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Please use this identifier to cite or link to this item: http://repository.iitr.ac.in/handle/123456789/4222
Title: Buckling behavior of blade-, angle-, T-, and hat-stiffened FRP panels subjected to in-plane shear
Authors: Jain H.K.
Upadhyay A.
Published in: Journal of Reinforced Plastics and Composites
Abstract: This article presents parametric studies on simply supported laminated composite stiffened panels subjected to in-plane shear loading. A number of models were analyzed using ANSYS and a database is prepared for blade-, angle-, T-, and hat-stiffened laminated composite panels. Studies are carried out by changing the type of stiffeners, the panel orthotropy ratio, smeared extensional stiffness ratio of stiffener to that of the plate, and extensional stiffness to shear stiffness ratio of the plate. The difference in buckling behavior of different types of stiffened panels is presented. Based on key parameters influencing the buckling behavior, guidelines for better stiffener proportioning are developed, which will be helpful to the designers. ¬© 2010 The Author(s).
Citation: Journal of Reinforced Plastics and Composites(2010), 29(24): 3614-3623
URI: https://doi.org/10.1177/0731684410383450
http://repository.iitr.ac.in/handle/123456789/4222
Issue Date: 2010
Keywords: angle-
Buckling behavior
FE analysis
hat-stiffened panels
in-plane shear loading
laminated composite blade-
T-
ISSN: 7316844
Author Scopus IDs: 36727430500
13608643500
Author Affiliations: Jain, H.K., Department of Civil Engineering, Indian Institute of Technology Roorkee, Roorkee 247667, Uttarakhand, India
Upadhyay, A., Department of Civil Engineering, Indian Institute of Technology Roorkee, Roorkee 247667, Uttarakhand, India
Corresponding Author: Upadhyay, A.; Department of Civil Engineering, Indian Institute of Technology Roorkee, Roorkee 247667, Uttarakhand, India; email: akhilfce@iitr.ernet.in
Appears in Collections:Journal Publications [CE]

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