Overset unstructured grids method for viscous flow computations

Fumiya Togashi, Yasushi Ito, Kazuhiro Nakahashi, Shigeru Obayashi

研究成果: Conference contribution

8 被引用数 (Scopus)

抄録

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.

本文言語English
ホスト出版物のタイトル21st AIAA Applied Aerodynamics Conference
出版社American Institute of Aeronautics and Astronautics Inc.
ISBN(印刷版)9781624100925
DOI
出版ステータスPublished - 2003
イベント21st AIAA Applied Aerodynamics Conference 2003 - Orlando, FL, United States
継続期間: 2003 6月 232003 6月 26

出版物シリーズ

名前21st AIAA Applied Aerodynamics Conference

Other

Other21st AIAA Applied Aerodynamics Conference 2003
国/地域United States
CityOrlando, FL
Period03/6/2303/6/26

ASJC Scopus subject areas

  • 航空宇宙工学
  • 機械工学

フィンガープリント

「Overset unstructured grids method for viscous flow computations」の研究トピックを掘り下げます。これらがまとまってユニークなフィンガープリントを構成します。

引用スタイル