• Boundary element methods for the prediction of aircraft noise shielding in flight

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    Clancy TCD THESIS 9138 Boundary element.pdf (124.22 MB)

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    2011

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    Trinity College (Dublin, Ireland). Department of Mechanical and Manufacturing Engineering

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    Cathal Clancy, 'Boundary element methods for the prediction of aircraft noise shielding in flight', [thesis], Trinity College (Dublin, Ireland). Department of Mechanical and Manufacturing Engineering, 2011, pp 215

    Abstract

    Aircraft noise emissions may be significantly reduced by positioning the aeroengines above the wings or fuselage so as to utilize the shielding effect of the airframe. Computational tools are likely to play a key role in the design of future low noise aircraft that maximize this shielding effect.

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    http://hdl.handle.net/2262/78843

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    Mechanical & Manufacturing Eng (Theses and Dissertations)
    Trinity College Dublin Theses & Dissertations

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    Keywords

    Mechanical and Manufacturing Engineering, Ph.D., Ph.D. Trinity College Dublin

    Author: Clancy, Cathal

    Qualification name: Doctor of Philosophy (Ph.D.)
    Publisher: Trinity College (Dublin, Ireland). Department of Mechanical and Manufacturing Engineering
    Type of material: thesis