Zobrazeno 1 - 10
of 21
pro vyhledávání: '"Hervé Denayer"'
A numerical approach based on high-order stabilized finite elements is proposed to solve thermo-acoustic and visco-acoustic problems accounting for non-uniform mean flow effects. The approach is based on the Linearized Navier-Stokes equations written
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1d606f62042ee9872253d7f6081b430f
https://lirias.kuleuven.be/handle/20.500.12942/701043
https://lirias.kuleuven.be/handle/20.500.12942/701043
Autor:
Luigi Criscuolo, Florent Renac, Vincent Couaillier, Fabio Naddei, Hervé Denayer, Wim De Roeck, Wim Desmet
ispartof: Aiaa Journal vol:60 issue:6 pages:3593-3602 ispartof: location:ELECTR NETWORK status: published
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::72d3396ebd74f6fd910970cd8f2fed21
https://lirias.kuleuven.be/handle/20.500.12942/686387
https://lirias.kuleuven.be/handle/20.500.12942/686387
ispartof: Proceedings of the 28th AIAA/CEAS Aeroacoustics Conference ispartof: 28th AIAA/CEAS Aeroacoustics Conference location:Southampton, UK date:14 Jun - 17 Jun 2022 status: Published online
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7a4feed8210fafb08047c9ad82f9f4e9
https://lirias.kuleuven.be/handle/20.500.12942/695587
https://lirias.kuleuven.be/handle/20.500.12942/695587
Publikováno v:
Journal of Sound and Vibration, 537
A Helmholtz resonator with a curved cavity is studied for reducing jet-installation noise in a configuration comprised by a subsonic jet and a nearby flat plate. The face-sheet and cavity are designed with the Guess method and the impedance is verifi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::9a780dcfe7ffbfe0af7c2a0a20603643
https://hdl.handle.net/11583/2976709
https://hdl.handle.net/11583/2976709
Publikováno v:
AIAA AVIATION 2021 FORUM.
ispartof: pages:2268-2268 ispartof: AIAA Aviation 2021 forum pages:2268-2268 ispartof: 27th AIAA/CEAS Aeroacoustics Conference (AIAA Aviation 2021 forum) location:Virtual conference date:2 Aug - 6 Aug 2021 status: published
ispartof: AIAA 2021 proceedings ispartof: AIAA 2021 AVIATION FORUM location:Virtual status: Published online
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b3941f03b92446644a61841b06a6e222
https://lirias.kuleuven.be/handle/123456789/678724
https://lirias.kuleuven.be/handle/123456789/678724
Publikováno v:
AIAA AVIATION 2021 FORUM.
ispartof: pages:1-14 ispartof: AIAA AVIATION 2021 Forum pages:1-14 ispartof: AIAA AVIATION 2021 Forum location:Virtual event date:2 Aug - 6 Aug 2021 status: published
Publikováno v:
AIAA AVIATION 2020 FORUM
AIAA AVIATION 2020 FORUM, Jun 2020, VIRTUAL EVENT, United States. ⟨10.2514/6.2020-2570⟩
AIAA AVIATION 2020 FORUM, Jun 2020, VIRTUAL EVENT, United States. ⟨10.2514/6.2020-2570⟩
International audience; This paper presents an analysis of the aeroacoustic instabilities in a slit-type Helmholtz resonator subjected to a low Mach number grazing flow. This configuration can be susceptible to non-linear feedback phenomena due to th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b12415692597b8237bb73325a08294b2
https://hal.archives-ouvertes.fr/hal-03199233/file/DAAA21035.1618489627_preprint.pdf
https://hal.archives-ouvertes.fr/hal-03199233/file/DAAA21035.1618489627_preprint.pdf
Publikováno v:
25th AIAA/CEAS Aeroacoustics Conference.
Publikováno v:
25th AIAA/CEAS Aeroacoustics Conference.