نتایج جستجو برای: fml stiffened shell

تعداد نتایج: 53728  

Journal: :Mathematical Problems in Engineering 2021

A novel approach for solving the stiffened shell structures by using an edge-based smoothed MITC3 finite element method (ES-MITC3) is presented in this paper. The ES-MITC3 efficient combining (ES-FEM) with original triangular to not only significantly improve accuracy but also overcome shear-locking phenomenon Reissner–Mindlin analysis. In study, applied and then reinforced stiffeners based on ...

Journal: :Nuclear Science and Techniques 2023

Abstract To improve the efficiency and accuracy of single-event effect (SEE) research at Heavy Ion Research Facility Lanzhou, Hi’Beam-SEE must precisely localize position which each heavy ion hitting integrated circuit (IC) causes SEE. In this study, we propose a fast multi-track location (FML) method based on deep learning to locate particle track with high speed accuracy. FML can process vast...

2008
Alvaro Hernández Beatriz López David Pardo Raúl Santos Luis Hernández José Relaño Ma Carmen Rodríguez

In this paper we propose a modular structure to define communication acts with verbal and nonverbal elements inspired in the SAIBA model. Our modular structure is a conceptual interpretation of the functional features of a multimodal interaction platform we have developed, with an embodied conversational agent (ECA) that implements verbal and gestural communication strategies aimed at minimisin...

2012
VLADIMIR L. POPOV

We construct counterexamples to the rationality conjecture regarding the new version of the Makar-Limanov invariant introduced in [Li2]. Let k be an algebraically closed field. Below variety means algebraic variety over k in the sense of Serre (so algebraic group means algebraic group over k). We use standard notation and conventions of [Bo] and [Sp]. In particular, given a variety X, we denote...

2009
Wei Wang S. Guo Nan Chang Wei Yang

Optimal design of laminated composite stiffened panels of symmetric and balanced layup with different number of T-shape stiffeners is investigated and presented. The stiffened panels are simply supported and subjected to uniform biaxial compressive load. In the optimization for the maximum buckling load without weight penalty, the panel skin and the stiffened laminate stacking sequence, thickne...

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