21st AIAA/CEAS Aeroacoustics Conference 2015
DOI: 10.2514/6.2015-2382
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Numerical Investigation of Indirect Noise Generation by Accelerated Vorticity

Abstract: Combustion noise of aero engines originates from unsteady combustion processes which in turn lead to vortical and temperature fluctuations. These so-called vorticity and entropy waves are convected from the combustor into the turbine where their acceleration results in an additional sound release, namely the indirect noise. In the present study the noise generation by accelerated vorticity waves is investigated in a convergent-divergent nozzle representing the simplest model of the flow through the turbine. A … Show more

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Cited by 8 publications
(6 citation statements)
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References 23 publications
(18 reference statements)
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“…Furthermore, the effects of turbulent mixing or flow separation on indirect combustion noise as described by Howe 19 can also be studied further within this specific numerical context. All of these effects have not been studied in previous EWG works, which are based on the coupling of RANS simulations with computational aeroacoustic (CAA) methodologies, 20,21 unsteady RANS simulations, 12,13 Euler simulations, and even analytical modeling. 9,11,22 To reach the need for higher-fidelity flow predictions, Large Eddy Simulation (LES) seems to be a first good candidate to simulate the high Reynolds number EWG subsonic test case, and provide further insight into the physical phenomena of indirect combustion noise generation and transmission.…”
Section: Introductionmentioning
confidence: 99%
“…Furthermore, the effects of turbulent mixing or flow separation on indirect combustion noise as described by Howe 19 can also be studied further within this specific numerical context. All of these effects have not been studied in previous EWG works, which are based on the coupling of RANS simulations with computational aeroacoustic (CAA) methodologies, 20,21 unsteady RANS simulations, 12,13 Euler simulations, and even analytical modeling. 9,11,22 To reach the need for higher-fidelity flow predictions, Large Eddy Simulation (LES) seems to be a first good candidate to simulate the high Reynolds number EWG subsonic test case, and provide further insight into the physical phenomena of indirect combustion noise generation and transmission.…”
Section: Introductionmentioning
confidence: 99%
“…numerical simulations [17][18][19][20], and experiments [21][22][23][24] aiming to evaluate and release the restrictive assumptions made by Marble and Candle [12]. While these studies advanced the theory considerably, most of them neglected the evolution of entropy waves during their convection by the mean flow.…”
Section: Nomenclaturementioning
confidence: 99%
“…Vortex-driven indirect-combustion noise is known to play a major role in the establishment of self-sustained pressure pulsations in large Solid Rocket Motors [1][2][3][4], and is believed to be an indirect-combustion noise source in aircraft engines [5,6]. Vortex-driven indirect-combustion noise will partly be radiated outward, thus contributing to environmental noise.…”
Section: Introductionmentioning
confidence: 99%
“…To the best of the authors' knowledge, in the literature there is only one attempt at model-based analysis of the above mentioned experiments, that by Ullrich et al [6] who reported simulations which used a hybrid CFD/CAA model. Echoing Kings' and Bake's hypothesis, Ullrich's et al [6] modeling approach fundamentally supposed that sound production in the experiments was due to acceleration of vorticity waves through the nozzle.…”
Section: Introductionmentioning
confidence: 99%