All Files
Doc
Ppt
DETAILED INFORMATION
WHAT IS THIS DOCUMENT ABOUT? :
An analytical study has been carried out to investigate the buckling behaviour of rectangular composite stiffenedpanels with circular cutouts. The effect ofparameters such as cutout size, inclination ofcutoutflange, location ofstringer with respect to the cutout and stringer height on the buckling and postbuckling performance has been studied through non-linear FE analysis. The study has helped to develop a few guidelines in thepreliminary design stage ofcomposite wingpanels.
Buckling and PostbiiekSing Studies on Stiffened Composite Panels with Circular Cutouts Author : Byji Varughese, A. Kishore 0 , K. Radhakrishna and M. Subba Rao
| Keywords | : | Buckling Postbuckling Stiffened panels Cutout First ply failure |
| file credit | : | Byji Varughese, A. Kishore 0 , K. Radhakrishna and M. Subba Rao |
| file type | : | |
| file topic | : | Engineering |
| rating | : |   Loading ... |
| viewed | : | 111 times |
| file address | : | nal-ir.nal.res.in/2488/01/article-369-379.pdf |
pdf preview:
file link is informed by: noname, http://filesforbrain.com
| « Geometrically Nonlinear Static Analysis of 3D Trusses Using the Arc-Length Method | Accuracy and Performance Comparison NEiNastran vs. MSC.Nastran vs. Abaqus vs. Marc Version 8.3 » |