IDR - IIT Kharagpur
Dynamic Stability of Laminated Composite Stiffened Shell Panels with Cutouts Subjected to Non-Uniform in-Plane Harmonic Edge Loading
Login
IDR Home
→
2. Ph.D Theses of IIT Kharagpur
→
Aerospace Engineering
→
Dynamic Stability of Laminated Composite Stiffened Shell Panels Harmonic Edge Loading
→
View Item
JavaScript is disabled for your browser. Some features of this site may not work without it.
Dynamic Stability of Laminated Composite Stiffened Shell Panels with Cutouts Subjected to Non-Uniform in-Plane Harmonic Edge Loading
Patel, Shuvendu Narayan
URI:
http://www.idr.iitkgp.ac.in/xmlui/handle/123456789/85
Date:
2006
Show full item record
Files in this item
Name:
NB13530_Abstract.pdf
Size:
216.5Kb
Format:
PDF
Description:
PDF File
View/
Open
Name:
NB13530_Chapter1.pdf
Size:
230.0Kb
Format:
PDF
Description:
PDF File
View/
Open
Name:
NB13530_TOC.pdf
Size:
221.1Kb
Format:
PDF
Description:
PDF File
View/
Open
Name:
NB13530_Thesis.pdf
Size:
6.574Mb
Format:
PDF
View/
Open
This item appears in the following Collection(s)
Dynamic Stability of Laminated Composite Stiffened Shell Panels Harmonic Edge Loading
Search DSpace
Search DSpace
This Collection
Advanced Search
Browse
All of DSpace
Communities & Collections
By Issue Date
Authors
Titles
Subjects
This Collection
By Issue Date
Authors
Titles
Subjects
My Account
Login