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Knowledge Management System of Institue of Mechanics, CAS
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Source Publication:AEROSPACE SCIENCE AND TECHNOLOGY
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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:223/49
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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:300/73
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Submit date:2021/11/15
Hypersonic combustion
Hydrogen
Improved Delayed Detached Eddy
Simulation (IDDES)
Dynamic zone flamelet model
Scramjet
Numerical modeling of a high-enthalpy shock tunnel driven by gaseous detonation
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 8
Authors:
Luo K(罗凯)
;
Wang Q(汪球)
;
Li JW(栗继伟)
;
Li JP(李进平)
;
Zhao W(赵伟)
Adobe PDF(2023Kb)
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View/Download:344/107
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Submit date:2020/11/30
Quasi-one-dimensional
Detonation
Shock tunnel
Shock speed
Investigation on rod-airfoil noise with high-order cell-centered finite difference method and acoustic analogy
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 102, 页码: 22
Authors:
Jin Y
;
Liao F(廖飞)
;
Cai JS
;
Morris PJ
Adobe PDF(7457Kb)
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View/Download:266/93
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Submit date:2020/07/06
Aeroacoustics
Rod-airfoil configuration
Cell-centered finite difference method
Delayed detached eddy simulation
FW-H acoustic analogy
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:412/150
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Submit date:2020/03/21
Supersonic combustion
Turbulence jet
Direct numerical simulations
Coherent structures
The design and main performance of a hydrogen peroxide/kerosene coaxial-swirl injector in a lab-scale rocket engine
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 70, 页码: 636-643
Authors:
Li HX(李慧鑫)
;
Ye L(叶亮)
;
Wei XL(魏小林)
;
Li T(李腾)
;
Li S(李森)
;
Wei, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
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Submit date:2017/12/18
H2o2/kerosene Bipropellant
Coaxial-swirl Injector
Geometric Constant
Performance
Numerical investigation of characteristic frequency excited highly underexpanded jets
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 63, 页码: 304-316
Authors:
Li XP
;
Fan E
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
;
Fan, XJ (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
Adobe PDF(3588Kb)
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View/Download:478/152
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Submit date:2017/07/24
Fuel Jets
Underexpanded Jets
Jet Mixing Control
Excited Jets
Large Eddy Simulation