Parametric study on composite panel subjected to compression load (Record no. 22108)

000 -LEADER
fixed length control field a
003 - CONTROL NUMBER IDENTIFIER
control field OSt
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20250113101413.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 250113b xxu||||| |||| 00| 0 eng d
040 ## - CATALOGING SOURCE
Original cataloging agency AIKTC-KRRC
Transcribing agency AIKTC-KRRC
100 ## - MAIN ENTRY--PERSONAL NAME
9 (RLIN) 25062
Author Shashi Kumar
245 ## - TITLE STATEMENT
Title Parametric study on composite panel subjected to compression load
250 ## - EDITION STATEMENT
Volume, Issue number Vol.105(1), Mar
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc. Mumbai
Name of publisher, distributor, etc. Springer
Year 2024
300 ## - PHYSICAL DESCRIPTION
Pagination 15-24p.
520 ## - SUMMARY, ETC.
Summary, etc. The local buckling and buckling capacity of the stiffened panel is increased with the raising depth of stiffeners; consequently, the panel local buckling can be prevented by maintaining the optimum stiffener depth for the design and use in maximum load bearing capacity of the lightweight structures. This study deals with numerical analysis of the hat-stiffened panel under compression load with the varying parameters of hat-stiffener, three types of Ply configuration, and panel aspect ratio by using FE tool ABAQUS. Using a strain gauge data-logger system, an experimental investigation is also performed on a panel with the boundary conditions of clamped-in-loaded edges and unrestricted two unloaded edges. Load–displacement curve of the experimental results is in good agreement with FE analysis results obtained from ABAQUS for the buckling and collapse of the panel. The buckling load and deformed shapes of the composite panel are analyzed here for the design of the lightweight compressive member. A database is prepared for buckling study on the stiffened panel with varying depth and spacing of stiffeners, panel orthotropy ratio, plies configuration, and aspect ratio. Based on the studies, a few crucial factors that affect buckling behavior are found, and general guidelines are provided for hat-stiffened panels with three different ply configurations.
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM
9 (RLIN) 4621
Topical term or geographic name entry element Civil Engineering
700 ## - ADDED ENTRY--PERSONAL NAME
9 (RLIN) 25063
Co-Author Subodh Kumar Suman
773 0# - HOST ITEM ENTRY
Title Journal of the institution of engineers (India): Series A
Place, publisher, and date of publication Switzerland Springer
International Standard Serial Number 2250-2149
856 ## - ELECTRONIC LOCATION AND ACCESS
URL https://link.springer.com/article/10.1007/s40030-023-00773-2
Link text Click here
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Source of classification or shelving scheme
Koha item type Articles Abstract Database
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Withdrawn status Lost status Source of classification or shelving scheme Damaged status Not for loan Permanent Location Current Location Shelving location Date acquired Barcode Date last seen Price effective from Koha item type
          School of Engineering & Technology (PG) School of Engineering & Technology (PG) Archieval Section 2025-01-13 2025-0024 2025-01-13 2025-01-13 Articles Abstract Database
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