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Exact(10)
The distribution of stresses in the meridional direction of the ring element is assumed to be linear with each element.
An analytical formulation for modelling the aerodynamic loads within the finite element is assumed in conformity with classical flutter analysis.
The laminated representative volume element is assumed for obtaining the effective material properties of the laminated composite.
In particular, the force in a spring element is assumed to be given as a function of the displacement from the equilibrium position.
The displacement field of the new element is assumed to be cubic in the axial direction and quadratic in the transverse direction.
The material property within each element is assumed to vary linearly in the thickness direction, which represents the spatial variation of material property of FGM.
Similar(50)
First, the three functions for the radial (or normal), tangential and rotational displacements of an arch element are assumed.
The reinforcement element was assumed to be a bilinear isotropic elastic-perfectly plastic material and identical in tension and compression as shown in Fig. 15.
The displacements within the element are assumed to be due to the superposition of its rigid body motion and the deflections relative to the rigid body configuration.
To develop the proposed finite element, the displacements of a point in the ring element are assumed by a pair of the natural modes of a ring with local deviation: symmetric and asymmetric modes.
A resolution of 0.1 wt.% for the alloying elements is assumed, consistent with manufacturing practice.
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Justyna Jupowicz-Kozak
CEO of Professional Science Editing for Scientists @ prosciediting.com