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Comments on paratrooper‐separation modeling with the DSD/SST formulation and FOIST
Author(s) -
Tezduyar Tayfun E.
Publication year - 2011
Publication title -
international journal for numerical methods in fluids
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.938
H-Index - 112
eISSN - 1097-0363
pISSN - 0271-2091
DOI - 10.1002/fld.2299
Subject(s) - aerodynamics , separation (statistics) , computational fluid dynamics , domain (mathematical analysis) , space (punctuation) , aerospace engineering , computer science , mathematics , algorithm , engineering , mathematical analysis , machine learning , operating system
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). Copyright © 2010 John Wiley & Sons, Ltd.