Parallelization of a finite volume scheme applied to ice accretion

  • Abdelkader Baggag*
  • , Mondher Chekki
  • , Wagdi G. Habashi
  • , François Morency
  • *Corresponding author for this work

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

2 Citations (Scopus)

Abstract

Modeling of ever increasingly complex industrial processes requires insatiable computing power. To keep reasonable calculation times, one way is to decompose the domain into smaller ones and solve each subdomain on independent processors. The message passing interface (MPI) protocol and the ParMetis library are two helpful tools to achieve such a task. The paper presents an algorithm that uses both tools to parallelize ICE3D, a finite volume scheme for Ice accretion on aircraft, a module of the well-known code FENSAP-ICE. The parallelized code is used to calculate ice accretion on large-scale problems such as wings and complete aircraft.

Original languageEnglish
Title of host publicationCollection of Technical Papers - 36th AIAA Fluid Dynamics Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
Pages2061-2071
Number of pages11
ISBN (Print)1563478102, 9781563478109
DOIs
Publication statusPublished - 2006
Externally publishedYes
Event36th AIAA Fluid Dynamics Confernce - San Francisco, CA, United States
Duration: 5 Jun 20068 Jun 2006

Publication series

NameCollection of Technical Papers - 36th AIAA Fluid Dynamics Conference
Volume3

Conference

Conference36th AIAA Fluid Dynamics Confernce
Country/TerritoryUnited States
CitySan Francisco, CA
Period5/06/068/06/06

Fingerprint

Dive into the research topics of 'Parallelization of a finite volume scheme applied to ice accretion'. Together they form a unique fingerprint.

Cite this