Analysis of Sound Propagation Behaviors for Supersonic Jet on Far Field Region by Computational Aero-Acoustics (CAA) Simulation

Noise emission is an essential issue for the aviation industry, as it harms health and induces various physiological responses. The noise generated by supersonic jets is very intense. It will cause fatigue and even damage the human hearing system in the surrounding area of jet operation. Besides, t...

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Main Authors: Maulana, Yudi, Manshoor, Bukhari, Khalid, Amir, Zaman, Izzuddin, Didane, Djamal Hissein, Abdul Haq, Reazul Haq, Kamarudin, Kamarul-Azhar, Nurmutia, Syahreen, Saleman, Abdul Rafeq, Rathje, Rio Marco, Rothe, Christin, Ibrahim, Mohd Nizam
Format: Article
Language:English
Published: semarak ilmu 2024
Online Access:http://eprints.uthm.edu.my/12416/1/J17885_1ca2063a0410f38eaddade0a06431092.pdf
http://eprints.uthm.edu.my/12416/
https://doi.org/10.37934/arfmts.117.1.7182
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Institution: Universiti Tun Hussein Onn Malaysia
Language: English
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spelling my.uthm.eprints.124162025-02-19T04:34:46Z http://eprints.uthm.edu.my/12416/ Analysis of Sound Propagation Behaviors for Supersonic Jet on Far Field Region by Computational Aero-Acoustics (CAA) Simulation Maulana, Yudi Manshoor, Bukhari Khalid, Amir Zaman, Izzuddin Didane, Djamal Hissein Abdul Haq, Reazul Haq Kamarudin, Kamarul-Azhar Nurmutia, Syahreen Saleman, Abdul Rafeq Rathje, Rio Marco Rothe, Christin Ibrahim, Mohd Nizam Noise emission is an essential issue for the aviation industry, as it harms health and induces various physiological responses. The noise generated by supersonic jets is very intense. It will cause fatigue and even damage the human hearing system in the surrounding area of jet operation. Besides, the experimental and prototyping cost for the jet model is prohibitive, and it is a vast project and process that takes a lot of time to run. The purpose of this study is to determine the sound propagation behaviours of a supersonic jet in the far-field region and to analyse the consequences of the velocity of a supersonic jet on sound propagation of supersonic jet by using computational fluid dynamics (CFD) and computational aeroacoustics (CAA) simulations. This study focused on the perspective of observing the distance of the receiver when receiving the sound propagation of a supersonic jet, the observed angle of the receiver when receiving the sound propagation of a supersonic jet, and the velocity of the supersonic jet. The CFD and CAA analyses were performed in transient state simulation and the 2-inch Acoustics Reference Nozzle (ARN2). The result shows that the overall SPL throughout the frequency is proportional to the jet velocity of the supersonic jet. However, the distance and angle of the receiver gave different results in sound propagation behaviour. The results also conclude that as the distance between the receiver and jet nozzle exit increases, the overall SPL trend will decrease throughout the frequency increase. As the vertical distance between the receiver and the axisymmetric line of the jet nozzle increases, the frequency of the receiver starts to observe will decrease. semarak ilmu 2024 Article PeerReviewed text en http://eprints.uthm.edu.my/12416/1/J17885_1ca2063a0410f38eaddade0a06431092.pdf Maulana, Yudi and Manshoor, Bukhari and Khalid, Amir and Zaman, Izzuddin and Didane, Djamal Hissein and Abdul Haq, Reazul Haq and Kamarudin, Kamarul-Azhar and Nurmutia, Syahreen and Saleman, Abdul Rafeq and Rathje, Rio Marco and Rothe, Christin and Ibrahim, Mohd Nizam (2024) Analysis of Sound Propagation Behaviors for Supersonic Jet on Far Field Region by Computational Aero-Acoustics (CAA) Simulation. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 117 (1). pp. 71-82. ISSN 2289-7879 https://doi.org/10.37934/arfmts.117.1.7182
