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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
Energy-based drag decomposition analyses for a turbulent channel flow developing over convergent-divergent riblets
期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 2, 页码: 16
Authors:
Guo TB(郭同彪)
;
Fang,Jian
;
Zhong,Shan
;
Moulinec,Charles
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Submit date:2022/03/28
Three-dimensional simulation of ligament formation and breakup caused by external vibration
期刊论文
PHYSICS OF FLUIDS, 2020, 卷号: 32, 期号: 8, 页码: 17
Authors:
Li YK
;
Zhang M
;
Wu K(吴坤)
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Submit date:2020/10/23
Analysis of the influence of the vane width on the fluid transmission performance in the vane-type tank
会议论文
International Conference on Energy, Power and Mechanical Engineering (EPME2019), Guangzhou, China, 20-22 December 2019
Authors:
Zhuang BT(庄宝唐)
;
Li Y
;
Pan HL
;
Rui W
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Submit date:2020/06/15
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
High-Pressure Capturing Wing Configurations
期刊论文
AIAA JOURNAL, 2017, 卷号: 55, 期号: 6, 页码: 1909-1919
Authors:
Cui K(崔凯)
;
Li GL
;
Xiao Y(肖尧)
;
Xu YZ
;
Cui,K(reprint author), Chinese Acad Sci, Inst Mech
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Submit date:2017/07/24
Experimental Study of Ignition and Flame Characteristics of Surrogate of Cracked Hydrocarbon Fuels in Supersonic Crossflow
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Cheng LW(程柳维)
;
Zhong FQ(仲峰泉)
;
Wang ZP(王知溥)
;
Gu HB(顾洪斌)
;
Ma SG(马素刚)
;
Zhang XY(张新宇)
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Submit date:2018/01/16
Combustors
Cracks
Diesel Engines
Efficiency
Ethylene
Fighter Aircraft
Fuels
High Speed Cameras
Ignition
Kerosene
Luminance
Spacecraft
Stabilization
Starting Process in a Large-Scale Shock Tunnel
期刊论文
AIAA Journal, 2016, 卷号: 54, 期号: 5, 页码: 1240-1249
Authors:
Wang YP(汪运鹏)
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
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Submit date:2017/09/19
Starting Process in a Large-Scale Shock Tunnel
会议论文
22nd AIAA Computational Fluid Dynamics Conference, Dallas, TX, JUN 22-26, 2015
Authors:
Wang YP
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
;
Wang, YP (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:2016/06/28
Numerical investigation of the starting process in a long-test-duration hypersonic shock tunnel
会议论文
22nd AIAA Computational Fluid Dynamics Conference, 2015, Dallas, TX, United states, June 22, 2015 - June 26, 2015
Authors:
Wang YP(汪运鹏)
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
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Submit date:2017/05/05
Inviscid Flows
Numerical Investigations
Outlet Diameters
Reflected Shock Waves
Simulated Results
Starting Process
Transmitted Shock
Unsteady Nozzle Flow