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Please use this identifier to cite or link to this item: http://hdl.handle.net/123456789/634

Title: THE FINITE ELEMENTS ANALYSIS VS. EXPERIMENTAL BUCKLING BEHAVIOR OF THE THINWALLED PLANE GUSSETS
Authors: DIMA, Gabriel
TEODORESCU - DRAGHICESCU, Horatiu
Keywords: aerospace
buckling
welded structures
gusset
finite element analysis
Issue Date: Oct-2014
Publisher: Transilvania University Press of Braşov
Citation: Google Scholar
Series/Report no.: I;143 - 150
Abstract: The lightweight tubular latticed beams are used in aerospace structures as well as in civil engineering applications. Depending of manufacturer, gussets may be used to increase the stiffness and rigidity of the beams. As a continuation of previous researches to obtain lighter structures by using gussets, this article presents the results of a research regarding the plane gussets buckling. Using analytical, finite elements calculation and experimental testing, the buckling behavior of tubular T joints reinforced with gussets was studied. The experimental testing was made for gussets subjected to both compression and tensile loads. The gusset buckling was analyzed together with the joint members failure, conclusions and design recommendation being made.
URI: http://hdl.handle.net/123456789/634
ISBN: 978 – 606 – 19 – 0411 - 2
Appears in Collections:COMAT 2014

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