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Knowledge Management System of Institue of Mechanics, CAS
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Indexed By:EI
Source Publication:AEROSPACE SCIENCE AND TECHNOLOGY
Document Type:期刊论文
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IDDES method based on differential Reynolds-stress model and its application in bluff body turbulent flows
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 119, 页码: 13
Authors:
Wang, Gang
;
Li, Quanzheng
;
Liu Y(刘毅)
Adobe PDF(4661Kb)
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View/Download:212/45
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Submit date:2022/06/11
Detached-eddy simulation
Reynolds-stress model
Massively separated flows
Tandem cylinders
Launch vehicle
Transonic buffet
Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 14
Authors:
Yao W(姚卫)
;
Liu H(刘杭)
;
Yue LJ(岳连捷)
;
Xiao YB(肖雅彬)
Adobe PDF(2954Kb)
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View/Download:290/67
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Submit date:2021/11/15
Hypersonic combustion
Hydrogen
Improved Delayed Detached Eddy
Simulation (IDDES)
Dynamic zone flamelet model
Scramjet
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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View/Download:279/61
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Submit date:2021/11/01
Store separation
Aerodynamic modeling
Interference aerodynamics
Dynamic simulation
Air-launch-to-orbit
A multi-time scale solution strategy for an elastomeric aircraft
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 103, 页码: 13
Authors:
Yang L(杨磊)
;
Sun QH(孙泉华)
Adobe PDF(1858Kb)
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View/Download:222/90
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Submit date:2020/08/26
Flight dynamic simulation
Multi-time scale
Elastomeric aircraft
Reduced order models
Store separation
DNS analysis of the effects of combustion on turbulence in a supersonic H2/air jet flow
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 93, 页码: 9
Authors:
Fu YW(符耀威)
;
Yu ZP(于长平)
;
Yan Z(闫正)
;
Li XL(李新亮)
Adobe PDF(2894Kb)
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View/Download:401/147
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Submit date:2020/03/21
Supersonic combustion
Turbulence jet
Direct numerical simulations
Coherent structures
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:385/138
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Submit date:2018/10/30
Inlet restart
Cowl shock
Shock wave boundary layer interactions
An efficient single-loop strategy for reliability-based multidisciplinary design optimization under non-probabilistic set theory
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 73, 页码: 148-163
Authors:
Wang XJ
;
Wang RX(王睿星)
;
Wang L
;
Chen XJ
;
Geng XY
Adobe PDF(3200Kb)
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Submit date:2018/10/30
Non-probabilistic reliability based
multidisciplinary design optimization
Single loop strategy
Uncertainty multidisciplinary analysis
Non-probabilistic reliability analysis
Translating distance calculation
Plasma-assisted ignition for a kerosene fueled scramjet at Mach 1.8
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2013, 卷号: 28, 期号: 1, 页码: 72-78
Authors:
Li F(李飞)
;
Yu XL(余西龙)
;
Tong YG(仝颖刚)
;
Shen Y(沈岩)
;
Chen J(陈健)
;
Chen LH(陈立红)
;
Zhang XY(张新宇)
;
Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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View/Download:1331/422
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Submit date:2013/07/30
Scramjet
Kerosene Fuel
Plasma Torch
Ignition