Zobrazeno 1 - 10
of 14
pro vyhledávání: '"Fernando Gea-Aguilera"'
Publikováno v:
International Journal of Turbomachinery, Propulsion and Power, Vol 6, Iss 2, p 12 (2021)
In the present paper, large eddy simulations are performed to study two different mechanisms of Fan/OGV broadband noise: airfoil self-noise and turbulence interaction noise. Firstly, the current study focuses on the prediction of airfoil self-noise f
Externí odkaz:
https://doaj.org/article/913a00c9d69a4094bc5a523f7f6be271
Publikováno v:
28th AIAA/CEAS Aeroacoustics 2022 Conference.
Publikováno v:
Physics of Fluids. 35:047104
A detailed aeroacoustic analysis of the flow induced by the clearance between the fan tip and the shroud is performed in a scale-model fan stage of an ultrahigh bypass ratio turbofan engine, which was designed to operate at transonic regimes. A wall-
Publikováno v:
Journal of Sound and Vibration. 537:117180
A scale model of a fan stage operating at approach condition is investigated using wall-resolved Large Eddy Simulations. The configuration is a state-of-the-art fan stage (rotor + stator) of an Ultra High Bypass Ratio turbofan engine, and the computa
Publikováno v:
Computers & Fluids. 157:240-252
A leading edge noise prediction methodology that uses an advanced digital filter method to generate synthetic turbulence is presented for efficient two- and three-dimensional simulations. The digital filter method combines the advantages of the Rando
Publikováno v:
25th AIAA/CEAS Aeroacoustics Conference
25th AIAA/CEAS Aeroacoustics Conference, 2019, Delft, France. ⟨10.2514/6.2019-2604⟩
25th AIAA/CEAS Aeroacoustics Conference, 2019, Delft, France. ⟨10.2514/6.2019-2604⟩
International audience
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7a182d339f49d34180df01ff353ff209
https://hal.archives-ouvertes.fr/hal-02382960
https://hal.archives-ouvertes.fr/hal-02382960
Publikováno v:
Journal of Sound and Vibration. 495:115895
This paper presents an investigation on the broadband noise produced by the interaction of anisotropic turbulence with isolated aerofoils. Computational aeroacoustic simulations are performed using a synthetic turbulence method with a linearised Eule
Publikováno v:
23rd AIAA/CEAS Aeroacoustics Conference.
Leading edge noise reductions caused by serrations have been shown to be sensitive to the length scales of vortical disturbances. In order to improve the understanding of wavy leading edge airfoils as a noise reduction technology, this paper examines
Publikováno v:
23rd AIAA/CEAS Aeroacoustics Conference.
An analytical solution to leading-edge noise produced by a translating two-dimensional flat plate ingesting turbulence in proximity to a hard-wall is presented. This is a relevant problem to calculate the installation noise of open rotors and un-duct
Publikováno v:
Journal of Sound and Vibration. 459:114859
This paper investigates simplified and representative configurations of fan wake-cascade interaction noise, which is a major source of broadband noise in ultra-high bypass ratio turbofan engines. To this end, two-dimensional computational aeroacousti