11 research outputs found

    A Multiphysics Simulation Approach for Efficient Modeling of Lightning Strike Tests on Aircraft Structures

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    Numerical and Experimental Investigation of Aircraft Panel Deformations During Riveting Process

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    The longitudinal growth of small panels with longitudinal stiffeners has been investigated. The stiffeners have been fastened to the panels with rivets and it has been observed that during this operation the panels expand in the longitudinal direction. It has been observed that the growth is variable and the challenge is to control the riveting process to minimise this variability. In this investigation, the assembly of the small panels and longitudinal stiffeners has been simulated using low and high fidelity nonlinear finite element models. The models have been validated against a limited set of experimental measurements; it was found that more accurate predictions of the riveting process are achieved using high fidelity explicit finite element models. Furthermore, through a series of numerical simulations and probabilistic analyses, the manufacturing process control parameters that influence panel growth have been identified. Alternative fastening approaches were examined and it was found that longitudinal growth can be controlled by changing the design of the dies used for forming the rivets

    Autoclave cure simulation of composite structures applying implicit and explicit FE techniques

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    Simulation of the autoclave manufacturing technique of composites can yield a preliminary estimation of induced residual thermal stresses and deformations that affect component fatigue life, and required tolerances for assembly. In this paper, an approach is proposed to simulate the autoclave manufacturing technique for unidirectional composites. The proposed approach consists of three modules. The first module is a Thermo-chemical model to estimate the temperature and the degree of cure distributions in the composite part during the cure cycle. The second and third modules are a sequential stress analysis using FE-Implicit and FE-Explicit respectively. User-material subroutine is used to model the Viscoelastic properties of the material based on theory of micromechanics
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