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dc.contributor.advisorRice, Henry
dc.contributor.authorClancy, Cathal
dc.date.accessioned2017-01-18T10:50:36Z
dc.date.available2017-01-18T10:50:36Z
dc.date.issued2011
dc.identifier.citationCathal 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
dc.identifier.otherTHESIS 9138
dc.description.abstractAircraft 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.
dc.format1 volume
dc.language.isoen
dc.publisherTrinity College (Dublin, Ireland). Department of Mechanical and Manufacturing Engineering
dc.relation.isversionofhttp://stella.catalogue.tcd.ie/iii/encore/record/C__Rb14633129
dc.subjectMechanical and Manufacturing Engineering, Ph.D.
dc.subjectPh.D. Trinity College Dublin
dc.titleBoundary element methods for the prediction of aircraft noise shielding in flight
dc.typethesis
dc.type.supercollectionthesis_dissertations
dc.type.supercollectionrefereed_publications
dc.type.qualificationlevelDoctoral
dc.type.qualificationnameDoctor of Philosophy (Ph.D.)
dc.rights.ecaccessrightsopenAccess
dc.format.extentpaginationpp 215
dc.description.noteTARA (Trinity’s Access to Research Archive) has a robust takedown policy. Please contact us if you have any concerns: rssadmin@tcd.ie
dc.identifier.urihttp://hdl.handle.net/2262/78843


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