20th AIAA/CEAS Aeroacoustics Conference 2014
DOI: 10.2514/6.2014-2315
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Performance improvements and new solution strategies of Actran/TM for nacelle simulations

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Cited by 9 publications
(2 citation statements)
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“…Since the number of liner dofs is generally large, the reduced-order model is constructed by introducing a pellicular basis constituted of a set of acoustic modes in a pellicular domain that is related to liner dofs. All this methodology has been implemented in a commercial software [19,21,22], which will be used for the numerical simulations presented in Section VIII B. Definition of the geometry of the acoustic problem For liner performance assessment, an aeroacoustic modeling of the acoustic radiation problem of a nacelle intake is used.…”
Section: Construction Of the Nominal Computational Modelmentioning
confidence: 99%
“…Since the number of liner dofs is generally large, the reduced-order model is constructed by introducing a pellicular basis constituted of a set of acoustic modes in a pellicular domain that is related to liner dofs. All this methodology has been implemented in a commercial software [19,21,22], which will be used for the numerical simulations presented in Section VIII B. Definition of the geometry of the acoustic problem For liner performance assessment, an aeroacoustic modeling of the acoustic radiation problem of a nacelle intake is used.…”
Section: Construction Of the Nominal Computational Modelmentioning
confidence: 99%
“…offs[69]. An Intel Skylake node with 32 cores 190 GB of RAM was used with 2 parallel tasks and 16 threads on each.…”
mentioning
confidence: 99%