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HomeKey Engineering MaterialsKey Engineering Materials Vol. 887Designing of Thin Composite Panels with the...

Designing of Thin Composite Panels with the Post-Buckling Behavior Considering Rigid Support and Loading with Shear Flows

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Abstract:

Geometrically non-linear problem of orthotropic thin rectangular panel post-buckling behavior with shear is solved. Deflection function takes all-boundary rigid support conditions into account. Based on derived solution method of smooth panels design which can be used for aircraft structures rib and spar webs optimal parameters is suggested.

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Periodical:

Key Engineering Materials (Volume 887)

Pages:

657-661

DOI:

https://doi.org/10.4028/www.scientific.net/KEM.887.657

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Online since:

May 2021

Authors:

O. Mitrofanov*, O. Mazen

Keywords:

All-Round Rigid Support, Orthotropic Material, Post-Buckling Behavior, Rectangular Panels, Shear

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© 2021 Trans Tech Publications Ltd. All Rights Reserved

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