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Numerical Simulation of an Aortic Flow Based on a HLLC Type Incompressible Flow Solver 被引量:3

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摘要 In this study,a three-dimensional artificial compressibility solver based on the average-state Harten-Lax-van Leer-Contact(HLLC)[13]type Riemann solution is first proposed and developed to solve the time-dependent incompressible flow equations.To implement unsteady flow calculations,a dual time stepping strategy including the LU decomposition method is used in the pseudo-time iteration and the second-order accurate backward difference is adopted to discretize the unsteady flow term.Also a third-order accurate HLLC numerical flux is derived for approximating the inviscid terms.To verify numerical accuracy,flows over a lid-driven cavity and an oscillating flat plate are chosen as the benchmark tests.In addition,the current solver is extended to solve blood flows in a realistic human aorta measured from MRI(Magnetic Resonance Imaging).The simulation geometry was derived from a three-dimensional reconstruction of a series of two-dimensional slices obtained in vivo.Numerical results demonstrate wall stresses were highly dynamic,but were generally high along the outer wall in the vicinity of the branches and low along the inner wall,particularly in the descending aorta.The maximum wall stress distribution is presented on the aortic arch in the systole.In addition,extensive counter-clockwise secondary flows and three-dimensional helical vortex influenced considerably by the presence of vessel contraction,torsion and the branches were shown in the descending aorta in the late systole and early diastolic cycles.
出处 《Communications in Computational Physics》 SCIE 2009年第1期142-162,共21页 计算物理通讯(英文)
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  • 2杜建一,汤华,赵晓路,徐建中.叶顶间隙对离心压气机性能影响的研究[J].工程热物理学报,2006,27(4):583-585. 被引量:24
  • 3吴虎,廉小纯,崔建勇.跨音多级轴流压气机对突变型扰动的动态响应[J].推进技术,1997,18(3):56-58. 被引量:4
  • 4MEI Y,GUHA A.Implicit numerical simulation of transonic flow through turbine cascades on unstructured grids[J].Proceedings of the Institution of Mechanical Engineers,Part A,Journal of Power and Energy,2005,219(1):35-47.
  • 5魏玲.跨声速压气机转子三维流场Navier-Stokes方程数值模拟[D].南京:南京航空航天大学,2005.
  • 6XU Da,DENG Qinghua,FENG Zhenping.Numerical investigation on rotor tip leakage control by casing air injection for a radial inflow turbine[R].ASME,2011-46123,2011.
  • 7TORO E E Riemann solvers and numerical methods for fluid dynamics,a practical introduction[M].3rd ed.London:Springer,2009.
  • 8JUNG S K,MYONG R S,CHO T H.Development of Eulerian droplets impingement model using HLLC Riemann solver and POD-based reduced order method[R].AIAA,2011-3907,2011.
  • 9BERTHON C,CHARRIER P,DUBROCA B.An HLLC scheme to solve the M1 model of radiative transfer in two space dimensions[J].Journal of Scientific Computing,2007,31(3):347-389.
  • 10GURSKI K F.An HLLC-type approximate Riemann solver for ideal magneto hydrodynamics[J].SIAM Journal of Science Computing,2004,25(6):2165-2187.

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