Overset unstructured grids method for viscous flow computations

Fumiya Togashi, Yasushi Ito, Kazuhiro Nakahashi, Shigeru Obayashi

Research output: Chapter in Book/Report/Conference proceedingConference contribution

5 Citations (Scopus)

Abstract

Overset Unstructured Grids method is extended to the viscous flow computations of the multiple bodies in contact. In this paper, the overset treatment of hybrid meshes composed of tetrahedral, prismatic, pyramidal elements. is discussed in detail when those elements are embedded or contacted to the wall boundary of another grid. This method is applied to the ONERA M5 wing-body model and computed by the Navier-Stokes code. The computational results show good agreements with those obtained by single grid and experimental data. The boundary layer in the intersection region between two grids is well captured without the collar grid.

Original languageEnglish
Title of host publication21st AIAA Applied Aerodynamics Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
ISBN (Print)9781624100925
DOIs
Publication statusPublished - 2003 Jan 1
Event21st AIAA Applied Aerodynamics Conference 2003 - Orlando, FL, United States
Duration: 2003 Jun 232003 Jun 26

Publication series

Name21st AIAA Applied Aerodynamics Conference

Other

Other21st AIAA Applied Aerodynamics Conference 2003
CountryUnited States
CityOrlando, FL
Period03/6/2303/6/26

ASJC Scopus subject areas

  • Aerospace Engineering
  • Mechanical Engineering

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  • Cite this

    Togashi, F., Ito, Y., Nakahashi, K., & Obayashi, S. (2003). Overset unstructured grids method for viscous flow computations. In 21st AIAA Applied Aerodynamics Conference (21st AIAA Applied Aerodynamics Conference). American Institute of Aeronautics and Astronautics Inc.. https://doi.org/10.2514/6.2003-3405