Prediction of broadband trailing-edge noise based on Blake model and Amiet theory
Prediction of broadband trailing-edge noise based on Blake model and Amiet theory
This paper extends previously published TNO-Blake methods to predict airfoil broadband self-noise due to interaction of a turbulent boundary-layer with a sharp trailing edge. The method presented herein combines Blake’s model to predict surface pressure fluctuations and Amiet model to predict trailing edge noise emission. The Blake method is based on the solution of the Poisson equation as an integral of the mean-shear turbulent source interaction source, over the entire boundary layer thickness. A recent advances in description of streamwise turbulent intensity are employed. Surface pressure spectra are measured with remote microphones and compared to the prediction. In the next step, the wavenumber- frequency spectrum as predicted by the TNO model was utilized as an input to the Amiet model to evaluate the far-field trailing edge noise.
American Institute of Aeronautics and Astronautics
Stalnov, O.
6ca7508b-4d32-4e46-9158-ef8f03795ece
Chaitanya, P.
2438fc85-839e-41f1-92d2-c081938513e6
Joseph, P. F.
9c30491e-8464-4c9a-8723-2abc62bdf75d
18 June 2016
Stalnov, O.
6ca7508b-4d32-4e46-9158-ef8f03795ece
Chaitanya, P.
2438fc85-839e-41f1-92d2-c081938513e6
Joseph, P. F.
9c30491e-8464-4c9a-8723-2abc62bdf75d
Stalnov, O., Chaitanya, P. and Joseph, P. F.
(2016)
Prediction of broadband trailing-edge noise based on Blake model and Amiet theory.
In 21st AIAA/CEAS Aeroacoustics Conference.
American Institute of Aeronautics and Astronautics..
(doi:10.2514/6.2015-2526).
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Conference or Workshop Item
(Paper)
Abstract
This paper extends previously published TNO-Blake methods to predict airfoil broadband self-noise due to interaction of a turbulent boundary-layer with a sharp trailing edge. The method presented herein combines Blake’s model to predict surface pressure fluctuations and Amiet model to predict trailing edge noise emission. The Blake method is based on the solution of the Poisson equation as an integral of the mean-shear turbulent source interaction source, over the entire boundary layer thickness. A recent advances in description of streamwise turbulent intensity are employed. Surface pressure spectra are measured with remote microphones and compared to the prediction. In the next step, the wavenumber- frequency spectrum as predicted by the TNO model was utilized as an input to the Amiet model to evaluate the far-field trailing edge noise.
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Published date: 18 June 2016
Venue - Dates:
21st AIAA/CEAS Aeroacoustics Conference, 2015, , Dallas, United States, 2015-06-22 - 2015-06-26
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Local EPrints ID: 443701
URI: http://eprints.soton.ac.uk/id/eprint/443701
PURE UUID: fbaf43b6-7ec8-4823-8f47-2f8d54226e91
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Date deposited: 09 Sep 2020 16:31
Last modified: 16 Mar 2024 09:14
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Author:
O. Stalnov
Author:
P. Chaitanya
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