Výsledky vyhledávání - "Retho, Fabien"

Dissertation/ Thesis

Méthodologie collaborative d'aide à la construction de produits virtuels pour la conception d'aéronefs à propulsion électrique.

Autor: Retho, Fabien

La recherche de moyens alternatifs pour la propulsion d'un aéronef est primordiale tant la dépendance au pétrole est forte. Le travail proposé dans cette thèse s'inscrit dans le besoin de soutenir les concepteurs de systèmes de propulsion innov

Externí odkaz: http://www.theses.fr/2015CSUP0010/document

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Multidisciplinary Simulation Model Development: Early inconsistency detection during the design stage

Autor: Sirin, Göknur, Retho, Fabien, YANNOU, Bernard, Callot, Martine, Dessante, Philippe, Landel, Eric

Publikováno v: Advances in Engineering Software
Advances in Engineering Software, inPress
Advances in Engineering Software, Elsevier, In press

International audience; Integration, Verification and Validation (IVV) practices in simulation-based design helps reduce inconsistencies in multidisciplinary systems, i.e. those combining multiple mechanics, structural, hydrodynamic or other complex

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::e10931d0bb4648ae71843c3c633d79e7
https://hal.science/hal-01673538

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Collaborative methodology for virtual product building to support aerial vehicles with electrical propulsion design

Autor: Retho, Fabien

Publikováno v: Autre. CentraleSupélec, 2015. Français. ⟨NNT : 2015CSUP0010⟩

The research of alternative aircraft propulsion system is mandatory because oil dependence is too strong. The work proposed in this thesis is oriented to support electric based innovative propulsion system designers. Considering that it is important

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::057c9b39b13ccb1cb827c6e896a65704
https://tel.archives-ouvertes.fr/tel-01323018/file/Retho_Manuscrit_PhD.pdf

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Model of Intention: A concept to support models building in a complex system design project

Autor: Retho, Fabien, Smaoui, Hichem, Vannier, Jean-Claude, Dessante, Philippe

A hybrid propulsion system for aircraft application represents a new paradigm for propulsionsystems designers. Several new problems appear, and classical design methods must be challenged.Indeed, addition of new systems and new components inside the

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::47afbc0fefb8a8b364d402094b40cd80
https://hal.science/hal-02272375

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