中国科学院机构知识库网格系统: 检索

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	Capillary-driven flows in eccentric annuli under microgravity 期刊论文 OAI收割 ARCHIVE OF APPLIED MECHANICS, 2022, 页码: 13 作者: Chen ST(陈上通); Guo, Lei; Li, Yong; Liu, Jintao; Kang Q(康琦) \| 收藏 \| 浏览/下载：39/0 \| 提交时间：2022/12/20 Capillary-driven flow Eccentric annulus Volume of fluid method Microgravity
	Studies on two-bubble energy transfer model with radiant-receiver structure 期刊论文 OAI收割 ACTA MECHANICA SINICA, 11, 2022, 卷号: 38, 页码: 322099 作者: Bian ZD(卞真东); Wang JZ(王静竹); Yin B(银波); Wang YJ(王永久); Qiu RD(丘润荻) \| 收藏 \| 浏览/下载：18/0 \| 提交时间：2022/10/23 Bubble Energy transfer Radiant-receiver structure Volume of fluid method
	Capillary Phenomena Between Plates from Statics to Dynamics Under Microgravity 期刊论文 OAI收割 MICROGRAVITY SCIENCE AND TECHNOLOGY, 2022, 卷号: 34, 期号: 4, 页码: 11 作者: Chen, Shangtong; Duan, Li; Li, Yong; Ding, Fenglin; Liu, Jintao \| 收藏 \| 浏览/下载：50/0 \| 提交时间：2022/08/28 Capillary phenomena Microgravity Plates Volume of Fluid method Differential equation
	Study on propellant management device in plate surface tension tanks 期刊论文 OAI收割 ACTA MECHANICA SINICA, 2021, 页码: 11 作者: Chen ST(陈上通); Duan L(段俐); Kang Q(康琦) \| 收藏 \| 浏览/下载：95/0 \| 提交时间：2021/08/30 Surface tension tank Capillary driven flow Drop tower Volume of fluid method
	Numerical simulation of dynamic characteristics of a water surface vehicle with a blended-wing-body shape 期刊论文 OAI收割 JOURNAL OF HYDRODYNAMICS, 2018, 卷号: 30, 期号: 3, 页码: 433-440 作者: Wu XC(吴小翠); Wang YW(王一伟); Huang CG(黄晨光); Hu ZQ; Yi RW \| 收藏 \| 浏览/下载：30/0 \| 提交时间：2018/10/19 High Speed Blended Wing Body Vehicle Volume Of Fluid (vOf) Method Semi-relative Reference Frame Wave Making Resistance
	Numerical simulation of dynamic characteristics of a water surface vehicle with a blended-wing-body shape 期刊论文 OAI收割 Journal of Hydrodynamics, 2018, 卷号: 30, 期号: 3, 页码: 433-440 作者: Huang CG(黄晨光); Hu ZQ(胡志强); Wu XC(吴小翠); Yi RW(衣瑞文); Wang YW(王一伟) \| 收藏 \| 浏览/下载：32/0 \| 提交时间：2018/07/01 High speed blended wing body vehicle volume of fluid (VOF) method semi-relative reference frame wave making resistance
	Numerical simulation of dynamic characteristics of a water surface vehicle with a blended-wing-body shape 期刊论文 OAI收割 Journal of Hydrodynamics, 2018, 卷号: 30, 期号: 3, 页码: 433-440 作者: Wu XC(吴小翠); Wang YW(王一伟); Huang CG(黄晨光); Hu ZQ(胡志强) \| 收藏 \| 浏览/下载：17/0 \| 提交时间：2018/07/01 High Speed Blended Wing Body Vehicle Volume Of Fluid (vOf) Method Semi-relative Reference Frame Wave Making Resistance
	CFD-Based Load Calculation Method for Monopile Support Configuration of Offshore Wind Turbine 期刊论文 OAI收割南京航空航天大学学报：英文版, 2016, 卷号: 33.0, 期号: 1, 页码: 88-94 作者: Guo Tongqing; Tong Xiaolong; Lu Zhiliang \| 收藏 \| 浏览/下载：19/0 \| 提交时间：2021/02/02 monopile-supported offshore wind turbine Navier-Stokes(N-S) equations volume of fluid(VOF) method small amplitude wave unsteady load
	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.