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力学研究所 [8]

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西安交通大学 [2]

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	Standing oblique detonation for hypersonic propulsion: A review 期刊论文 PROGRESS IN AEROSPACE SCIENCES, 2023, 卷号: 143, 页码: 17 作者: Jiang ZL(姜宗林) 收藏 \| 浏览/下载：0/0 \| 提交时间：2024/02/26 Standing oblique detonation Scramjet engine Oblique detonation engine Shock wave Supersonic combustion Hypersonic ramjet propulsion
	Criteria for hypersonic airbreathing propulsion and its experimental verification 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104 作者: Jiang ZL(姜宗林); Zhang ZJ(张子健); Liu YF(刘云峰); Wang C(王春); Luo ZT(罗长童) 收藏 \| 浏览/下载：50/0 \| 提交时间：2021/05/17 Concept demonstration Hypersonic propulsion Oblique detonation engine Scramjet Shock wave Supersonic combustion Wind tunnel test
	Aerodynamic principles of shock-induced combustion ramjet engines 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 103, 页码: 8 作者: Ma KF(马凯夫); Zhang ZJ(张子健); Liu YF(刘云峰); Jiang ZL(姜宗林) 收藏 \| 浏览/下载：17/0 \| 提交时间：2020/08/26 Scramjet engines Shock-induced combustion ramjet engines Supersonic combustion Chapman-Jouguet detonation
	Reconstruction of two-dimensional velocity distribution in scramjet by laser absorption spectroscopy tomography 期刊论文 APPLIED OPTICS, 2019, 卷号: 58, 页码: 205-212 作者: Qu, Qianwei; Cao, Zhang; Xu, Lijun; Liu, Chang; Chang, Liuyong 收藏 \| 浏览/下载：13/0 \| 提交时间：2019/12/30 Absorption spectroscopy Angular distribution Computational fluid dynamics Flow fields Image reconstruction Image segmentation Iterative methods Laser beams Molecules Nonlinear equations Ordinary differential equations Ramjet engines Tomography Velocity Absorbance coefficients Distribution of water High-speed flow fields Interior point algorithm Landweber iteration algorithms Laser absorption spectroscopy Simplified equations Two Dimensional (2 D) Velocity distribution
	辐射加热碳氢燃料主动冷却特性研究学位论文北京: 中国科学院大学, 2018 作者: 董达收藏 \| 浏览/下载：45/0 \| 提交时间：2018/05/29 超燃冲压发动机再生冷却辐射加热平板冷却结构 Ledinegg失稳
	Numerical simulation of heat transfer of n-decane under supercritical pressure in horizontal rectangular cooling channels [超临界压力下正癸烷在水平矩形冷却通道内的流动传热数值模拟] 期刊论文 Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2018, 卷号: 39 作者: Zhang, Z.; Huang, S.; Gao, X. 收藏 \| 浏览/下载：4/0 \| 提交时间：2019/12/02 Buoyancy Computational fluid dynamics Cooling Engines Heat flux Location Numerical models Paraffins Ramjet engines, Active cooling Distribution of temperature Heat Transfer enhancement Heat transfer predictions Hydrocarbon fuel Rectangular cooling channels Simulation of heat transfer Super-critical pressures, Heat transfer performance
	Fluorescence and absorption characteristics of p-xylene: applicability for temperature measurements 期刊论文 APPLIED PHYSICS B-LASERS AND OPTICS, 2017, 卷号: 123, 期号: 9 作者: Wang, Qianlong; Zhang, Yuyin; Jiang, Liqiao; Zhao, Daiqing; Guibert, Philippe 收藏 \| 浏览/下载：25/0 \| 提交时间：2017/11/24
	Development of zone flamelet modelfor scramjet combustor modeling 会议论文 Xiamen, China, March 6, 2017 - March 9, 2017 作者: Yao W(姚卫); Fan XJ(范学军) 收藏 \| 浏览/下载：30/0 \| 提交时间：2018/11/08 Combustion Cost benefit analysis Costs Mixtures Ramjet engines Supersonic aircraft Computational costs Equivalence ratios Local flow conditions Scramjet combustors Statistics approaches Supersonic combustion Supersonic combustors Turbulent combustion
	A low-dissipation solver based on openFOAM designed for large eddy simulation in compressible flow 会议论文 Xiamen, China, March 6, 2017 - March 9, 2017 作者: Lee YC; Yao W(姚卫); Fan XJ(范学军) 收藏 \| 浏览/下载：49/0 \| 提交时间：2018/11/08 Computational Fluid Dynamics Digital Storage Kinetic Energy Kinetics Open Source Software Open Systems Ramjet Engines Runge Kutta Methods Shock Tubes Turbulence Two Phase Flow Bench Mark Problems Central Upwind Scheme Computational Fluid Dynamics Software Skew Symmetric Forms Temporal Discretization Turbulence Structures Unstructured Meshes Wall Bounded Turbulence
	Classification of Combustor-Inlet Interactions for Airbreathing Ramjet Propulsion 期刊论文 AIAA JOURNAL, 2015 Cui, Tao; Wang, Yong; Liu, Kai; Jin, Jianren 收藏 \| 浏览/下载：5/0 \| 提交时间：2017/12/03 TRANSONIC DIFFUSER FLOW MODE TRANSITION HYSTERESIS PHENOMENON SCRAMJET ENGINES SUPERSONIC INLET SHOCK POSITION UNSTART OSCILLATIONS DYNAMICS SIMULATION

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