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A numerical simulation of unsteady flow in small diameter helical grafts
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作者 Tinghui Zheng2,Yubo Fan1,Weizhong Wang2,Wentao Jiang2,Xiaoyan Deng1(1.School of Biological Science and Medical Engineering,Beihang University,Beijing,China 2.Department of Applied Mechanics,Sichuan University,Chengdu,Chin 《医用生物力学》 EI CAS CSCD 2009年第S1期40-41,共2页
The application of small diameter arterial grafts is limited due to the fact of relatively poor long-time patency which is caused by thrombosis formation in the short term and intimal hyperplasia(IH) in the medium and... The application of small diameter arterial grafts is limited due to the fact of relatively poor long-time patency which is caused by thrombosis formation in the short term and intimal hyperplasia(IH) in the medium and long term.Thrombosis,obstructing the flow of blood 展开更多
关键词 A numerical simulation of unsteady flow in small diameter helical grafts flow
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NUMERICAL SIMULATION OF UNSTEADY FLOW AROUND A CIRCULAR CYLINDER AT HIGH REYNOLDS NUMBERS
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作者 Yin Xieyuan Tong Bingang University of Science and Technology of ChinaHefei, Anhui, 230026, ChinaTao Feng Institute of Mechanics, Acadmia Sinica,Beijing, 100080, China 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 1991年第2期198-206,共9页
A Lagrangian-Eulerian hybrid scheme to solve unsteady N-S equation in two-dimensional incompressible fluid at high Reynolds numbers is presented in this paper. A random walk is imposed to simulate the viscous diffusio... A Lagrangian-Eulerian hybrid scheme to solve unsteady N-S equation in two-dimensional incompressible fluid at high Reynolds numbers is presented in this paper. A random walk is imposed to simulate the viscous diffusion, the vortex-in-cell method is used to obtain the convection velocity, and nascent vortices are created on a cylinder to satisfy the zero-slip condition. The impulsively started flow around a circular cylinder and the separation induced by a pair of incident vortices symmetrically approaching a circular cylinder have been successfully simulated by the hybrid scheme. The impulsively started flow from rest has been computed at Reynolds numbers 3000 and 9500. Comparisons are made with those results of finite-difference method, vortex method and flow visualization. Agreement is good. The particular attention has been paid to the evolutions of flow pattern. A topological analysis has been proposed in the region of the near wake. The bulge, isolated secondary vortex, a pair of secondary vortices, ' forewake phenomenon and other patterns are simulated numerically. The separation induced by a pair of incident vortices approaching a circular cylinder has been investigated by using the same scheme. The rebounding phenomenon of the incident vortex is observed and is attributed to the effect of the secondary vortex. In particular, we have found that a tertiary vortex can be formed near the surface; this phenomenon has been verified by flow visualization reported recently. 展开更多
关键词 numerical simulation OF unsteady flow AROUND A CIRCULAR CYLINDER AT HIGH REYNOLDS NUMBERS AT
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Unsteady Flow Variability Driven by Rotor-stator Interaction at Rotor Exit 被引量:5
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作者 ZHAO Ben YANG Ce +2 位作者 CHEN Shan QI Mingxu ZHOU Mi 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2012年第6期871-878,共8页
Numerical investigation of the unsteady flow variability driven by rotorstator interaction in a transonic axial compressor is performed. Two models with close and far axial gap between rotor and stator rows are studie... Numerical investigation of the unsteady flow variability driven by rotorstator interaction in a transonic axial compressor is performed. Two models with close and far axial gap between rotor and stator rows are studied in the simulation. Particular attention is attached to the analysis of mechanisms involved in driving rotor wake oscillation, rotor wake skewing and flow angle fluctuation at rotor exit. The results show that smaller axial gap is favorable to enhance the interaction in the region between two adjacent rows, and the fluctuation of the static pressure difference between two sides of rotor wake is improved by potential field from down stator, which is the driving force for rotor wake oscillation. The interaction between rotor and stator is weakened by increasing axial distance, rotor wake shifts to suction side of rotor blade with 5%-10% of rotor pitch, the absolute value of flow angle at rotor exit is less than that in the case of close interspace for every time step, and the fluctuation amplitude is also decreased. 展开更多
关键词 transonic compressor numerical simulation rotor-stator interaction unsteady flow wake oscillation
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