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dc.contributor.advisorDattaguru, B
dc.contributor.authorSeshadri, B R
dc.date.accessioned2013-06-14T05:05:05Z
dc.date.accessioned2018-07-31T05:15:27Z
dc.date.available2013-06-14T05:05:05Z
dc.date.available2018-07-31T05:15:27Z
dc.date.issued2013-06-14
dc.date.submitted1995
dc.identifier.urihttps://etd.iisc.ac.in/handle/2005/2052
dc.identifier.abstracthttp://etd.iisc.ac.in/static/etd/abstracts/2648/G14122-Abs.pdfen_US
dc.language.isoen_USen_US
dc.relation.ispartofseriesG14122en_US
dc.subjectAircraft Structures - Damageen_US
dc.subjectAircraft Structures - Fatigueen_US
dc.subjectFatigue Crack Growthen_US
dc.subjectCrack Closureen_US
dc.subjectCyclic Loadingen_US
dc.subjectFatigue Crack Closureen_US
dc.subjectCyclic Load Sequenceen_US
dc.subjectFinite Element Analysisen_US
dc.subject.classificationAeronauticsen_US
dc.titleNumerical Simulation And Experimental Correlation Of Crack Closure Phenomenon Under Cyclic Loadingen_US
dc.typeThesisen_US
dc.degree.namePhDen_US
dc.degree.levelDoctoralen_US
dc.degree.disciplineFaculty of Engineeringen_US


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