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FSI-OLKAcad. year: 2013/2014
The influence of longitudinal deformation. The bearing capacity of stiffened panels and thin-walled aircraft structures. Computational methods used in aviation. The stress-strain analysis of aircraft structures and its parts. Sandwich structures. The finite element method introduction. The FEM application on dynamic behaviour of structures. Material and geometric non-linearity. Introduction and practise of FEM application using the MSC-NASTRAN, ANSYS and MSC-PATRAN software packs.
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Specification of controlled education, way of implementation and compensation for absences
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branch M-STL , 1 year of study, summer semester, compulsory
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Computer-assisted exercise