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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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激波风洞智能测力方法研究与应用
学位论文
博士论文,北京: 中国科学院大学, 2024
Authors:
聂少军
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View/Download:21/7
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Submit date:2024/06/04
激波风洞
气动力试验
静态校准
动态校准
智能测力方法
背负式两体分离流动机理与安全分离方案研究
学位论文
博士论文,北京: 中国科学院大学, 2024
Authors:
王粤
Adobe PDF(35220Kb)
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Submit date:2024/06/04
两级入轨
级间分离
高超声速
非定常流动
气动干扰
Representation of Thermomechanical Damage in Fiber-Reinforced Ceramic Composites at High Thermal Gradients
期刊论文
AIAA JOURNAL, 2024, 页码: 11
Authors:
Wang JT(王江涛)
;
Yang ZM(杨正茂)
;
Yue LJ(岳连捷)
;
Yang, Rui
;
Jiao, Jian
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Submit date:2024/06/11
Thermodynamic Properties
Experimental study on shock interaction control of double wedge in high-enthalpy hypersonic flow subject to plasma synthetic jet
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2024, 卷号: 37, 期号: 4, 页码: 151-165
Authors:
Xie, Xuzhen
;
Liu, Qiang
;
Zhou, Yan
;
Luo, Zhenbing
;
Xie,Wei
;
Bai, Guanghui
;
Luo K(罗凯)
;
Wang Q(汪球)
;
Wu, Jianjun
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Submit date:2024/06/11
Hypersonic flow
High-enthalpy flow
Plasma synthetic jet
Shock wave
Flow control
Nonequilibrium Heating/Cooling Effects in a Mach Number 10 Hydrogen-Fueled Scramjet
期刊论文
JOURNAL OF PROPULSION AND POWER, 2024, 页码: 17
Authors:
Liu H(刘杭)
;
Yao W(姚卫)
;
Zhang X(张旭)
;
Zhang XY(张晓源)
;
Liu, Jianwen
;
Yue LJ(岳连捷)
;
Sun QH(孙泉华)
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Submit date:2024/03/11
Scramjet
Dynamic Zone Flamelet Model
High Enthalpy Shock Tunnel
Combustors
Improved Delayed Detached Eddy Simulation
Vibrational Energy
nonequilibrium heating
cooling effects
thermal nonequilibrium
chemical nonequilibrium
hydrogen
Comparison of the dynamic wake meandering model against large eddy simulation for horizontal and vertical steering of wind turbine wakes
期刊论文
RENEWABLE ENERGY, 2024, 卷号: 221, 页码: 22
Authors:
Rivera-Arreba, Irene
;
Li ZB(李曌斌)
;
Yang XL(杨晓雷)
;
Bachynski-Polic, Erin E.
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Submit date:2024/02/26
Wind turbine wake
Dynamic wake meandering
Large eddy simulation
Wake deflection
Wake steering
Investigation of Burst Pressure of Flat-Scored Metal Diaphragms in Hypersonic Impulse Facilities
期刊论文
AIAA JOURNAL, 2024, 页码: 8
Authors:
Wang WT(王文韬)
;
Wang Q(汪球)
;
Li JP(李进平)
;
Zhao W(赵伟)
;
Gao, Liangjie
;
Liu, Zhongchen
;
Qian, Zhansen
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Submit date:2024/02/26
Finite Element Method
Hypersonic
Shock Tube/Tunnel
Diaphragm
Burst Pressure
Experimental and numerical investigation on the unsteady interaction in longitudinal stage separation for parallel-staged two-body configuration
期刊论文
Physics of Fluids, 2024, 卷号: 36, 页码: 016116
Authors:
Wang Y(王粤)
;
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
Adobe PDF(7258Kb)
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Submit date:2024/01/15
Two-stage-to-orbit
Wind tunnel test
Numerical simulation
Stage separation
Hypersonic
Shock waves
Prediction of Transition Locations in Regions of the Minor Axis of Hypersonic Elliptic Cones using the BiGlobal-
e
N
Method
期刊论文
ADVANCES IN APPLIED MATHEMATICS AND MECHANICS, 2024, 页码: 28
Authors:
Zhao, Lei
;
Zhou, Wenqiang
;
Li XL(李新亮)
;
Zhang, Shaolong
;
Zhang, Yongming
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Submit date:2024/02/19
BiGlobal stability
transition
boundary layer
hypersonic elliptic cone
minor axis.