Finite element validation on adhesive joint for composite fuselage model

Finite element analysis (FEA) modeling on adhesive joint for composite fuselage model

In this paper, a finite element modeling via ABAQUS/Explicit simulation on a novel fabrication miniature composite fuselage structure is presented. The fuselage structure is modeled as a continuum composite layup that consisted of a woven C-glass fiber/epoxy 200 g/m 2 composite laminated [908] with the orthotropic elastic material properties and adhesively bonded butt joint. The adhesively bond...

Adhesive joint modeling using compatible element formulation

The use...

Surrogate Model Based Control Considering Uncertainties for Composite Fuselage Assembly

adhesive joint modeling using compatible element formulation

the use of structural adhesives in automotive structures has been increased recently for their role in noise, vibration and harshness (nvh). therefore, the dynamic behavior of structures containing bonded joints has become an area with numerous investigations over the past decades. development of accurate formulations capable of representing adhesively bonded joint dynamics is a step forward in...

Finite element model updating of bolted lap joints implementing identification of joint affected region parameters

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