institution Universiti Tun Hussein Onn Malaysia
building UTHM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Tun Hussein Onn Malaysia
content_source UTHM Institutional Repository
url_provider http://eprints.uthm.edu.my/
language English
description Noise emission is an essential issue for the aviation industry, as it harms health and induces various physiological responses. The noise generated by supersonic jets is very intense. It will cause fatigue and even damage the human hearing system in the surrounding area of jet operation. Besides, the experimental and prototyping cost for the jet model is prohibitive, and it is a vast project and process that takes a lot of time to run. The purpose of this study is to determine the sound propagation behaviours of a supersonic jet in the far-field region and to analyse the consequences of the velocity of a supersonic jet on sound propagation of supersonic jet by using computational fluid dynamics (CFD) and computational aeroacoustics (CAA) simulations. This study focused on the perspective of observing the distance of the receiver when receiving the sound propagation of a supersonic jet, the observed angle of the receiver when receiving the sound propagation of a supersonic jet, and the velocity of the supersonic jet. The CFD and CAA analyses were performed in transient state simulation and the 2-inch Acoustics Reference Nozzle (ARN2). The result shows that the overall SPL throughout the frequency is proportional to the jet velocity of the supersonic jet. However, the distance and angle of the receiver gave different results in sound propagation behaviour. The results also conclude that as the distance between the receiver and jet nozzle exit increases, the overall SPL trend will decrease throughout the frequency increase. As the vertical distance between the receiver and the axisymmetric line of the jet nozzle increases, the frequency of the receiver starts to observe will decrease.
format Article
author Maulana, Yudi
Manshoor, Bukhari
Khalid, Amir
Zaman, Izzuddin
Didane, Djamal Hissein
Abdul Haq, Reazul Haq
Kamarudin, Kamarul-Azhar
Nurmutia, Syahreen
Saleman, Abdul Rafeq
Rathje, Rio Marco
Rothe, Christin
Ibrahim, Mohd Nizam
spellingShingle Maulana, Yudi
Manshoor, Bukhari
Khalid, Amir
Zaman, Izzuddin
Didane, Djamal Hissein
Abdul Haq, Reazul Haq
Kamarudin, Kamarul-Azhar
Nurmutia, Syahreen
Saleman, Abdul Rafeq
Rathje, Rio Marco
Rothe, Christin
Ibrahim, Mohd Nizam
Analysis of Sound Propagation Behaviors for Supersonic Jet on Far Field Region by Computational Aero-Acoustics (CAA) Simulation
author_facet Maulana, Yudi
Manshoor, Bukhari
Khalid, Amir
Zaman, Izzuddin
Didane, Djamal Hissein
Abdul Haq, Reazul Haq
Kamarudin, Kamarul-Azhar
Nurmutia, Syahreen
Saleman, Abdul Rafeq
Rathje, Rio Marco
Rothe, Christin
Ibrahim, Mohd Nizam
author_sort Maulana, Yudi
title Analysis of Sound Propagation Behaviors for Supersonic Jet on Far Field Region by Computational Aero-Acoustics (CAA) Simulation
title_short Analysis of Sound Propagation Behaviors for Supersonic Jet on Far Field Region by Computational Aero-Acoustics (CAA) Simulation
title_full Analysis of Sound Propagation Behaviors for Supersonic Jet on Far Field Region by Computational Aero-Acoustics (CAA) Simulation
title_fullStr Analysis of Sound Propagation Behaviors for Supersonic Jet on Far Field Region by Computational Aero-Acoustics (CAA) Simulation
title_full_unstemmed Analysis of Sound Propagation Behaviors for Supersonic Jet on Far Field Region by Computational Aero-Acoustics (CAA) Simulation
title_sort analysis of sound propagation behaviors for supersonic jet on far field region by computational aero-acoustics (caa) simulation
publisher semarak ilmu
publishDate 2024
url http://eprints.uthm.edu.my/12416/1/J17885_1ca2063a0410f38eaddade0a06431092.pdf
http://eprints.uthm.edu.my/12416/
https://doi.org/10.37934/arfmts.117.1.7182
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