1. DSpace at My University
  2. 2. Ph.D Theses of IIT Kharagpur
  3. Aerospace Engineering
  4. Dynamic Stability of Laminated Composite Stiffened Shell Panels Harmonic Edge Loading
Please use this identifier to cite or link to this item: http://www.idr.iitkgp.ac.in/xmlui/handle/123456789/85
Full metadata record
DC FieldValueLanguage
dc.contributor.authorPatel, Shuvendu Narayan
dc.date.accessioned2010-02-02T04:32:02Z
dc.date.available2010-02-02T04:32:02Z
dc.date.issued2006
dc.identifier.govdocNB13530
dc.identifier.govdocNB13750 ; NB13824
dc.identifier.urihttp://www.idr.iitkgp.ac.in/xmlui/handle/123456789/85
dc.language.isoenen
dc.publisherIIT Kharagpuren
dc.subjectShell Panels
dc.subjectBuckling
dc.subjectGeometric Stiffness
dc.subjectVibrationen
dc.subjectDynamic Stability
dc.titleDynamic Stability of Laminated Composite Stiffened Shell Panels with Cutouts Subjected to Non-Uniform in-Plane Harmonic Edge Loadingen
dc.typeThesisen
Appears in Collections:Dynamic Stability of Laminated Composite Stiffened Shell Panels Harmonic Edge Loading

Files in This Item:
File Description SizeFormat 
NB13530_Abstract.pdfPDF File216.53 kBAdobe PDFThumbnail
View/Open
NB13530_Chapter1.pdfPDF File230.05 kBAdobe PDFThumbnail
View/Open
NB13530_TOC.pdfPDF File221.11 kBAdobe PDFThumbnail
View/Open
NB13530_Thesis.pdf6.73 MBAdobe PDFThumbnail
View/Open
Show simple item record


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