Residual stress measurement and structural integrity evaluation of SLM Ti-6Al-4V

Simple item page
dc.contributor.advisorTait, Robert Ben_ZA
dc.contributor.authorKnowles, Craig Russellen_ZA
dc.date.accessioned2015-09-14T07:07:59Z
dc.date.available2015-09-14T07:07:59Z
dc.date.issued2012en_ZA
dc.descriptionIncludes bibliographical references.en_ZA
dc.description.abstractThe constant drive toward cleaner, more powerful and more efficient jet turbines in the aerospace industry has narrowed the gap between the aircraft performance envelope requirements and the material limits. The most advanced turbine engines are incredibly complex in design and the weight-saving requirements have placed significant pressure on material capabilities and the manufacturing systems. The next generation of manufacturing methodologies are being developed in the Additive Manufacturing (AM) arena from which Selective Laser Melting (SLM) has emerged as a promising candidate for producing highly complex components. Selective Laser Melting is a laser-based AM technique which builds 3-dimensionsal parts from CAD models in a layerwise fashion...en_ZA
dc.identifier.apacitationKnowles, C. R. (2012). <i>Residual stress measurement and structural integrity evaluation of SLM Ti-6Al-4V</i>. (Thesis). University of Cape Town ,Faculty of Engineering & the Built Environment ,Department of Mechanical Engineering. Retrieved from http://hdl.handle.net/11427/13845en_ZA
dc.identifier.chicagocitationKnowles, Craig Russell. <i>"Residual stress measurement and structural integrity evaluation of SLM Ti-6Al-4V."</i> Thesis., University of Cape Town ,Faculty of Engineering & the Built Environment ,Department of Mechanical Engineering, 2012. http://hdl.handle.net/11427/13845en_ZA
dc.identifier.citationKnowles, C. 2012. Residual stress measurement and structural integrity evaluation of SLM Ti-6Al-4V. University of Cape Town.en_ZA
dc.identifier.ris TY - Thesis / Dissertation AU - Knowles, Craig Russell AB - The constant drive toward cleaner, more powerful and more efficient jet turbines in the aerospace industry has narrowed the gap between the aircraft performance envelope requirements and the material limits. The most advanced turbine engines are incredibly complex in design and the weight-saving requirements have placed significant pressure on material capabilities and the manufacturing systems. The next generation of manufacturing methodologies are being developed in the Additive Manufacturing (AM) arena from which Selective Laser Melting (SLM) has emerged as a promising candidate for producing highly complex components. Selective Laser Melting is a laser-based AM technique which builds 3-dimensionsal parts from CAD models in a layerwise fashion... DA - 2012 DB - OpenUCT DP - University of Cape Town LK - https://open.uct.ac.za PB - University of Cape Town PY - 2012 T1 - Residual stress measurement and structural integrity evaluation of SLM Ti-6Al-4V TI - Residual stress measurement and structural integrity evaluation of SLM Ti-6Al-4V UR - http://hdl.handle.net/11427/13845 ER - en_ZA
dc.identifier.urihttp://hdl.handle.net/11427/13845
dc.identifier.vancouvercitationKnowles CR. Residual stress measurement and structural integrity evaluation of SLM Ti-6Al-4V. [Thesis]. University of Cape Town ,Faculty of Engineering & the Built Environment ,Department of Mechanical Engineering, 2012 [cited yyyy month dd]. Available from: http://hdl.handle.net/11427/13845en_ZA
dc.language.isoengen_ZA
dc.publisher.departmentDepartment of Mechanical Engineeringen_ZA
dc.publisher.facultyFaculty of Engineering and the Built Environment
dc.publisher.institutionUniversity of Cape Town
dc.subject.otherMechanical Engineeringen_ZA
dc.titleResidual stress measurement and structural integrity evaluation of SLM Ti-6Al-4Ven_ZA
dc.typeMaster Thesis
dc.type.qualificationlevelMasters
dc.type.qualificationnameMScen_ZA
uct.type.filetypeText
uct.type.filetypeImage
uct.type.publicationResearchen_ZA
uct.type.resourceThesisen_ZA
Files
Original bundle
Now showing 1 - 1 of 1
Thumbnail Image
Name:
thesis_ebe_2012_knowles_c.pdf
Size:
9.34 MB
Format:
Adobe Portable Document Format
Description:
Download
Collections
Masters