
AIAA Journal, 2017, 卷号: 55, 期号: 3, 页码: 942-954
Authors:
Liu W(刘文)
;
Zhang CA(张陈安)
;
Han HQ
;
Wang FM(王发民)
;
Zhang, CA (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:2017/03/28
Hypersonic
Unsteady Aerodynamics
Piston Theory
Aeroelasticity
Numerical Study of Unsteady Properties of Ethylene/Air Turbulent Jet Diffusion Flame with Detached Eddy Simulation
期刊论文
INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2016, 卷号: 33, 期号: 4, 页码: 407-411
Authors:
Ma SG
;
Zhong FQ(仲峰泉)
;
Zhang XY(张新宇)
;
Zhong, FQ (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:2017/02/24
Combustion
Ignition
Hydrocarbon Fuel
Reduced Mechanism
Detached Eddy Simulation
Design methodology for shape transition inlets based on constant contraction of discrete streamtubes
期刊论文
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2016, 卷号: 230, 期号: 8, 页码: 1496-1506
Authors:
Xiao YB(肖雅斌)
;
Yue LJ(岳连捷)
;
Ma SH
;
Zhang XY(张新宇)
;
Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100864, Peoples R China.
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Submit date:2016/09/14
Hypersonic Inlet
Shape Transition
Inward Turning
Scramjet
Design Method
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
Development of efficient and accurate skeletal mechanisms for hydrocarbon fuels and kerosene surrogate
期刊论文
ACTA MECHANICA SINICA, 2015, 卷号: 31, 期号: 5, 页码: 732-740
Authors:
Zhong FQ(仲峰泉)
;
Ma SG
;
Zhang XY(张新宇)
;
Sung CJ
;
Niemeyer KE
;
Zhong, FQ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
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Submit date:2016/01/08
Reduced Chemistry
Hydrocarbons
Directed Relation Graph
Ignition Delay Time