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北京航空航天大学 [6]

力学研究所 [5]

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	Influence of high temperature non-equilibrium effects on Mach 12 scramjet inlet 期刊论文 ACTA ASTRONAUTICA, 2022, 卷号: 193, 页码: 237-254 作者: Dai, Chunliang; Sun, Bo; Zhou, Shengbing; Zhuo, Changfei; Zhou, Changsheng 收藏 \| 浏览/下载：34/0 \| 提交时间：2022/05/17 Mach 12 scramjet inlet High temperature Non-equilibrium effects Thermochemical Inlet performance
	Evaluation of the effectiveness of VOC-contaminated soil preparation based on AHP-CRITIC-TOPSIS model 期刊论文 CHEMOSPHERE, 2021, 卷号: 271, 页码: 11 作者: Li, Yuan; Wei, Mingli; Liu, Lei; Yu, Bowei; Dong, Zhiwei 收藏 \| 浏览/下载：43/0 \| 提交时间：2021/05/25 VOC-Contaminated soil Homogeneity AHP-CRITIC-TOPSIS model Adsorption effect
	Differential Trends of Qinghai Spruce Growth with Elevation in Northwestern China during the Recent Warming Hiatus 期刊论文 FORESTS, 2019, 卷号: 10, 期号: 9, 页码: - 作者: Wang, Bin; Yu, Pengtao; Zhang, Lei; Wang, Yanhui; Yu, Yipeng 收藏 \| 浏览/下载：8/0 \| 提交时间：2020/09/09 Qinghai spruce warming hiatus elevation gradient tree growth growth-climate relationships
	Aero-thermal coupled design optimization of the non-axisymmetric endwall for a gas turbine blade 会议论文作者: Feng, Zhenping 收藏 \| 浏览/下载：17/0 \| 提交时间：2019/11/19 Aero-dynamic performance Aerodynamic and heat transfers Engineering applications Multi-objective genetic algorithm Numerical validations Static pressure coefficient Total pressure recovery coefficient Turbine blade aerodynamics
	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
	Effects of Radial Cooling Channel Length on Aero-Thermodynamic Performance of Air Cooled Flameholder [径向冷却通道长度对气冷稳定器气动热力性能的影响] 期刊论文 Tuijin Jishu/Journal of Propulsion Technology, 2018, 卷号: 39, 页码: 308-316 作者: Luo, Y.-F.; Liu, Y.-H.; Li, J.-N.; Xu, X.-P.; Zhang, Z.-X. 收藏 \| 浏览/下载：3/0 \| 提交时间：2019/12/30 Afterburners (engine) Afterburners (oven) Air Cooling systems Flow fields Mixing Navier Stokes equations Recovery Cooling channels Cooling performance Efficiency distributions External flow fields Flow loss Thermal mixing Thermodynamic performance Total pressure recovery coefficient Cooling
	Numerical investigation of effect of vortex generators on Bump inlet performance [涡流发生器对Bump进气道性能影响数值研究] 期刊论文 Hangkong Dongli Xuebao/Journal of Aerospace Power, 2018, 卷号: 33, 页码: 2476-2482 作者: He, T.; Wang, Q. 收藏 \| 浏览/下载：7/0 \| 提交时间：2019/12/30 Ducts Flow control Flow separation Intake systems Vortex flow Bump inlet External flow fields Numerical investigations Off-design points Total pressure distortion Total pressure recovery coefficient Total-pressure loss Vortex generators Computational fluid dynamics
	Numerical study on boundary layer suction at throat of a CARET inlet [一种CARET进气道喉部附面层抽吸数值研究] 期刊论文 Hangkong Dongli Xuebao/Journal of Aerospace Power, 2018, 卷号: 33, 页码: 2278-2284 作者: He, T.; Wang, Q. 收藏 \| 浏览/下载：3/0 \| 提交时间：2019/12/30 Computational fluid dynamics Flow control Flow fields Flow separation Recovery Boundary layer interaction Boundary layer suction CARET inlet Inlet performance Throat section Total pressure distortion Total pressure recovery Total pressure recovery coefficient Boundary layers
	Uncertainty Quantification of Cascade Manufacturing Error Based Non-Stationary Gaussian Process 期刊论文 Tuijin Jishu/Journal of Propulsion Technology, 2017, 卷号: 38, 页码: 1767-1775 作者: Yan, Yong; Zhu, Pei-Yuan; Song, Li-Ming; Li, Jun; Feng, Zhen-Ping 收藏 \| 浏览/下载：3/0 \| 提交时间：2019/11/26 Aero-dynamic performance Karhunen Loeve Expansion Manufacturing errors Nonstationary Reynolds-averaged navier stokes solvers Sparse grid Total pressure recovery coefficient Uncertainty quantifications
	Effect of notch width-ratio of core lobe to bypass lobe on performance of two-dimensional lobed mixer 会议论文 International Conference on Energy Engineering and Environmental Protection (EEEP), Sanya, PEOPLES R CHINA, 2016-11-21 作者: Wu, Jingyi; Fan, Weijun; Zhang, Rongchun; Zhang, Dawei 收藏 \| 浏览/下载：4/0 \| 提交时间：2019/12/30 Environmental protection Mixers (machinery) Mixing Flow direction Thermal mixing Total pressure recovery coefficient Width ratio Bypass ratio

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