ABSTRAK Muhammad Rizki Mahalik
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In this thesis, one numerical strategy is conducted as an alternative approach to
other existing methods in simulating the Fluid Structure Interaction (FSI) of an
amphibious aircraft pontoon section subjected to hydrodynamic loading. As one of
principal components of amphibious aircraft, the analysis of aircraft pontoon
withstanding an impact load during landing is carried out. Landing phase has been
considered as critical condition as the structures were being dependable to handle
the supporting role for the whole aircraft.
Within ABAQUS environment, FSI simulation is performed by utilising the
Coupled Eulerian-Lagrangian (CEL) in maintaining the solid body being
undisturbed by the fluids, instead it flows around the body. With the development
of computational mechanics, such methods known as Multiscale Modelling is
introduced to reduce computational time and resource while still maintaining its
accuracy. As the Multistage Multiscale Modelling has been carried out, here, the
Concurrent Multiscale Modelling is performed as an alternative strategy to model
the pontoon section undergoes hydrodynamic loading.
Beforehand, static convergence tests were conducted to ensure the reliability of
elements size being used during the simulation. Moreover, from the FSI simulation,
the Concurrent Multiscale Model turned out to be outperformed the global solid
model, while having a comparable performance with the Multistage Multiscale
Modelling, in terms of stress distribution and usage of computational resource,
compared to the global shell model as the reference.