A review on generation and mitigation of airfoil self-induced noise

A review on passive acoustic control of airfoil self-noise by means of porous trailing edge is presented. Porous surfaces are defined using various terms such as porosity, permeability, resistivity, porosity constant, dimensionless permeability, flow control severity and tortuosity. The primary purp...

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Main Authors: Ibren, Mohamed, Andan, Amelda Dianne, Asrar, Waqar, Sulaeman, Erwin
Format: Article
Language:English
English
Published: Penerbit Akademia Baru 2022
Subjects:
Online Access:http://irep.iium.edu.my/100345/7/100345_A%20review%20on%20generation%20and%20mitigation_SCOPUS.pdf
http://irep.iium.edu.my/100345/8/100345_A%20review%20on%20generation%20and%20mitigation.pdf
http://irep.iium.edu.my/100345/
https://semarakilmu.com.my/journals/index.php/fluid_mechanics_thermal_sciences/article/view/209/119
https://doi.org/10.37934/arfmts.90.1.163178
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Institution: Universiti Islam Antarabangsa Malaysia
Language: English
English
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spelling my.iium.irep.1003452022-09-30T01:07:25Z http://irep.iium.edu.my/100345/ A review on generation and mitigation of airfoil self-induced noise Ibren, Mohamed Andan, Amelda Dianne Asrar, Waqar Sulaeman, Erwin TJ Mechanical engineering and machinery A review on passive acoustic control of airfoil self-noise by means of porous trailing edge is presented. Porous surfaces are defined using various terms such as porosity, permeability, resistivity, porosity constant, dimensionless permeability, flow control severity and tortuosity. The primary purpose of this review paper is to provide key findings regarding the sources and mitigation techniques of self-induced noise generated by airfoils. In addition, various parametric design concepts were presented, which are critically important for porous-airfoil design specifications. Most research focus on experimentation with some recent efforts on numerical simulations. Detail study on flow topology is required to fully understand the unsteady flow nature. In general, noise on the airfoil surface is linked to the vortex shedding, instabilities on the surface, as well as feedback mechanism. In addition, acoustic scattering can be minimized by reducing extent of the porous region from the trailing edge while increasing resistivity. Moreover, blowing might also be another means of reducing noise near the trailing edge. Ultimately, understanding the flow physics well provides a way to unveil the unknowns in self-induced airfoil noise generation, mitigation, and control. Penerbit Akademia Baru 2022-01-01 Article PeerReviewed application/pdf en http://irep.iium.edu.my/100345/7/100345_A%20review%20on%20generation%20and%20mitigation_SCOPUS.pdf application/pdf en http://irep.iium.edu.my/100345/8/100345_A%20review%20on%20generation%20and%20mitigation.pdf Ibren, Mohamed and Andan, Amelda Dianne and Asrar, Waqar and Sulaeman, Erwin (2022) A review on generation and mitigation of airfoil self-induced noise. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 90 (1). pp. 163-178. ISSN 2289-7879 https://semarakilmu.com.my/journals/index.php/fluid_mechanics_thermal_sciences/article/view/209/119 https://doi.org/10.37934/arfmts.90.1.163178
institution Universiti Islam Antarabangsa Malaysia
building IIUM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider International Islamic University Malaysia
content_source IIUM Repository (IREP)
url_provider http://irep.iium.edu.my/
language English
English
topic TJ Mechanical engineering and machinery
spellingShingle TJ Mechanical engineering and machinery
Ibren, Mohamed
Andan, Amelda Dianne
Asrar, Waqar
Sulaeman, Erwin
A review on generation and mitigation of airfoil self-induced noise
description A review on passive acoustic control of airfoil self-noise by means of porous trailing edge is presented. Porous surfaces are defined using various terms such as porosity, permeability, resistivity, porosity constant, dimensionless permeability, flow control severity and tortuosity. The primary purpose of this review paper is to provide key findings regarding the sources and mitigation techniques of self-induced noise generated by airfoils. In addition, various parametric design concepts were presented, which are critically important for porous-airfoil design specifications. Most research focus on experimentation with some recent efforts on numerical simulations. Detail study on flow topology is required to fully understand the unsteady flow nature. In general, noise on the airfoil surface is linked to the vortex shedding, instabilities on the surface, as well as feedback mechanism. In addition, acoustic scattering can be minimized by reducing extent of the porous region from the trailing edge while increasing resistivity. Moreover, blowing might also be another means of reducing noise near the trailing edge. Ultimately, understanding the flow physics well provides a way to unveil the unknowns in self-induced airfoil noise generation, mitigation, and control.
format Article
author Ibren, Mohamed
Andan, Amelda Dianne
Asrar, Waqar
Sulaeman, Erwin
author_facet Ibren, Mohamed
Andan, Amelda Dianne
Asrar, Waqar
Sulaeman, Erwin
author_sort Ibren, Mohamed
title A review on generation and mitigation of airfoil self-induced noise
title_short A review on generation and mitigation of airfoil self-induced noise
title_full A review on generation and mitigation of airfoil self-induced noise
title_fullStr A review on generation and mitigation of airfoil self-induced noise
title_full_unstemmed A review on generation and mitigation of airfoil self-induced noise
title_sort review on generation and mitigation of airfoil self-induced noise
publisher Penerbit Akademia Baru
publishDate 2022
url http://irep.iium.edu.my/100345/7/100345_A%20review%20on%20generation%20and%20mitigation_SCOPUS.pdf
http://irep.iium.edu.my/100345/8/100345_A%20review%20on%20generation%20and%20mitigation.pdf
http://irep.iium.edu.my/100345/
https://semarakilmu.com.my/journals/index.php/fluid_mechanics_thermal_sciences/article/view/209/119
https://doi.org/10.37934/arfmts.90.1.163178
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