Zobrazeno 1 - 10
of 12
pro vyhledávání: '"Christelle Seror"'
Autor:
Malcolm Smith, Leung Choi Chow, Christelle Seror, Werner Dobrzynski, Christopher Neil Wood, Britta Schöning
Publikováno v:
International Journal of Aeroacoustics. 5:233-262
In the approach phase of large commercial aircraft, airframe noise - and in particular that from landing gears - is one of the dominating aircraft noise components. Within a European co-financed research project entitled “Significantly Lower Commun
Publikováno v:
Physics of Fluids. 13:476-487
This paper addresses the problem of the estimation of the noise radiated by forced isotropic turbulence using an hybrid large-eddy simulation/Lighthill analogy approach. The scale separation associated with the LES approach leads to splitting the aco
Publikováno v:
Comptes Rendus de l'Académie des Sciences - Series IIB - Mechanics-Physics-Astronomy. 327:463-466
Resume Dans le cadre de la simulation des grandes echelles, une procedure dynamique d'adaptation de la constante du modele sous-maille fondee sur la relation de Germano est souvent employee. Lorsqu'un operateur lineaire de degre n applique au tenseur
Autor:
Christelle Seror, Pierre Sagaut, Christophe Bailly, Daniel Juvé, G. H. Ayers, L. S. Fletcher, C. V. Madhusudana
Publikováno v:
Journal of Thermophysics and Heat Transfer. 11:72-81
Autor:
L. Choi Chow, Malcolm Smith, Nicolas Molin, Werner Dobrzynski, Benjamin A. Fenech, Christelle Seror
Publikováno v:
12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference).
The main landing gears of large commercial aircraft are an important contributor to the total aircraft noise during landing approach. Within a European financed research project called SILENCER (“Significantly Lower Community Exposure to Aircraft N
Autor:
Leung Choi Chow, Malcolm Smith, Christelle Seror, Nicholas Molin, Jean-Francois Piet, Werner Dobrzynski
Publikováno v:
12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference).
Publikováno v:
10th AIAA/CEAS Aeroacoustics Conference.
This paper presents results of an unsteady simulation of a detailed nose landing gear. The discussion focuses on a steering system which is one of the most important nose landing gear source of noise. The results show that the complex geometry of the
Publikováno v:
The Journal of the Acoustical Society of America. 105:1066-1066
Most CAA applications rely on hybrid methods providing the radiated sound (using the Lighthill analogy, Kirchhoff integral or linearized Euler equations) from unsteady CFD. In that context, LES is widely considered as a compromise between full DNS an
Autor:
Werner M. Dobrzynski, Britta Schöning;, Leung Choi Chow, Chris Wood, Malcolm Smith, Christelle Seror
Publikováno v:
International Journal of Aeroacoustics; Sep2006, Vol. 5 Issue 3, p233-262, 30p
Publikováno v:
Scopus-Elsevier
5th AIAA/CEAS Aeroacoustics Conference and Exhibit
5th AIAA/CEAS Aeroacoustics Conference and Exhibit, 1999, Bellevue, France. ⟨10.2514/6.1999-1979⟩
5th AIAA/CEAS Aeroacoustics Conference and Exhibit
5th AIAA/CEAS Aeroacoustics Conference and Exhibit, 1999, Bellevue, France. ⟨10.2514/6.1999-1979⟩
An estimation of the noise generated by subgrid scales provided by a large-eddy simulation (LES) calculation is performed based on a priori tests. The derivation of Navier-Stokes equation to obtain Lighthill's equation (Lighthill, M.J.) is presented
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