Comments on paratrooper-separation modeling with the DSD/SST formulation and FOIST

Research output: Contribution to journalArticle

Abstract

We provide a brief chronological background on the deforming-spatial-domain/stabilized space-time (DSD/SST) formulation, its use in aerodynamic modeling of a paratrooper separating from an aircraft, and the fluid-object interactions subcomputation technique (FOIST).

Original languageEnglish
Pages (from-to)1068-1072
Number of pages5
JournalInternational Journal for Numerical Methods in Fluids
Volume66
Issue number8
DOIs
Publication statusPublished - 2011 Jul 20
Externally publishedYes

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Keywords

  • Aerodynamic modeling
  • Cargo aircraft
  • DSD/SST formulation
  • FOIST
  • Mesh moving techniques
  • Paratrooper separation

ASJC Scopus subject areas

  • Computer Science Applications
  • Computational Mechanics
  • Mechanical Engineering
  • Mechanics of Materials
  • Applied Mathematics

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