Comptes Rendus
Combustion, flow and spray dynamics for aerospace propulsion
Computing combustion noise by combining large eddy simulations with analytical models for the propagation of waves through turbine blades
[Méthode de calcul du bruit de combustion combinant des simulations aux grandes échelles avec des méthodes analytiques pour la propagation des ondes à travers les étages de turbine]
Comptes Rendus. Mécanique, Combustion, spray and flow dynamics for aerospace propulsion, Volume 341 (2013) no. 1-2, pp. 131-140.

Deux mécanismes sont responsables de la génération de bruit de combustion : le bruit direct, dans lequel les ondes acoustiques se propagent à travers les étages de la turbine et le bruit indirect, dans lequel les ondes de vorticité ou entropiques génèrent du bruit quand elles sont convectées. Une méthode pour calculer le bruit de combustion a été mise en place dans lʼoutil CHORUS. La méthode utilise des simulations aux grandes échelles (LES) pour la chambre de combustion, avec le code AVBP developpé au CERFACS (Schønfeld et Rudgyard, 1999 [2]), et des méthodes analytiques pour la propagation des ondes à travers les étages de la turbine. Le modèle est validé avec des simulations numériques.

Two mechanisms control combustion noise generation as shown by Marble and Candel (1977) [1]: direct noise, in which acoustic waves propagate through the turbine stages and indirect noise, in which vorticity and/or entropy waves generate noise as they are convected through turbine stages. A method to calculate combustion-generated noise has been implemented in a tool called CHORUS. The method uses the large eddy simulations of the combustion chamber obtained with the unstructured solver AVBP developed at CERFACS (Schønfeld and Rudgyard, 1999 [2]) and analytical models for the propagation through turbine stages. The propagation models (Cumpsty and Marble, 1977 [3]) use the compact row hypothesis to write matching conditions between the inlet and the outlet of a turbine stage. Using numerical simulations, the validity of the analytical methods is studied and the errors made quantified.

Publié le :
DOI : 10.1016/j.crme.2012.10.012
Keywords: Combustion, Thermoacoustics, Indirect combustion noise, Large eddy simulation
Mots-clés : Combustion, Thermoacoustique, Bruit de combustion indirect, Simulation aux grandes échelles

Ignacio Duran 1, 2 ; Matthieu Leyko 1 ; Stéphane Moreau 3 ; Franck Nicoud 4 ; Thierry Poinsot 5

1 Snecma, 77550 Moissy-Cramayel, France
2 CERFACS, 31057 Toulouse, France
3 Université de Sherbrooke, Sherbrooke, QC J1K2R1, Canada
4 Université Montpellier II, 34095 Montpellier, France
5 CNRS, institut de mécanique des fluides, 31400 Toulouse, France
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Ignacio Duran; Matthieu Leyko; Stéphane Moreau; Franck Nicoud; Thierry Poinsot. Computing combustion noise by combining large eddy simulations with analytical models for the propagation of waves through turbine blades. Comptes Rendus. Mécanique, Combustion, spray and flow dynamics for aerospace propulsion, Volume 341 (2013) no. 1-2, pp. 131-140. doi : 10.1016/j.crme.2012.10.012. https://comptes-rendus.academie-sciences.fr/mecanique/articles/10.1016/j.crme.2012.10.012/

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