Zobrazeno 1 - 10
of 33
pro vyhledávání: '"Hector Climent"'
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part D: Journal of Automobile Engineering. 237:455-468
Current European vehicle homologation regulations are increasingly restrictive. Recently, World-wide light-duty test cycle (WLTC) and Real driving emissions (RDE) cycles have been introduced as type approval tests for new vehicles. This document stud
Publikováno v:
CEAS Aeronautical Journal. 10:1071-1087
Aeroservoelastic loads calculations usually rely on linear analyses that use implicit structural models (Finite Elements Method) and frequency domain unsteady aerodynamics (Doublet Lattice Method). The hypotheses that underpin this methodology impose
Autor:
Emilio Santos Fernandez, Hector Climent Mañez, Felix Arevalo, Moti Karpel, Jesus Barrera Rodriguez, Martin Weiss
Publikováno v:
AIAA Scitech 2020 Forum.
Autor:
Héctor Climent Puchades
Este libro se enmarca dentro de una línea de investigación sobre los motores de dos tiempos de pequeña cilindrada y gira alrededor de un proyecto de colaboración con la empresa española Nacional Motor S.A. Derbi, a la que agradecemos desde aquí
Publikováno v:
RiuNet. Repositorio Institucional de la Universitat Politécnica de Valéncia
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[EN] Internal combustion engine developments are more focused on efficiency optimization and emission reduction for the upcoming future. To achieve these goals, technologies like downsizing and downspeeding are needed to be developed according to the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::fd6892eec7d9add5ef3bdf96253ad09a
https://doi.org/10.1177/1468087417731654
https://doi.org/10.1177/1468087417731654
Publikováno v:
AIAA Journal. 53:3233-3239
Linear structural dynamics, unsteady aerodynamics, control system, and actuator models are combined for linear aeroservoelastic equations of motion that are augmented with nonlinear feedback loops based on the increased-order modeling approach. Altho
Publikováno v:
Progress in Aerospace Sciences. 71:54-84
© 2014 Elsevier Ltd.Flutter of T-tail configurations is caused by the aeroelastic coupling between the vertical fin and the horizontal stabiliser. The latter is mounted on the fin instead of the fuselage, and hence the arrangement presents distinct
Publikováno v:
57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
High altitude long range aircraft have recently gained research interest due to the varied mission profiles they can fulfil. Consequences of their light design are large structural deformations, which cannot be accurately modelled by linear analysis.
Publikováno v:
54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
Autor:
Alexander Shousetrman, Mordechay Karpel, Alvaro P. de la Serna, Hector Climent, Carlos Maderuelo
Publikováno v:
54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.