Please use this identifier to cite or link to this item: https://hdl.handle.net/2440/19503
Full metadata record
DC FieldValueLanguage
dc.contributor.authorLee, Hock Sengen
dc.date.issued1983en
dc.identifier.urihttp://hdl.handle.net/2440/19503-
dc.descriptionA supplement to this thesis containing tabulations of all acoustic data is available from the Department of Mechanical Engineering, University of Adelaideen
dc.descriptionBibliography: leaves 109-113en
dc.descriptionix, 118 leaves, 9 plates : ill ; 30 cm.en
dc.format.extent219141 bytesen
dc.format.mimetypeapplication/pdfen
dc.language.isoenen
dc.subject.ddc629.13232 19en
dc.subject.lcshAerodynamic noise.en
dc.subject.lcshTurbulence.en
dc.titleExperimental study on the effects of density, Mach number and geometry on the large scale structure in a turbulent jet and its radiated noise / by Lee Hock Sengen
dc.typeThesisen
dc.contributor.schoolDept. of Mechanical Engineeringen
dc.provenanceThis electronic version is made publicly available by the University of Adelaide in accordance with its open access policy for student theses. Copyright in this thesis remains with the author. This thesis may incorporate third party material which has been used by the author pursuant to Fair Dealing exception. If you are the author of this thesis and do not wish it to be made publicly available or If you are the owner of any included third party copyright material you wish to be removed from this electronic version, please complete the take down form located at: http://www.adelaide.edu.au/legals-
dc.description.dissertationThesis (Ph.D.)--University of Adelaide, Dept. of Mechanical Engineering, 1984en
Appears in Collections:Mechanical Engineering theses
Research Theses

Files in This Item:
File Description SizeFormat 
01front.pdf214 kBAdobe PDFView/Open
02whole.pdf6.16 MBAdobe PDFView/Open


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