Proceedings Vol. 26 (2020)
ENGINEERING MECHANICS 2020
November 24 – 25, 2020, Brno, Czech Republic
Copyright © 2020 Brno University of Technology Institute of Solid Mechanics, Mechatronics and Biomechanics
ISSN 1805-8248 (printed)
ISSN 1805-8256 (electronic)
list of papers scientific commitee
pages 358 - 361, full text
Composite panels are widely used in aerospace structural applications (e.g., fuselage, wings). A typical hat-stiffened panel was manufactured using the vacuum infusion process. The applied material is carbon/epoxy 10-layer laminate. The global properties of the laminate were computed from the mechanical properties of a single ply. Finite element model of the panel was created and validated experimentally by measuring bending stiffness of the panel in different points.
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All papers were reviewed by members of the scientific committee.