Simultaneous structural/acoustical design of composite panels

Since advanced composite materials generally experience coincidence at lower frequencies than metals when used in aircraft fuselage sidewalls, they may allow more transmission of airborne noise thereby requiring heavier acoustical treatments. A sequential design approach of addressing first structur...

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Main Author: Ruckman, Christopher E.
Other Authors: Aerospace Engineering
Format: Others
Language:en_US
Published: Virginia Polytechnic Institute and State University 2019
Subjects:
Online Access:http://hdl.handle.net/10919/91150
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spelling ndltd-VTETD-oai-vtechworks.lib.vt.edu-10919-911502020-09-26T05:37:50Z Simultaneous structural/acoustical design of composite panels Ruckman, Christopher E. Aerospace Engineering LD5655.V855 1986.R835 Composite materials Acoustical materials Since advanced composite materials generally experience coincidence at lower frequencies than metals when used in aircraft fuselage sidewalls, they may allow more transmission of airborne noise thereby requiring heavier acoustical treatments. A sequential design approach of addressing first structural and then acoustical design does not take advantage of structural/acoustical coupling. A simultaneous approach is expected to help minimize the total sidewall mass. This thesis uses numerical optimization to examine structural/acoustical interactions and compare the sequential and simultaneous design approaches. Acoustical performance is defined in terms of the infinite panel transmission loss at frequencies surrounding the coincidence region (1600 Hz - 12800 Hz for the panels studied.) Impedance transfer theory is used to predict the acoustical properties of a flat unstiffened anisotropic panel treated with a fibrous acoustic blanket, airgap, and limp-mass septum. Structural analysis is based on a fatigue damage resistance criterion. Sequentially designed treated composite panels exibit transmission losses 15 dB - 45 dB higher (transmitted pressure is 6 - 180 times smaller) than a structurally equivalent, equal-mass aluminum panel. Depending on the type of acoustic excitation (specific incidence direction or diffuse source) and the acoustic frequency considered, the simultaneous approach alters the sequential minimum-mass panel in order to 1) improve low frequency performance by raising coincidence frequencies, 2) improve high frequency performance by lowering coincidence frequencies, or 3) make the coincidence region as narrow as possible. Since these structural alterations require that more mass be allotted to the panel and less to the treatment, they only occur for strong structural/acoustical interactions (i.e. near coincidence.) The simultaneous design approach can achieve a moderate improvement (TL increased up to 10 dB, transmitted pressure decreased by a factor or 3) over a sequential design for a particular acoustic performance index, although computation time is increased and acoustic performance may be sacrificed in other regions. M.S. 2019-07-03T20:34:02Z 2019-07-03T20:34:02Z 1986 Thesis Text http://hdl.handle.net/10919/91150 en_US OCLC# 15255686 In Copyright http://rightsstatements.org/vocab/InC/1.0/ xii, 138 leaves application/pdf application/pdf Virginia Polytechnic Institute and State University
collection NDLTD
language en_US
format Others
sources NDLTD
topic LD5655.V855 1986.R835
Composite materials
Acoustical materials
spellingShingle LD5655.V855 1986.R835
Composite materials
Acoustical materials
Ruckman, Christopher E.
Simultaneous structural/acoustical design of composite panels
description Since advanced composite materials generally experience coincidence at lower frequencies than metals when used in aircraft fuselage sidewalls, they may allow more transmission of airborne noise thereby requiring heavier acoustical treatments. A sequential design approach of addressing first structural and then acoustical design does not take advantage of structural/acoustical coupling. A simultaneous approach is expected to help minimize the total sidewall mass. This thesis uses numerical optimization to examine structural/acoustical interactions and compare the sequential and simultaneous design approaches. Acoustical performance is defined in terms of the infinite panel transmission loss at frequencies surrounding the coincidence region (1600 Hz - 12800 Hz for the panels studied.) Impedance transfer theory is used to predict the acoustical properties of a flat unstiffened anisotropic panel treated with a fibrous acoustic blanket, airgap, and limp-mass septum. Structural analysis is based on a fatigue damage resistance criterion. Sequentially designed treated composite panels exibit transmission losses 15 dB - 45 dB higher (transmitted pressure is 6 - 180 times smaller) than a structurally equivalent, equal-mass aluminum panel. Depending on the type of acoustic excitation (specific incidence direction or diffuse source) and the acoustic frequency considered, the simultaneous approach alters the sequential minimum-mass panel in order to 1) improve low frequency performance by raising coincidence frequencies, 2) improve high frequency performance by lowering coincidence frequencies, or 3) make the coincidence region as narrow as possible. Since these structural alterations require that more mass be allotted to the panel and less to the treatment, they only occur for strong structural/acoustical interactions (i.e. near coincidence.) The simultaneous design approach can achieve a moderate improvement (TL increased up to 10 dB, transmitted pressure decreased by a factor or 3) over a sequential design for a particular acoustic performance index, although computation time is increased and acoustic performance may be sacrificed in other regions. === M.S.
author2 Aerospace Engineering
author_facet Aerospace Engineering
Ruckman, Christopher E.
author Ruckman, Christopher E.
author_sort Ruckman, Christopher E.
title Simultaneous structural/acoustical design of composite panels
title_short Simultaneous structural/acoustical design of composite panels
title_full Simultaneous structural/acoustical design of composite panels
title_fullStr Simultaneous structural/acoustical design of composite panels
title_full_unstemmed Simultaneous structural/acoustical design of composite panels
title_sort simultaneous structural/acoustical design of composite panels
publisher Virginia Polytechnic Institute and State University
publishDate 2019
url http://hdl.handle.net/10919/91150
work_keys_str_mv AT ruckmanchristophere simultaneousstructuralacousticaldesignofcompositepanels
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