TY - GEN
T1 - Modelling the Dissipation Range of von Kármán Turbulence Spectrum
AU - Dos Santos, Fernanda Leticia
AU - Botero-Bolívar, Laura
AU - Venner, Cornelis H.
AU - de Santana, Leandro Dantas
N1 - Funding Information:
The authors would like to acknowledge Ing. W. Lette, ir. E. Leusink, S. Wanrooij, and the technicians from the metal workshop of the University of Twente for the technical support. The authors also would like to acknowledge TNO and the Maritime Research Institute Netherlands (MARIN) for the insightful discussions. Part of this research received support from the European Union’s Horizon 2020 research and innovation programme under the Marie Sklodowska-Curie grant agreement No 860101.
Publisher Copyright:
© 2021, American Institute of Aeronautics and Astronautics Inc.. All rights reserved.
PY - 2021
Y1 - 2021
N2 - Noise pollution caused by inflow turbulence is a major problem in many applications, such as propellers and fans. Leading edge noise models, e.g., Amiet’s model, are widely applied to predict the noise produced by these applications. This noise prediction model relies on the accuracy of the turbulence spectrum, which is usually assumed to be the von Kármán energy spectrum for isotropic turbulence. However, the von Kármán spectrum does not model accurately the dissipation range of the turbulent energy, resulting in incorrect far-field noise predictions for the high-frequency range. An exponential correction can be applied to the spectrum to model the dissipation range. This correction depends on the dissipation frequency, which is the frequency where the energy spectrum changes from a dependence of−5/3 to an exponential decay. This study experimentally investigates nearly isotropic inflow turbulence and determines the flow field characteristics that affect the dissipation frequency in order to model this frequency and the dissipation range. Experiments have been conducted with two passive grids and hot-wire anemometry in the Aeroacoustic Wind Tunnel of the University of Twente. The turbulence uniformity in the test section and the turbulence development in the streamwise direction were analyzed, showing that the grid generated turbulence was mostly uniform and nearly isotropic. The dissipation frequency was observed to depend on the turbulence intensity, the free-stream velocity, and the turbulence length scale. An expression to compute this frequency is proposed, as well as a formula to predict the dissipation range. The predicted leading edge noise is affected by the dissipation range modelling in the high-frequency range, presenting a decrease in level up to 17 dB for the highest frequencies.
AB - Noise pollution caused by inflow turbulence is a major problem in many applications, such as propellers and fans. Leading edge noise models, e.g., Amiet’s model, are widely applied to predict the noise produced by these applications. This noise prediction model relies on the accuracy of the turbulence spectrum, which is usually assumed to be the von Kármán energy spectrum for isotropic turbulence. However, the von Kármán spectrum does not model accurately the dissipation range of the turbulent energy, resulting in incorrect far-field noise predictions for the high-frequency range. An exponential correction can be applied to the spectrum to model the dissipation range. This correction depends on the dissipation frequency, which is the frequency where the energy spectrum changes from a dependence of−5/3 to an exponential decay. This study experimentally investigates nearly isotropic inflow turbulence and determines the flow field characteristics that affect the dissipation frequency in order to model this frequency and the dissipation range. Experiments have been conducted with two passive grids and hot-wire anemometry in the Aeroacoustic Wind Tunnel of the University of Twente. The turbulence uniformity in the test section and the turbulence development in the streamwise direction were analyzed, showing that the grid generated turbulence was mostly uniform and nearly isotropic. The dissipation frequency was observed to depend on the turbulence intensity, the free-stream velocity, and the turbulence length scale. An expression to compute this frequency is proposed, as well as a formula to predict the dissipation range. The predicted leading edge noise is affected by the dissipation range modelling in the high-frequency range, presenting a decrease in level up to 17 dB for the highest frequencies.
KW - 2022 OA procedure
UR - https://www.scopus.com/pages/publications/85113429720
U2 - 10.2514/6.2021-2292
DO - 10.2514/6.2021-2292
M3 - Conference contribution
AN - SCOPUS:85113429720
SN - 9781624106101
BT - AIAA Aviation Forum 2021
PB - American Institute of Aeronautics and Astronautics
T2 - AIAA Aviation Forum 2021
Y2 - 2 August 2021 through 6 August 2021
ER -