Please use this identifier to cite or link to this item: http://www.idr.iitkgp.ac.in/xmlui/handle/123456789/85
Title: Dynamic Stability of Laminated Composite Stiffened Shell Panels with Cutouts Subjected to Non-Uniform in-Plane Harmonic Edge Loading
Authors: Patel, Shuvendu Narayan
Keywords: Shell Panels
Buckling
Geometric Stiffness
Vibration
Dynamic Stability
Issue Date: 2006
Publisher: IIT Kharagpur
Gov't Doc #: NB13530
NB13750 ; NB13824
URI: http://www.idr.iitkgp.ac.in/xmlui/handle/123456789/85
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


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