Zobrazeno 1 - 10
of 91
pro vyhledávání: '"Yves Gervais"'
Screech tones in supersonic jets are underpinned by resonance between downstream-travelling Kelvin–Helmholtz waves and upstream-travelling acoustic waves. Specifically, recent works suggest that the relevant acoustic waves are guided within the jet
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::0572efcb24535a408de56844adda5ebe
https://hdl.handle.net/11590/428950
https://hdl.handle.net/11590/428950
Publikováno v:
25th AIAA/CEAS Aeroacoustics Conference.
Publikováno v:
25th AIAA/CEAS Aeroacoustics Conference.
Publikováno v:
Journal of Fluid Mechanics. 788:358-380
We present a study of the turbulent and acoustic fields of subsonic jets, controlled by means of a novel actuator that introduces perturbations via steady-fluidic actuation from a rotating centrebody. The actuation can produce louder or quieter jets,
Publikováno v:
23rd AIAA/CEAS Aeroacoustics Conference.
Publikováno v:
23rd AIAA/CEAS Aeroacoustics Conference.
Publikováno v:
Journal of Sound and Vibration. 333:6516-6531
We present an investigation of the acoustic scattering due to the presence of a flat plate in the vicinity of a turbulent subsonic jet. Experiments have been performed to measure changes in the velocity and sound fields for Mach numbers ranging from
Autor:
Dimitri Papamoschou, Joel Delville, Yves Gervais, André V. G. Cavalieri, Peter Jordan, Maxime Kœnig
Publikováno v:
Journal of Sound and Vibration. 332:4067-4088
Jet noise is analysed using data-processing tools adapted to two particular structural traits of the far field: the strong polar dependence and the temporal intermittency. Proper Orthogonal Decomposition is used to probe the polar structure of the so
Autor:
Julien Marty, Cyril Polacsek, Lionel Castillon, Virginie Bonneau, Yves Gervais, Stéphane Moreau
Publikováno v:
22nd AIAA/CEAS Aeroacoustics Conference.
Turbofan broadband noise prediction is a major concern for industry and probably the most challenging issue for Aeroacoustic community. The dominant source mechanism is attributed to the rotor turbulent wakes impacting on the outlet guide vanes. Unst