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A ray tracing method applied to the propagation of jet noise

A ray tracing method applied to the propagation of jet noise
A ray tracing method applied to the propagation of jet noise
Aircraft noise remains a major obstacle for air traffic growth as new aircraft must meet ever more stringent certification requirements for noise emissions around airports. A large part of aircraft noise arises from the engine and manufacturers have taken steps to make them quieter. In the case of turbofan aircraft this has been achieved largely by increasing the bypass ratio. Today, there is little room left for further reduction of noise in this way and more novel solutions must be found. One such method is to redesign exhaust nozzles in order manipulate the flow in a way that gives an acoustic benefit, for example in non-circular nozzles a larger flow field may shield the noise sources more efficiently. In turn, this brings a requirement for more advanced noise prediction tools. In this paper, a jet noise prediction method based on Lighthill’s Acoustic Analogy coupled with a Ray-Tracing theory is presented. A full 3D Ray-Tracing method is developed which provides information about the refraction effects due to wave propagation in a non-axisymmetric jet flow. Using the turbulence information obtained from a RANS CFD simulation and the refractions effects obtained from the Ray-Tracing, the method calculates the far-field noise using a modified Lighthill’s equation (LRT). The classic jet noise prediction method, known as MGBK, is also used here for comparison. Results are presented for subsonic single-stream jets operating at Mach 0.75, 0.9 and different temperatures. The refraction results obtained using the ray tracing method are compared with those found using Lilley’s wave propagation equation. Comparisons have shown that the ray tracing method works well for all polar angles outside the zone of silence. The far-field noise comparisons have shown that the LRT method is capable of capturing the peak frequency much better than the MGBK method. The general trend of the spectrum at high and low frequencies as obtained using the new method is also better than those found using MGBK.

Illario, Carlos Roberto
f45cc33e-cfaf-44ea-ae96-9fd90a8f1810
Meneghini, Julio Romano
19d617b7-de6b-4450-850d-67ee2dbc7578
Azarpeyvand, Mahdi
1d61e228-84cd-4330-bacd-0b189f0b05df
Self, Rod H.
8b96166d-fc06-48e7-8c76-ebb3874b0ef7
Illario, Carlos Roberto
f45cc33e-cfaf-44ea-ae96-9fd90a8f1810
Meneghini, Julio Romano
19d617b7-de6b-4450-850d-67ee2dbc7578
Azarpeyvand, Mahdi
1d61e228-84cd-4330-bacd-0b189f0b05df
Self, Rod H.
8b96166d-fc06-48e7-8c76-ebb3874b0ef7

Illario, Carlos Roberto, Meneghini, Julio Romano, Azarpeyvand, Mahdi and Self, Rod H. (2010) A ray tracing method applied to the propagation of jet noise. 17th International Congress on Sound and Vibration (ICSV), Cairo, Cairo, Egypt. 17 - 21 Jul 2010. 8 pp .

Record type: Conference or Workshop Item (Paper)

Abstract

Aircraft noise remains a major obstacle for air traffic growth as new aircraft must meet ever more stringent certification requirements for noise emissions around airports. A large part of aircraft noise arises from the engine and manufacturers have taken steps to make them quieter. In the case of turbofan aircraft this has been achieved largely by increasing the bypass ratio. Today, there is little room left for further reduction of noise in this way and more novel solutions must be found. One such method is to redesign exhaust nozzles in order manipulate the flow in a way that gives an acoustic benefit, for example in non-circular nozzles a larger flow field may shield the noise sources more efficiently. In turn, this brings a requirement for more advanced noise prediction tools. In this paper, a jet noise prediction method based on Lighthill’s Acoustic Analogy coupled with a Ray-Tracing theory is presented. A full 3D Ray-Tracing method is developed which provides information about the refraction effects due to wave propagation in a non-axisymmetric jet flow. Using the turbulence information obtained from a RANS CFD simulation and the refractions effects obtained from the Ray-Tracing, the method calculates the far-field noise using a modified Lighthill’s equation (LRT). The classic jet noise prediction method, known as MGBK, is also used here for comparison. Results are presented for subsonic single-stream jets operating at Mach 0.75, 0.9 and different temperatures. The refraction results obtained using the ray tracing method are compared with those found using Lilley’s wave propagation equation. Comparisons have shown that the ray tracing method works well for all polar angles outside the zone of silence. The far-field noise comparisons have shown that the LRT method is capable of capturing the peak frequency much better than the MGBK method. The general trend of the spectrum at high and low frequencies as obtained using the new method is also better than those found using MGBK.

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More information

e-pub ahead of print date: July 2010
Additional Information: Paper 676, CD-ROM
Venue - Dates: 17th International Congress on Sound and Vibration (ICSV), Cairo, Cairo, Egypt, 2010-07-17 - 2010-07-21

Identifiers

Local EPrints ID: 172057
URI: http://eprints.soton.ac.uk/id/eprint/172057
PURE UUID: 3f4aa259-faa4-4910-b271-2810593cd408

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Date deposited: 24 Jan 2011 11:51
Last modified: 09 Jan 2022 07:07

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Contributors

Author: Carlos Roberto Illario
Author: Julio Romano Meneghini
Author: Mahdi Azarpeyvand
Author: Rod H. Self

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