Zobrazeno 1 - 10
of 39
pro vyhledávání: '"Cyril Polacsek"'
Autor:
Sébastien Guérin, Carolin Kissner, Pascal Seeler, Ricardo Blázquez, Pedro Carrasco Laraña, Hélène de Laborderie, Danny Lewis, Paruchuri Chaitanya, Cyril Polacsek, Johan Thisse
Publikováno v:
Acoustics, Vol 2, Iss 3, Pp 617-649 (2020)
A benchmark dedicated to RANS-informed analytical methods for the prediction of turbofan rotor–stator interaction broadband noise was organised within the framework of the European project TurboNoiseBB. The second part of this benchmark focuses on
Externí odkaz:
https://doaj.org/article/6d30940db2e54966a61b7969cd8d5e55
Publikováno v:
AIAA Journal. 60:6763-6782
In the framework of improving aircraft nacelle design to comply international regulation on aircraft noise, a time-domain impedance boundary condition (TDIBC) based on the oscillo-diffusive representation is implemented in an industrial computational
Publikováno v:
Journal of Turbomachinery. 144
This article deals with the zonal detached eddy simulation of the fan module of a modern turbofan engine for the prediction of the broadband noise due to the interaction of the fan turbulent wakes with the stationary outlet guide vanes. The simulatio
Publikováno v:
Journal of Turbomachinery. 144
This paper (Part II) presents the broadband noise predictions of a turbofan stage based on a hybrid method proposed by ONERA in the framework of the European project TurboNoiseBB. The numerical approach relies on a ZDES (Zonal Detached Eddy Simulatio
Autor:
Carolin Kissner, Sebastien Guerin, Ricardo Blázquez, Johan Thisse, Danny Lewis, Pedro Carrasco Laraña, Cyril Polacsek, Hélène de Laborderie, Pascal Seeler, Paruchuri Chaitanya
Publikováno v:
Acoustics
Volume 2
Issue 3
Pages 33-649
Acoustics, Vol 2, Iss 33, Pp 617-649 (2020)
Acoustics, MDPI, 2020, 2 (3), pp.617-649. ⟨10.3390/acoustics2030033⟩
Volume 2
Issue 3
Pages 33-649
Acoustics, Vol 2, Iss 33, Pp 617-649 (2020)
Acoustics, MDPI, 2020, 2 (3), pp.617-649. ⟨10.3390/acoustics2030033⟩
A benchmark dedicated to RANS-informed analytical methods for the prediction of turbofan rotor&ndash
stator interaction broadband noise was organised within the framework of the European project TurboNoiseBB. The second part of this benchmark fo
stator interaction broadband noise was organised within the framework of the European project TurboNoiseBB. The second part of this benchmark fo
Publikováno v:
Aviation Noise Impact Management
Publikováno v:
AIAA Journal
AIAA Journal, American Institute of Aeronautics and Astronautics, 2021
AIAA Journal, American Institute of Aeronautics and Astronautics, 2021
International audience; The objective of the paper is to assess the capability of the isothermal Lattice Boltzmann Method (LBM) to correctly capture aerodynamic and acoustic features from a low-speed turbofan. The evaluation is done on the Advanced N
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::12a2fe1292d4d09bf87102778d7b93a5
https://hal.archives-ouvertes.fr/hal-03368520/document
https://hal.archives-ouvertes.fr/hal-03368520/document
Publikováno v:
AIAA AVIATION 2021 FORUM
AIAA AVIATION 2021 FORUM, Aug 2021, VIRTUAL EVENT, France. ⟨10.2514/6.2021-2257⟩
AIAA AVIATION 2021 FORUM, Aug 2021, VIRTUAL EVENT, France. ⟨10.2514/6.2021-2257⟩
International audience; The context of this study is the development of innovative stator concepts to reduce noise from rotor/stator interaction in future high bypass engines. Leading edge serrations are examined using a hybrid CFD/CAA method. A stoc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::be9588f96029fa24515ec5e682673911
https://hal.archives-ouvertes.fr/hal-03368344/document
https://hal.archives-ouvertes.fr/hal-03368344/document
Publikováno v:
AIAA Aviation 2021 Forum-Session: Duct Acoustics V
AIAA Aviation 2021 Forum
AIAA Aviation 2021 Forum, Aug 2021, Virtual event, United States. pp.AIAA 2021-2297, ⟨10.2514/6.2021-2297⟩
AIAA Aviation 2021 Forum
AIAA Aviation 2021 Forum, Aug 2021, Virtual event, United States. pp.AIAA 2021-2297, ⟨10.2514/6.2021-2297⟩
International audience; Noise pollution is a major concern for aircraft manufacturer during design and certification. Very high sound levels are recorded in take-off phases upstream of the engine fan, where multitonal noise components can appear (so-
Publikováno v:
ASME Turbo Expo 2020
ASME Turbo Expo 2020, Sep 2020, Virtual, Online, United Kingdom
Volume 2A: Turbomachinery
ASME Turbo Expo 2020, Sep 2020, Virtual, Online, United Kingdom
Volume 2A: Turbomachinery
The present article deals with the Zonal Detached Eddy Simulation of the fan module of a modern turbofan engine. The fan module, tested at the AneCom facility, is equipped with rotating fan blades and stationary outlet guide vanes (OGV). The simulati
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e020d001ebf8a5c24233cbd6705c5f7d
https://hal.archives-ouvertes.fr/hal-03048643/document
https://hal.archives-ouvertes.fr/hal-03048643/document