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	Analysis of Influencing Factors on Lift Coefficients of Autonomous Sail-boat Double Sail Propulsion System Based on Vortex Panel Method 期刊论文 OAI收割 China Ocean Engineering, 2019, 卷号: 33, 期号: 6, 页码: 746-752 作者: Sun ZY(孙朝阳); Yu JC(俞建成); Zhang AQ(张艾群); Jin QL( 金乾隆) \| 收藏 \| 浏览/下载：31/0 \| 提交时间：2020/01/11 autonomous sailboat wing sail double sail vortex panel method lift coefficient
	Effects of accessory parts topology on the aerodynamics of high-speed trains 会议论文 OAI收割 Cagliari, Sardinia, Italy , 5-8 April 2016 作者: Zhang Y(张业); Sun ZX(孙振旭); Guo DL(郭迪龙); Yang GW(杨国伟) \| 收藏 \| 浏览/下载：31/0 \| 提交时间：2018/11/08 Aerodynamics Bogies (railroad rolling stock) Electric current collection Pantographs Railroad cars Railroads Speed Topology Vehicle performance Aero dynamic performance High speed train (HST) Key factors Lift coefficient Local optimizations Running speed Total drags
	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：58/0 \| 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
	A strong coupled CFD-CSD method on computational aeroelastity (EI CONFERENCE) 会议论文 OAI收割 2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011, July 15, 2011 - July 17, 2011, Inner Mongolia, China Xi R.; Jia H. 收藏 \| 浏览/下载：67/0 \| 提交时间：2013/03/25 In this paper a strong coupled CFD-CSD method is developed to simulate the aeroelastic phenomena. The CFD solver is based on the finite-volume algorithm for the Navier-Stokes equations on unstructured grid. The CSD solver solves the aeroelastic governing equations in the modal space. Their coupling is realized by a dual-time method. The spring-based smoothing method is adopted to deform and regenerate the aerodynamic grid. Two test cases are selected to validate the authors' method for static and dynamic aeroelastity .The results of the simulation for the static aeroelastic problems of a missile wing show that the Lift Coefficient and Drag Coefficient are severally 7% and 5% lower than those don't consider the elasticity of the wing. The results for the flutter boundary prediction of the AGARD 445.6 wing have been proved much closer to the experiment than using the DLM. This method can describe the effects of fluid viscosity more exactly for highly nonlinear transonic flight conditions. The calculation has proved reliable in the subsonic regime but not accurate enough in the supersonic regime. 2011 IEEE.
	Effect of Streamwise Fences on Secondary Flows and Losses in a Two-dimensional Turbine Rotor Cascade 期刊论文 OAI收割 JOURNAL OF THERMAL SCIENCE, 2006, 卷号: 15, 期号: 4, 页码: 296,305 M. Govardhan; A. Rajender; J. P. Umang 收藏 \| 浏览/下载：16/0 \| 提交时间：2013/01/31 Turbine cascade streamwise fences loss core lift coefficient
	Kinetic and technical studies on large-scale culture of Rhodiola sachalinensis compact callus aggregates with air-lift reactors 期刊论文 OAI收割 Journal of Chemical Technology and Biotechnology, 1998, 期号: 3, 页码: 227-234 Xu, J. F.; Xie, J.; Han, A. M.; Feng, P. S.; Su, Z. G. 收藏 \| 浏览/下载：21/0 \| 提交时间：2013/11/15 Rhodiola sachalinensis salidroside plant cell culture aggregates air-lift reactor oxygen transfer coefficient plant-cell cultures tissue-cultures growth accumulation root