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Advances in plasma-assisted ignition and combustion for combustors of aerospace engines
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 27
Authors:
Li, Mengzhe
;
Wang, Zhikai
;
Xu, Rongguang
;
Zhang, Xiaoliang
;
Chen, Zhitong
;
Wang Q(汪球)
Adobe PDF(8841Kb)
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View/Download:282/109
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Submit date:2021/11/01
Non-equilibrium plasma
Plasma-assisted ignition
Plasma-assisted combustion
Aerospace engine
Combustor
Extreme condition
Longitudinal aerodynamic modeling and verification for air-launch-to-orbit system during stage separation
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 21
Authors:
Yang L(杨磊)
;
Ye, Zhengyin
;
Li WH(李文皓)
;
Sun QH(孙泉华)
Adobe PDF(4621Kb)
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Submit date:2021/11/01
Store separation
Aerodynamic modeling
Interference aerodynamics
Dynamic simulation
Air-launch-to-orbit
A sharp interface immersed boundary method for flow-induced noise prediction using acoustic perturbation equations
期刊论文
COMPUTERS & FLUIDS, 2021, 卷号: 227, 页码: 15
Authors:
Zhao, Cheng
;
Yang Y(杨焱)
;
Zhang, Tao
;
Dong, Haibo
;
Hou, Guoxiang
Adobe PDF(3919Kb)
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Submit date:2021/08/30
Acoustic perturbation equations
Immersed boundary method
Flow-induced noise
Four-cylinder array
Numerical and experimental study on high-speed hydrogen-oxygen combustion gas flow and aerodynamic heating characteristics
期刊论文
PHYSICS OF FLUIDS, 2021, 卷号: 33, 期号: 7, 页码: 11
Authors:
Yu JP(于江鹏)
;
Li JP(李进平)
;
Wang Q(汪球)
;
Zhang SZ(张仕忠)
;
Zhang XY(张晓源)
Adobe PDF(3271Kb)
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Submit date:2021/11/01
Direct numerical simulation of impinging shock wave and turbulent boundary layer interaction over a wavy-wall
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 5, 页码: 350-363
Authors:
Tong FL(童福林)
;
Sun D(孙栋)
;
Li XL(李新亮)
Adobe PDF(4402Kb)
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View/Download:216/51
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Submit date:2021/06/07
Direct numerical simulation
Low-frequency unsteadiness
Shock waves
Turbulent boundary layer
Wavy-wall
Incident shock wave and supersonic turbulent boundarylayer interactions near an expansion corner
期刊论文
COMPUTERS & FLUIDS, 2020, 卷号: 198, 页码: 18
Authors:
Tong FL(童福林)
;
Li XL(李新亮)
;
Yuan XX
;
Yu ZP(于长平)
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Submit date:2020/04/07
Shock wave
Turbulent boundary layer
Unsteadiness
Expansion corner
Numerical investigation of mode transition and hysteresis in a cavity-based dual-mode scramjet combustor
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 94, 页码: 10
Authors:
Zhang X(张旭)
;
Yue LJ(岳连捷)
;
Huang TL(黄庭隆)
;
Zhang QF(张启帆)
;
Zhang XY(张新宇)
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View/Download:354/124
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Submit date:2020/03/21
Hysteresis
Dual-mode scramjet
Supersonic combustion
Mode transition
Flame stabilization
Combustion oscillation
Statistical analysis of temperature distribution on vortex surfaces in hypersonic turbulent boundary layer
期刊论文
PHYSICS OF FLUIDS, 2019, 卷号: 31, 期号: 10, 页码: 7
Authors:
Lin X(林鑫)
;
Tong FL(童福林)
;
Yu ZP(于长平)
;
Li XL(李新亮)
Adobe PDF(3152Kb)
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Submit date:2020/03/11
Experimental Investigation of Fuel Composition and Mix-Enhancer Effects on the Performance of Paraffin-Based Hybrid Rocket Motors
期刊论文
Aerospace Science and Technolog, 2018, 页码: 10.1016/j.ast.2018.09.026
Authors:
Wu Y(武毅)
;
Yu XL(余西龙)
;
Lin X(林鑫)
;
Li S(李森)
;
Wei XL(魏小林)
;
Zhu C
;
Wu LL
Adobe PDF(2794Kb)
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Submit date:2018/11/06
Numerical analysis of confined flow past permeable square cylinder with CE/SE method
期刊论文
PROGRESS IN COMPUTATIONAL FLUID DYNAMICS, 2016, 卷号: 16, 期号: 5, 页码: 281-287
Authors:
Yang LH
;
Yang DX
;
Zhang LZ
;
Zhang DL(张德良)
;
Xue ZQ
;
Yang, DX (reprint author), CEA, Inst Crustal Dynam, Beijing, Peoples R China.
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View/Download:264/93
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Submit date:2016/12/08
Porous Media
Unsteady Flow
Ce/se Method
Computational Fluid Dynamics
Cfd