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For the special case of an orthotropic plate, explicit plate equations are presented and compared analytically and numerically to other approximate theories given in the literature.
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To support this conversion project, reference models with representative experiment target loading and explicit fuel plate representation were developed and benchmarked for both fuels to (1) allow for consistent comparison between designs for both fuel types and (2) assess the potential impact of low-enriched uranium conversion.
A variational formulation of the Ritz method is used to establish an eigenvalue problem, and explicit solutions of plate local buckling coefficients in term of the rotational restraint stiffness (k) are obtained.
The model has realistic tectonic plates, which include oceanic lithosphere, that are defined by explicit and rigorously managed plate boundaries, the nature and kinematics of which are derived from geological evidence and plate tectonic principles.
In this paper, a method to compute explicit solutions for laminated plate with arbitrary stacking sequences is presented.
The process model used a sequential dynamic explicit formulation for the plate pressing phase and a static implicit formulation for the unloading (springback) phase in the Lagrangian framework.
For laminated plates, an explicit parametric representation of the yield surface ∂Ghomp is given thanks to the π-function (the plastic dissipation power density function) that describes the local strength domain at each point of the plate.
Based on the computed data, two different design equations for sufficiently long plates are developed which allow for a rapid and closed-form analytical assessment of the buckling behavior of symmetrically layered composite plates under explicit consideration of bending twisting coupling.
The applicability of the explicit solutions of restrained composite plates is illustrated in the discrete plate analysis of two composite structures: short thin-walled composite columns and honeycomb sandwich cores.
We present explicit relations for three-layer sandwich plates which have a wide range of applications in structural/mechanical engineering fields.
Examination of the eigenvalues of the velocity solution gives an explicit relationship for the size of the plate penetration hole.
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CEO of Professional Science Editing for Scientists @ prosciediting.com