A gas turbine model combustor is simulated with a hybrid, stochastic and particle-based method for combustion noise prediction with full 3D sound source modeling and sound propagation. Alongside, an incompressible LES simulation of the burner is considered for the investigation of the performance of the hybrid approach. The highly efficient time-domain method consists of a stochastic sound source reconstruction algorithm, the Fast Random Particle Method (FRPM) and sound wave propagation via Linearized Euler Equations (LEEs). In the context of this work, the method is adapted and tested for Combustion Noise (CN) prediction. Monopole sound sources are reconstructed by using an estimation of turbulence statistics from reacting CFD-RANS simulations. First, steady state and unsteady CFD calculations of flow field and combustion of the model combustor are evaluated and compared to experimental results. Two equation modeling for turbulence and the EDM (Eddy Dissipation Model) with FRC (Finite Rate Chemistry) for combustion are employed. In a second step, the acoustics simulation setup for the model combustor is introduced. Selected results are presented and FRPM-CN pressure spectra are compared to experimental levels.
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ASME Turbo Expo 2015: Turbine Technical Conference and Exposition
June 15–19, 2015
Montreal, Quebec, Canada
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-5668-0
PROCEEDINGS PAPER
Efficient Combustion Noise Simulation of a Gas Turbine Model Combustor Based on Stochastic Sound Sources Available to Purchase
Felix Grimm,
Felix Grimm
German Aerospace Center (DLR), Stuttgart, Germany
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Roland Ewert,
Roland Ewert
German Aerospace Center (DLR), Braunschweig, Germany
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Jürgen Dierke,
Jürgen Dierke
German Aerospace Center (DLR), Braunschweig, Germany
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Gilles Reichling,
Gilles Reichling
German Aerospace Center (DLR), Stuttgart, Germany
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Berthold Noll,
Berthold Noll
German Aerospace Center (DLR), Stuttgart, Germany
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Manfred Aigner
Manfred Aigner
German Aerospace Center (DLR), Stuttgart, Germany
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Felix Grimm
German Aerospace Center (DLR), Stuttgart, Germany
Roland Ewert
German Aerospace Center (DLR), Braunschweig, Germany
Jürgen Dierke
German Aerospace Center (DLR), Braunschweig, Germany
Gilles Reichling
German Aerospace Center (DLR), Stuttgart, Germany
Berthold Noll
German Aerospace Center (DLR), Stuttgart, Germany
Manfred Aigner
German Aerospace Center (DLR), Stuttgart, Germany
Paper No:
GT2015-42390, V04AT04A034; 14 pages
Published Online:
August 12, 2015
Citation
Grimm, F, Ewert, R, Dierke, J, Reichling, G, Noll, B, & Aigner, M. "Efficient Combustion Noise Simulation of a Gas Turbine Model Combustor Based on Stochastic Sound Sources." Proceedings of the ASME Turbo Expo 2015: Turbine Technical Conference and Exposition. Volume 4A: Combustion, Fuels and Emissions. Montreal, Quebec, Canada. June 15–19, 2015. V04AT04A034. ASME. https://doi.org/10.1115/GT2015-42390
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