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北京航空航天大学 [20]

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限定条件	专题：北京航空航天大学第一署名单位第一作者单位通讯作者单位

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	An improved AUSM-family scheme with robustness and accuracy for all Mach number flows 期刊论文 Applied Mathematical Modelling, 2020, 卷号: 77, 页码: 1065-1081 作者: Chen, Shu-sheng; Cai, Fang-jie; Xue, Hai-chao; Wang, Ning; Yan, Chao 收藏 \| 浏览/下载：62/0 \| 提交时间：2019/12/30
	Control of corner separation via dimpled surface for a highly loaded compressor cascade under different inlet Mach number 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 85, 页码: 48-60 作者: Lu, Huawei; Yang, Yi; Guo, Shuang; Pang, Wenxuan; Yang, Fan 收藏 \| 浏览/下载：9/0 \| 提交时间：2019/12/30 Highly loaded compressor cascade Dimple Flow loss Variation of inlet Mach number
	Hybrid CFD-CAA Numerical Simulation of Rotor-Stator Interaction Tonal Noise 会议论文 PROCEEDINGS OF 2019 16TH INTERNATIONAL BHURBAN CONFERENCE ON APPLIED SCIENCES AND TECHNOLOGY (IBCAST), 2019-01-01 作者: Akhtar, Tayyab Tahir; Li, Xiaodong; Tang, Xiaolong 收藏 \| 浏览/下载：7/0 \| 提交时间：2019/12/30 Acoustic generators Acoustic noise Acoustic variables control Aerodynamics Axial flow Boundary element method Boundary layers Computational fluid dynamics Frequency domain analysis Harmonic analysis Mach number NASA Numerical models Sailing vessels Shear flow Stators Advanced noise control fans Aerodynamically generated noise Discrete frequencies Frequency domains Higher order harmonics Pressure perturbation Rotor-stator interactions Rotor-stator interface Acoustic wave propagation
	Effects of shock tube length on step pressure waveform [激波管管长对阶跃压力波形的影响分析] 期刊论文 Zhendong yu Chongji/Journal of Vibration and Shock, 2019, 卷号: 38, 页码: 252-257 作者: Yang, J.; Xue, B. 收藏 \| 浏览/下载：31/0 \| 提交时间：2019/12/30 Aerodynamics Calibration Mach number Simulation platform Tubes (components) Attenuation coefficient Dynamic pressures Incident shock waves Platform time Pressure amplitudes Shock wave attenuations Simulation analysis Tube length Shock tubes
	Effective low-Mach number improvement for upwind schemes 期刊论文 COMPUTERS & MATHEMATICS WITH APPLICATIONS, 2018, 卷号: 75, 页码: 3737-3755 作者: Chen, Shu-sheng; Yan, Chao; Xiang, Xing-hao 收藏 \| 浏览/下载：3/0 \| 提交时间：2019/12/30 Upwind scheme Low Mach number Accuracy Asymptotic analysis Low dissipation Reliable
	Density enhancement mechanism of upwind schemes for low Mach number flows 期刊论文 ACTA MECHANICA SINICA, 2018, 卷号: 34, 页码: 431-445 作者: Lin, Bo-Xi; Yan, Chao; Chen, Shu-Sheng 收藏 \| 浏览/下载：3/0 \| 提交时间：2019/12/30 Energy equation Density fluctuation Roe TV-MAS Low speeds All speeds Computational fluid dynamics
	Preliminary experiment on spontaneous ignition performances of cavity-based strut flameholder [凹腔支板火焰稳定器自燃点火性能初步试验] 期刊论文 Hangkong Dongli Xuebao/Journal of Aerospace Power, 2018, 卷号: 33, 页码: 1298-1304 作者: Liu, Y.; Xie, Y.; Jin, J. 收藏 \| 浏览/下载：6/0 \| 提交时间：2019/12/30 Aerodynamics Atmospheric pressure Atmospheric temperature Ignition Mach number Struts Air temperature Bluff body Cavity Cavity structure Inlet temperature Spontaneous ignition Spray distances Temperature range Spontaneous combustion
	Hypersonic air inlet performance based on engineering transition model [基于工程转捩模型的高超声速进气道特性] 期刊论文 Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2018, 卷号: 44, 页码: 1408-1418 作者: Yang, H.; Lu, W.; Li, H.; Yue, L. 收藏 \| 浏览/下载：10/0 \| 提交时间：2019/12/30 Atmospheric thermodynamics Boundary layer flow Computer simulation Flight simulators Free flight Hypersonic boundary layers Location Mach number Numerical models Recovery Turbulence Boundary layer thickness Boundary layer transitions Flight height Free stream mach numbers Performance parameters Total pressure recovery coefficient Transition model Turbulence intensity Hypersonic inlets
	Aerodynamics of a Transonic Airfoil in Ground Effect 期刊论文 JOURNAL OF AIRCRAFT, 2018, 卷号: 55, 页码: 2240-2255 作者: Gao, Boshun; Qu, Qiulin; Agarwal, Ramesh K. 收藏 \| 浏览/下载：11/0 \| 提交时间：2019/12/30 Airfoils Angle of attack Angle of attack indicators Drag Ground effect Lift Lift drag ratio Mach number Supersonic aircraft Transonic aerodynamics Transonic flow Turbulence models Vortex flow Angle of attacks (AOA) Lift to drag ratio Reynolds Averaged Navier-Stokes Equations Spalart-Allmaras turbulence model Supercritical airfoils Transonic airfoils Transonic flight Wing in ground effect Navier Stokes equations
	Steady state error estimation and modification of a shielded thermocouple [屏蔽式总温热电偶的稳态误差分析及改型设计] 期刊论文 Hangkong Dongli Xuebao/Journal of Aerospace Power, 2018, 卷号: 33, 页码: 2784-2795 作者: Yang, W.; Zhang, W.; Zou, Z.; Wang, X.; Zhao, J. 收藏 \| 浏览/下载：5/0 \| 提交时间：2019/12/30 Aerodynamics Aircraft engines Heat transfer Mach number Numerical methods Thermocouples Wire Accuracy of measurements Area ratios Conjugate heat transfer High-accuracy measurements Length to diameter ratio Numerical simulation method Steady state errors Variation characteristics Errors

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