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	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：46/0 \| 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
	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: Qi DW; He GW(何国威); Liu YM 收藏 \| 浏览/下载：60/0 \| 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：38/0 \| 提交时间：2015/12/18 vortex generators airfoil blunt trailing-edge