Callado Pérez, Víctor(Universitat Politècnica de València, 2019-10-28)
[ES] En el presente Trabajo de Fin de Máster se realiza un estudio aerodinámico de un perfil alar a través de diversas metodologías tales como un estudio experimental, el uso de métodos numéricos que pretenden aproximarse ...
Lázaro, Mario; Niemczynowicz, A.; Siemaszko, A.; García-Raffi, L. M.(Elsevier, 2022-01-20)
[EN] In this paper, wave propagation in structured media with quasiperiodic patterns is investigated. We propose a methodology based on Sturmian sequences for the generation of structured mechanical systems from a given ...
Mansilla Navarro, Francisco de Asís(Universitat Politècnica de València, 2016-10-17)
[EN] Strain gauges are frecuently used for measuring structural deformations with many industrial applications. This project aims to study the experimental operation of this type of sensor, its theoretical validation and ...
Augustin Gallego, Sergio(Universitat Politècnica de València, 2020-09-17)
[EN] Currently, a developing line regarding airplanes goes through appliance of morphing geometrics in terms of approaching the performance of our aircrafts to those achieved by nature with evolution. In this context is ...
[EN] In this paper, exact closed forms of critical damping manifolds for multiple-kernel-based nonviscous single-degree-of-freedom oscillators are derived. The dissipative forces are assumed to depend on the past history ...
Martínez Medina, Óscar(Universitat Politècnica de València, 2020-05-14)
[ES] Este Trabajo Final de Máster verifica un modelo por elementos finitos de un dispositivo de prueba CAI, para paneles de plástico reforzado con fibra de carbono de pared delgada. Las simulaciones se calculan desde el ...
Merle Bolufer, Henriette María(Universitat Politècnica de València, 2018-11-07)
[ES] El presente Trabajo Fin de Grado aborda el estudio aeroelástico en cuanto a
la inestabilidad de una de las partes más fundamentales de una aeronave, las
alas. En concreto, se ha escogido un sistema con un solo grado ...
[ES] Consiste en desarrollar sistemas que permitan una continua monitorización, inspección y detección de daños de las estructuras. Los resultados deberían ser
inmediatamente reportados a una red local o a un centro de ...
Abril Porcar, Cristina(Universitat Politècnica de València, 2018-09-21)
El objetivo principal de este trabajo es llevar a cabo un análisis de diferentes maniobras del avión teniendo en cuenta la deformabilidad de las alas y fuselajes del avión. Para ello se desarrollará un modelo numérico con ...
Lázaro, Mario; Ferrer, Ignacio(Universitat Politècnica de València, 2014-03-31)
[EN] In the present article, a methodology for teaching modeling problem of mixed torsion for thin-walled open
sections. The mathematical analogy of warped twist as a problem of Euler-Bernoulli beams is exploited. In
fact, ...
Lázaro, Mario; Barrera Rodríguez, Jesús; García Olivas, Guillermo(Universitat Politècnica de València, 2018-07-31)
[EN] The subject \Flight Loads" framed in the Master in Aerospace Engineering is based largelyon the concepts seen in courses like Flight Mechanics or Structural Analysis of the Degreein Aerospace Engineering. On the ...
Lázaro, Mario(Universitat Politècnica de València, 2015-07-11)
[EN] Mechanical vibrations as subject can be found within many Engineering and Science Degrees.
To achieve that the students understand the mathematics and its physical interpretation
is the objective we should get as ...
Lázaro, Mario; Pérez-Aparicio, José L.(Elsevier, 2013-02)
A new methodology for the computation of complex eigenvalues for multi-degree-of-freedom linear viscoelastic structures is presented. It is assumed that damping matrix does not only depends on the frequency but also on a ...
[EN] The interaction formulae for the plastic resistance of channel sections under combination of 4 internal forces: the bending moment about strong axis My,Ed, the bending moment about weak axis Mz,Ed, the bimoment BEd ...
[EN] Exact interaction formulae for the plastic resistances of Z-sections under a combination of three internal forces, i.e., the bending moment about the strong axis (y,Ed), bending moment about the weak axis (z,Ed) and ...
López Zamora, Pedro Miguel(Universitat Politècnica de València, 2020-01-10)
[ES] El presente Proyecto Final de Carrera aborda el problema de las grandes deflexiones en vigas y estructuras aeronáuticas esbeltas. Las grandes deflexiones convierten el problema a resolver en no lineal de tipo geométrico. ...
Lázaro, Mario(American Society of Mechanical Engineers (ASME), 2015-12)
Nonviscously damped vibrating systems are characterized by dissipative mechanisms
depending on the time-history of the response velocity, introduced in the physical models
using convolution integrals involving hereditary ...
Alarcón Fallado, Héctor(Universitat Politècnica de València, 2020-01-14)
[EN] The main aim of this thesis was the simulation and posterior analysis of the results of different configurations, which depend mainly on the angle of attack and incident flow's velocity. The geometry had been already ...
Fernández Casanova, César; Gallego-Molina, Antolino; Lázaro, Mario(American Society of Mechanical Engineers (ASME), 2013-12)
This paper presents a new four-node composite element, which incorporates nd delaminations
through its thickness. Based on the extended finite element method (X-FEM) technology,
the element is particularized on a CLT ...