A survey of overset domain assembly methods

  • Cameron T. Druyor
  • , William T. Jones
  • , Steve L. Karman

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

3 Scopus citations

Abstract

Overset or Chimera grid methods are widely used in industry and academia to solve problems with bodies in relative motion or complex geometry that would otherwise be challenging or even impossible due to the impediments imposed by a single grid representation. These methods utilize a composite mesh to span the computational domain. The composite mesh consists of an arbitrary number of overlapping component meshes. Because the component meshes overlap, inter-grid boundaries must be defined and interpolation stencils must be provided to the flow solver by an overset domain assembly code. The process of defining inter-grid boundaries is often referred to as "hole cutting" because pieces of the component meshes are removed from the computational domain. Hole cutting is computationally expensive and has proven difficult to efficiently parallelize. In order to address this difficulty, the sources of computational cost and those that impede scalability must be identified. This work presents the major sources of computational cost and summarizes current techniques used in their mitigation.

Original languageEnglish
Title of host publication53rd AIAA Aerospace Sciences Meeting
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624103438
DOIs
StatePublished - 2015
Externally publishedYes
Event53rd AIAA Aerospace Sciences Meeting, 2015 - Kissimmee, United States
Duration: Jan 5 2015Jan 9 2015

Publication series

Name53rd AIAA Aerospace Sciences Meeting

Conference

Conference53rd AIAA Aerospace Sciences Meeting, 2015
Country/TerritoryUnited States
CityKissimmee
Period01/5/1501/9/15

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