Levantamiento industrial del helicóptero OH-58 KIOWA perteneciente al Museo Histórico Militar de Valencia

Autor: Pachés Moreno, Josep Vicent

Publikováno v: RiuNet. Repositorio Institucional de la Universitat Politécnica de Valéncia
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[ES] El trabajo consiste en un levantamiento industrial, correspondiente con un escáner láser, para un posterior diseño CAD del helicóptero, impresión 3D y estudio aerodinámico.
[EN] The work consists of an industrial survey, corresponding

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::535d47544ca1e3464d777b00f1a855ba
https://hdl.handle.net/10251/125462

Large-Eddy Simulation of constant volume combustion in a ground-breaking new aeronautical engine

Autor: Exilard, Gorka

Au cours des dernières années, le transport aérien de passagers connaît un développement sans cesse croissant et continue ainsi d’accroire sa contribution aux émissions mondiale de CO2. Par conséquent, un effort commun entre les avionneurs e

Externí odkaz: http://www.theses.fr/2018SACLC082/document

Unilateral contact induced blade/casing vibratory interactions in impellers: Analysis for rigid casings

Autor: Batailly, Alain, Meingast, Markus, Legrand, Mathias

Publikováno v: Journal of Sound and Vibration
Journal of Sound and Vibration, Elsevier, 2015, 17, pp.244-262. ⟨10.1016/j.jsv.2014.10.010⟩

International audience; This contribution addresses the vibratory analysis of unilateral-contact induced structural interactions between a bladed impeller and its surrounding rigid casing. Such assemblies can be found in helicopter or small aircraft

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=od_______212::652696f8cbc23e424c9f462380bb1116
https://hal.archives-ouvertes.fr/hal-01120157/document

Comportement dynamique d'une aube de compresseur haute-pression sous l'effet cumulé d'un chargement aérodynamique et de contraintes unilatérales de contact

Autor: Francois Maurice Garcin, Mathias Legrand, Alain Batailly, Antoine Millecamps

Publikováno v: Conférence ASME Turbo Expo 2014
ASME Turbo Expo 2014
ASME Turbo Expo 2014, ASME, Jun 2014, Düsseldorf, Germany. ⟨10.1115/GT2014-25675⟩

International audience; Recent studies focused on the numerical prediction of structural instabilities that may arise in rotating components of an aircraft engine. These instabilities are commonly classified into two categories: those induced by aero

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3191e06a977e801119407d68c9381c33
https://hal.archives-ouvertes.fr/hal-01130542/file/articleHaL.pdf

Nouvelle conception d'une aube de compresseur haute-pression en prenant en compte des interactions structurelles non-linéaires

Autor: Batailly, Alain, Legrand, Mathias, Millecamps, Antoine, Cochon, Sébastien, Garcin, François

Publikováno v: Journal of Engineering for Gas Turbines and Power
Journal of Engineering for Gas Turbines and Power, American Society of Mechanical Engineers, 2014, 137 (2), pp.022502. ⟨10.1115/1.4028263⟩

International audience; Recent numerical developments dedicated to the simulation of rotor/stator interaction involving direct structural contacts have been integrated within the Snecma industrial environment. This paper presents the first attempt to

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=od_______212::422303d4da74a6af4952316133938db5
https://hal.archives-ouvertes.fr/hal-01120158/file/article_JGTP.pdf