Please use this identifier to cite or link to this item: http://hdl.handle.net/20.500.11889/7892
Title: Reducing airplane cabin and fuselage noise using active and passive control techniques
Authors: Abu Hanieh, Ahmed 
Keywords: Aircraft cabins - Noise;active control of vibrations;Passive control of vibrations;Tuned mass dampers;Integral force feedback;IFF;Acoustical engineering;Structural control (Engineering)
Issue Date: Jan-2023
Publisher: Inderscience
Source: Hanieh, A.A., 2023. Reducing airplane cabin and fuselage noise using active and passive control techniques. International Journal of Vehicle Noise and Vibration, 19(1-2), pp.67-77.
Abstract: The focus of this research is on making a wide discussion about the sources and control techniques of noise propagating to the passenger airplane cabin and fuselage. The first part of the document discusses the effects of vibration induced noise (vibro-acoustic) transmitted from airplane engines and aerodynamic impact on the main body of the aircraft besides to air-conditioning vibrations. These vibrations transmit noise to the cabin and fuselage causing discomfort to passengers. Finite element modelling technique is used to make this study. Two different solutions are suggested to control and get rid of these vibrations; passive control techniques using tuned mass dampers is one of the suggested solutions and the second solution is an active control technique using piezoelectric actuator and force sensor with integral force feedback compensator. The performance of the active control is much higher than that of the passive one but it is much more expensive.
URI: http://hdl.handle.net/20.500.11889/7892
DOI: https://doi.org/10.1504/IJVNV.2023.130248
Appears in Collections:Fulltext Publications

Files in This Item:
File Description SizeFormat
24_Journal_IJVNV_2023_Fuselage noise.pdf790.73 kBAdobe PDFView/Open
Show full item record

Page view(s)

29
checked on Jun 27, 2024

Download(s)

96
checked on Jun 27, 2024

Google ScholarTM

Check

Altmetric


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.