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title:(Improved AND Trailing AND Edge AND Noise AND Model)

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1 Book chapter

Improved Trailing Edge Noise Model

Bertagnolio, Franck

Eudp Project: Low Noise Airfoil - Final Report — 2012, pp. 30-35

The modeling of the surface pressure spectrum under a turbulent boundary layer is investigated in the presence of an adverse pressure gradient along the flow direction. It is shown that discrepancies between measurements and results from a well-known model increase as the pressure gradient

Year: 2012

Language: English

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2 Conference paper

Improvement of TNO type trailing edge noise models

Fischer, Andreas; Bertagnolio, Franck; Aagaard Madsen, Helge

Proceedings of 16th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery — 2016

The paper describes an improvement of the so-called TNO model to predict the noise emission from aerofoil sections due to the interaction of the boundary layer turbulence with the trailing edge. The surface pressure field close to the trailing edge acts as source of sound in the TNO model

Year: 2016

Language: English

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3 Journal article

Improvement of TNO type trailing edge noise models

The paper describes an improvement of the so-called TNO model to predict the noise emission from aerofoil sections due to the interaction of the boundary layer turbulence with the trailing edge. The surface pressure field close to the trailing edge acts as source of sound in the TNO model

Year: 2017

Language: English

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4 Journal article

Validations and improvements of airfoil trailing-edge noise prediction models using detailed experimental data : Validations and improvements of aeroacoustic models

This paper describes an extensive assessment and a step by step validation of different turbulent boundary-layer trailing-edge noise prediction schemes developed within the European Union funded wind energy project UpWind. To validate prediction models, measurements of turbulent boundary-layer

Year: 2012

Language: English

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5 Journal article

Tuning of turbulent boundary layer anisotropy for improved surface pressure and trailing-edge noise modeling

The modeling of the surface pressure spectrum beneath a turbulent boundary layer is investigated, focusing on the case of airfoil flows and associated trailing edge noise prediction using the so-called TNO model. This type of flow is characterized by the presence of an adverse pressure gradient

Year: 2014

Language: English

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