2006
DOI: 10.1016/j.apm.2005.06.014
|View full text |Cite
|
Sign up to set email alerts
|

Parallel distributed numerical simulations in aeronautic applications

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1

Citation Types

0
4
0

Year Published

2006
2006
2020
2020

Publication Types

Select...
7

Relationship

0
7

Authors

Journals

citations
Cited by 8 publications
(4 citation statements)
references
References 20 publications
0
4
0
Order By: Relevance
“…While the BEM clearly cannot represent the flow physics fully, it can be applied to three-dimensional intakes at acceptable cost [27,28]. The interest in BEM for such calculations has increased recently with the development of efficient Fast Multipole Methods (FMM), such as that implemented in the EADS/AIRBUS BE code actipole [29,30].…”
Section: Boundary Element Methods (Bem)mentioning
confidence: 99%
“…While the BEM clearly cannot represent the flow physics fully, it can be applied to three-dimensional intakes at acceptable cost [27,28]. The interest in BEM for such calculations has increased recently with the development of efficient Fast Multipole Methods (FMM), such as that implemented in the EADS/AIRBUS BE code actipole [29,30].…”
Section: Boundary Element Methods (Bem)mentioning
confidence: 99%
“…While the BEM clearly does not represent the flow physics fully, because of the assumption of uniform flow, it is nonetheless a valuable approximate tool which can be applied to fully three-dimensional intakes at acceptable cost, and has been used for this purpose in recent years [50,51]. Interest in the use of BEM for such calculations has increased with improvements in performance through the use of Fast Multipole Methods (FMM), implemented for example in the EADS/AIRBUS BE code actipole [52,53].…”
Section: Boundary Element Methodsmentioning
confidence: 99%
“…The standard exterior BEM in a vibro-acoustic settting has been applied in aircraft noise [210,211]. The wave Equation 1 [47,48,[302][303][304] and, similarly, to underwater vehicles [305,306].…”
Section: Aero-acousticsmentioning
confidence: 99%
“…The computational resources include the computer processing time and/or the memory requirements. One approach for improving the execution time of numerical methods is to use parallel processing, so that instructions are executed simultaneously, rather than sequentially, and such techniques have been applied in the boundary element method [304,344].…”
Section: Efficiencymentioning
confidence: 99%