Combustion noise in the laboratory scale PRECCINSTA (prediction and control of combustion instabilities in industrial gas turbines) burner is simulated with a new, robust, and highly efficient approach for combustion noise prediction. The applied hybrid method FRPM-CN (fast-random particle method for combustion noise prediction) relies on a stochastic, particle-based sound source reconstruction approach. Turbulence statistics from reacting CFD-RANS (computational fluid dynamics–Reynolds-Averaged Navier–Stokes) simulations are used as input for the stochastic method, where turbulence is synthesized based on a first-order Langevin ansatz. Sound propagation is modeled in the time domain with a modified set of linearized Euler equations and monopole sound sources are incorporated as right-hand side forcing of the pressure equation at every timestep of the acoustics simulations. First, the reacting steady-state CFD simulations are compared to experimental data, showing very good agreement. Subsequently, the computational combustion acoustics (CCA) setup is introduced, followed by comparisons of numerical with experimental pressure spectra. It is shown that FRPM-CN accurately captures absolute combustion noise levels without any artificial correction. Benchmark runs show that the computational costs of FRPM-CN are much lower than that of direct simulation approaches. The robustness and reliability of the method is demonstrated with parametric studies regarding source grid refinement, the choice of either RANS or URANS statistics, and the employment of different global reaction mechanisms.
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January 2017
Research-Article
Broadband Combustion Noise Simulation of the PRECCINSTA Burner Based on Stochastic Sound Sources
Felix Grimm,
Felix Grimm
Institute of Combustion Technology,
German Aerospace Center (DLR),
Pfaffenwaldring 38-40,
Stuttgart 70569, Germany
e-mail: felix.grimm@dlr.de
German Aerospace Center (DLR),
Pfaffenwaldring 38-40,
Stuttgart 70569, Germany
e-mail: felix.grimm@dlr.de
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Duncan Ohno,
Duncan Ohno
Institute of Combustion Technology,
German Aerospace Center (DLR),
Pfaffenwaldring 38-40,
Stuttgart 70569, Germany
German Aerospace Center (DLR),
Pfaffenwaldring 38-40,
Stuttgart 70569, Germany
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Berthold Noll,
Berthold Noll
Institute of Combustion Technology,
German Aerospace Center (DLR),
Pfaffenwaldring 38-40,
Stuttgart 70569, Germany
German Aerospace Center (DLR),
Pfaffenwaldring 38-40,
Stuttgart 70569, Germany
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Manfred Aigner,
Manfred Aigner
Institute of Combustion Technology,
German Aerospace Center (DLR),
Pfaffenwaldring 38-40,
Stuttgart 70569, Germany
German Aerospace Center (DLR),
Pfaffenwaldring 38-40,
Stuttgart 70569, Germany
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Roland Ewert,
Roland Ewert
Institute of Aerodynamics and Flow Technology,
German Aerospace Center (DLR),
Lilienthalplatz 7,
Braunschweig 38108, Germany
German Aerospace Center (DLR),
Lilienthalplatz 7,
Braunschweig 38108, Germany
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Jürgen Dierke
Jürgen Dierke
Institute of Aerodynamics and Flow Technology,
German Aerospace Center (DLR),
Lilienthalplatz 7,
Braunschweig 38108, Germany
German Aerospace Center (DLR),
Lilienthalplatz 7,
Braunschweig 38108, Germany
Search for other works by this author on:
Felix Grimm
Institute of Combustion Technology,
German Aerospace Center (DLR),
Pfaffenwaldring 38-40,
Stuttgart 70569, Germany
e-mail: felix.grimm@dlr.de
German Aerospace Center (DLR),
Pfaffenwaldring 38-40,
Stuttgart 70569, Germany
e-mail: felix.grimm@dlr.de
Duncan Ohno
Institute of Combustion Technology,
German Aerospace Center (DLR),
Pfaffenwaldring 38-40,
Stuttgart 70569, Germany
German Aerospace Center (DLR),
Pfaffenwaldring 38-40,
Stuttgart 70569, Germany
Berthold Noll
Institute of Combustion Technology,
German Aerospace Center (DLR),
Pfaffenwaldring 38-40,
Stuttgart 70569, Germany
German Aerospace Center (DLR),
Pfaffenwaldring 38-40,
Stuttgart 70569, Germany
Manfred Aigner
Institute of Combustion Technology,
German Aerospace Center (DLR),
Pfaffenwaldring 38-40,
Stuttgart 70569, Germany
German Aerospace Center (DLR),
Pfaffenwaldring 38-40,
Stuttgart 70569, Germany
Roland Ewert
Institute of Aerodynamics and Flow Technology,
German Aerospace Center (DLR),
Lilienthalplatz 7,
Braunschweig 38108, Germany
German Aerospace Center (DLR),
Lilienthalplatz 7,
Braunschweig 38108, Germany
Jürgen Dierke
Institute of Aerodynamics and Flow Technology,
German Aerospace Center (DLR),
Lilienthalplatz 7,
Braunschweig 38108, Germany
German Aerospace Center (DLR),
Lilienthalplatz 7,
Braunschweig 38108, Germany
Contributed by the Combustion and Fuels Committee of ASME for publication in the JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER. Manuscript received June 21, 2016; final manuscript received June 30, 2016; published online September 8, 2016. Editor: David Wisler.
J. Eng. Gas Turbines Power. Jan 2017, 139(1): 011505 (10 pages)
Published Online: September 8, 2016
Article history
Received:
June 21, 2016
Revised:
June 30, 2016
Citation
Grimm, F., Ohno, D., Noll, B., Aigner, M., Ewert, R., and Dierke, J. (September 8, 2016). "Broadband Combustion Noise Simulation of the PRECCINSTA Burner Based on Stochastic Sound Sources." ASME. J. Eng. Gas Turbines Power. January 2017; 139(1): 011505. https://doi.org/10.1115/1.4034236
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