Fatigue due to noise-induced pressure

T. W. Wu; J. J. Wang; A. F. Seybert

doi:10.1115/91-GT-150

Fatigue due to noise-induced pressure

T. W. Wu, J. J. Wang, A. F. Seybert

Mechanical and Aerospace Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Abstract

The paper presents results of a preliminary study of the acoustic fatigue of an airframe structure as a result of turbojet engine noise. The acoustic pressure distribution, induced by jet-noise, is determined by a coupled FEM/BEM approach. A model of an airframe structure with no defects or microcracks is assumed to be subjected to loadings induced by a time-harmonic noise source. Solution techniques are summarized. A method is presented to analyze the acoustic stresses, additional to mechanical loading induced stresses, for the potential to initiate fatigue cracks and propagation of these cracks. Applications to similar structural systems are suggested.

Original language	English
Title of host publication	Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; IGTI Scholar Award; General
ISBN (Electronic)	9780791879023
DOIs	https://doi.org/10.1115/91-GT-150
State	Published - 1991
Event	ASME 1991 International Gas Turbine and Aeroengine Congress and Exposition, GT 1991 - Orlando, United States Duration: Jun 3 1991 → Jun 6 1991

Publication series

Name	Proceedings of the ASME Turbo Expo
Volume	5

Conference

Conference	ASME 1991 International Gas Turbine and Aeroengine Congress and Exposition, GT 1991
Country/Territory	United States
City	Orlando
Period	6/3/91 → 6/6/91

Bibliographical note

Publisher Copyright:
Copyright © 1991 by ASME.

ASJC Scopus subject areas

General Engineering

Access to Document

10.1115/91-GT-150

Cite this

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title = "Fatigue due to noise-induced pressure",

abstract = "The paper presents results of a preliminary study of the acoustic fatigue of an airframe structure as a result of turbojet engine noise. The acoustic pressure distribution, induced by jet-noise, is determined by a coupled FEM/BEM approach. A model of an airframe structure with no defects or microcracks is assumed to be subjected to loadings induced by a time-harmonic noise source. Solution techniques are summarized. A method is presented to analyze the acoustic stresses, additional to mechanical loading induced stresses, for the potential to initiate fatigue cracks and propagation of these cracks. Applications to similar structural systems are suggested.",

author = "Wu, {T. W.} and Wang, {J. J.} and Seybert, {A. F.}",

note = "Publisher Copyright: Copyright {\textcopyright} 1991 by ASME.; ASME 1991 International Gas Turbine and Aeroengine Congress and Exposition, GT 1991 ; Conference date: 03-06-1991 Through 06-06-1991",

year = "1991",

doi = "10.1115/91-GT-150",

language = "English",

series = "Proceedings of the ASME Turbo Expo",

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Wu, TW, Wang, JJ & Seybert, AF 1991, Fatigue due to noise-induced pressure. in Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; IGTI Scholar Award; General. Proceedings of the ASME Turbo Expo, vol. 5, ASME 1991 International Gas Turbine and Aeroengine Congress and Exposition, GT 1991, Orlando, United States, 6/3/91. https://doi.org/10.1115/91-GT-150

Fatigue due to noise-induced pressure. / Wu, T. W.; Wang, J. J.; Seybert, A. F.
Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; IGTI Scholar Award; General. 1991. (Proceedings of the ASME Turbo Expo; Vol. 5).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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N2 - The paper presents results of a preliminary study of the acoustic fatigue of an airframe structure as a result of turbojet engine noise. The acoustic pressure distribution, induced by jet-noise, is determined by a coupled FEM/BEM approach. A model of an airframe structure with no defects or microcracks is assumed to be subjected to loadings induced by a time-harmonic noise source. Solution techniques are summarized. A method is presented to analyze the acoustic stresses, additional to mechanical loading induced stresses, for the potential to initiate fatigue cracks and propagation of these cracks. Applications to similar structural systems are suggested.

AB - The paper presents results of a preliminary study of the acoustic fatigue of an airframe structure as a result of turbojet engine noise. The acoustic pressure distribution, induced by jet-noise, is determined by a coupled FEM/BEM approach. A model of an airframe structure with no defects or microcracks is assumed to be subjected to loadings induced by a time-harmonic noise source. Solution techniques are summarized. A method is presented to analyze the acoustic stresses, additional to mechanical loading induced stresses, for the potential to initiate fatigue cracks and propagation of these cracks. Applications to similar structural systems are suggested.

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BT - Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; IGTI Scholar Award; General

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Fatigue due to noise-induced pressure

Abstract

Publication series

Conference

Bibliographical note

ASJC Scopus subject areas

Access to Document

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