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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2019, Vol. 40 ›› Issue (3): 122483-122483.doi: 10.7527/S1000-6893.2018.22483

• Fluid Mechanics and Flight Mechanics • Previous Articles     Next Articles

A parallel high-order method for simulating vortex-induced vibrations

QIU Zihua1, XU Min1, ZHANG Bin2, LIANG Chunlei2   

  1. 1. School of Astronautics, Northwestern Polytechnical University, Xi'an 710072, China;
    2. Department of Mechanical and Aerospace Engineering, The George Washington University, Washington, D.C. 20052, United States
  • Received:2018-06-26 Revised:2018-08-28 Online:2019-03-15 Published:2018-10-19
  • Supported by:
    National Natural Science Foundation of China (11602296, 11802179)

Abstract: This paper presents a parallel high-order method for simulating Vortex-Induced Vibrations (VIV) at very challenging situations, such as vibrations of very closely placed solid objects or a row of multiple objects with large relative displacements. This method works on unstructured triangular/quadrilateral hybrid grids by employing the high-order Spectral Difference (SD) method for spatial discretization. By introducing nonuniform sliding meshes, a computational domain is split into several non-overlapping subdomains, and each subdomain can enclose an object and move freely with respect to its neighbors. The two sides of a sliding interface are coupled through a newly developed nonuniform mortar method. A monolithic approach is adopted to seamlessly couple the fluid and the solid vibration equations. Parallelization strategy is studied and achieved by message passing interface implementation. Through a series of numerical tests, we demonstrate that the present method is high-order accurate for both inviscid and viscous flows; for steady uniform flow, the solver can assure free stream preservation; single cylinder VIV simulation agrees well with previous simulations, which verifies the reliability of the method; mesh deformation can be easily applied even when the deformation of the flow field is complicated, and high parallel efficiency can be achieved at the same time.

Key words: fluid-structure interaction, high-order scheme, spectral difference method, sliding-mesh, vortex-induced vibration, parallel computing

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