机构

• 工程热物理研究所 [7]
• 力学研究所 [3]
• 合肥物质科学研究院 [1]

采集方式

• OAI收割 [11]

内容类型

• 期刊论文 [10]
• 会议论文 [1]

发表日期

• 2022 [1]
• 2021 [2]
• 2016 [2]
• 2012 [4]
• 2010 [1]
• 2004 [1]
• 更多

学科主题

• Engineerin... [1]
• Engineerin... [1]

筛选

浏览/检索结果: 共11条，第1-10条 帮助 条数/页： 5101520253035404550556065707580859095100 排序方式： 请选择题名升序题名降序提交时间升序提交时间降序作者升序作者降序发表日期升序发表日期降序 Effect of the trailing-edge flap on tones due to self-excited oscillation within the leading-edge slat cove 期刊论文  OAI收割 PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2022 作者:  Lu WS(陆维爽);  Liu, Peiqing;  Guo, Hao   |  收藏  |  浏览/下载：32/0  |  提交时间：2022/10/23 high-lift device  leading-edge slat  aerodynamic noise  acoustic characteristics  trailing-edge flap   Fluid-structure interaction-based aerodynamic modeling for flight dynamics simulation of parafoil system 期刊论文  OAI收割 NONLINEAR DYNAMICS, 2021, 页码: 22 作者:  Zhu, Hong;  Sun, Qinglin;  Liu, Xuefeng;  Liu, Jinglei;  Sun, Hao   |  收藏  |  浏览/下载：116/0  |  提交时间：2021/08/03 Fluid-structure interaction  Parafoil system  Flexible deformation  Trailing edge deflection  Aerodynamic performance  Dynamic model   Experimental Study of the Performance of a Propeller with Trailing-Edge Serrations 期刊论文  OAI收割 ACOUSTICS AUSTRALIA, 2021 作者:  Wei, Yuliang;  Qian, Yujie;  Bian, Shiyuan;  Xu, Feng;  Kong, Deyi   |  收藏  |  浏览/下载：30/0  |  提交时间：2021/04/26 Noise reduction  Propeller  Trailing-edge (TE) serration  Aerodynamic force  Unmanned aerial vehicle (UAV)   Numerical Study of Improving Aerodynamic Performance of Low Solidity LPT Cascade through Increasing Trailing Edge Thickness 期刊论文  OAI收割 2016 作者:  Li, C., Yan, P. G., Wang, X. F., Han, W. J. and Wang, Q. C. 收藏  |  浏览/下载：45/0  |  提交时间：2017/05/27 Aircraft engine low pressure turbine trailing edge thickness profile loss flow control vortex-generator jets separation control local variables   Numerical Study of Combining Steady Vortex Generator Jets and Deflected Trailing Edge to Reduce the Blade Numbers of Low Pressure Turbine Stage 期刊论文  OAI收割 2016 作者:  Li, C., Yan, P. G., Wang, X. F., Han, W. J. and Wang, Q. C. 收藏  |  浏览/下载：30/0  |  提交时间：2017/05/27 low pressure turbine  profile loss  flow control  Vortex Generator Jets  deflected trailing edge  separation control  local variables  part i transition   Effect of Smart Rotor Control Using a Deformable Trailing Edge Flap on Load Reduction under Normal and Extreme Turbulence 期刊论文  OAI收割 ENERGIES, 2012, 卷号: 5, 期号: 9, 页码: 3608-3626 作者:  Yu, Wei;  Zhang, Ming Ming;  Xu, Jian Zhong 收藏  |  浏览/下载：24/0  |  提交时间：2015/11/03 smart rotor control  deformable trailing edge flap  load  turbulent wind  PID controller   Heat Transfer in Internal Channel of a Blade: Effects of Rotation in a Trailing Edge Cooling System 期刊论文  OAI收割 JOURNAL OF THERMAL SCIENCE, 2012, 卷号: 21, 期号: 3, 页码: 236,249 Luca Andrei; Antonio Andreini; Leonardo Bonanni; Bruno Facchini 收藏  |  浏览/下载：15/0  |  提交时间：2013/01/07 heat transfer  trailing edge  pedestal  rotation number  OpenFOAM  CFD  TLC thermography   Heat Transfer in Internal Channel of a Blade: Effects of Rotation in a Trailing Edge Cooling System 期刊论文  OAI收割 JOURNAL OF THERMAL SCIENCE, 2012, 卷号: 21, 期号: 3, 页码: 236,249 作者:  Luca Andrei;  Antonio Andreini;  Leonardo Bonanni;  Bruno Facchini   |  收藏  |  浏览/下载：22/0  |  提交时间：2013/01/07 Heat Transfer  Trailing Edge  Pedestal  Rotation Number  Openfoam  Cfd  Tlc Thermography   Lattice Boltzmann Simulations of a pitch-up and pitch-down maneuver of a span-wise flexible wing in a free stream flow Read More: http://arc.aiaa.org/doi/abs/10.2514/6.2012-300 会议论文  OAI收割 50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Nashville, TN, United states, JAN 09-12, 2012 作者:   收藏  |  浏览/下载：59/0  |  提交时间：2013/02/26 Aerospace engineering  Deformation  Exhibitions  Flexible wings  Reynolds number  Rigidity  Vortex flow  Aerodynamic forces  Chord-based Reynolds number  Flexural rigidities  Free stream  Free-stream flow  Lattice boltzmann  Leading-edge vortices  Lift coefficient  Lift force  Particle methods  Pitch rate  Power efficiency  Reduced frequency  Three dimensional space  Time-periods  Tip edge  Trailing edges  Trailing vortex   Simulation of aerodynamic performance affected by vortex generators on blunt trailing-edge airfoils 期刊论文  OAI收割 SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2010, 卷号: 53, 期号: 1, 页码: 1-7 作者:  Yang Ke;  Zhang Lei;  Xu JianZhong 收藏  |  浏览/下载：37/0  |  提交时间：2015/12/18 vortex generators  airfoil  blunt trailing-edge