المؤلفون: Johanning, Andreas^Aff8, Scholz, Dieter^Aff8

المساهمون: Chaari, Fakher, Series Editor^Aff1, Haddar, Mohamed, Series Editor^Aff2, Kwon, Young W., Series Editor^Aff3, Gherardini, Francesco, Series Editor^Aff4, Ivanov, Vitalii, Series Editor^Aff5, Bajpai, Ram P., editor^Aff6, Chandrasekhar, U., editor^Aff7

المصدر: Innovative Design and Development Practices in Aerospace and Automotive Engineering : I-DAD, February 22 - 24, 2016. :589-603

المؤلفون: Dmitry V. Vedernikov, Alexander N. Shanygin, Yury S. Mirgorodsky, Mikhail D. Levchenkov

المصدر: Aerospace, Vol 8, Iss 3, p 80 (2021)

مصطلحات موضوعية: aircraft structure, strut-braced wing, parametric modeling, decomposition principles, strength analysis, finite element method (FEM), Motor vehicles. Aeronautics. Astronautics, TL1-4050

وصف الملف: electronic resource

Relation: https://www.mdpi.com/2226-4310/8/3/80; https://doaj.org/toc/2226-4310

URL الوصول: https://doaj.org/article/eecdc444a5664927b3add4665146c57a

المؤلفون: P. Chiozzotto, Gabriel

المصدر: CEAS Aeronautical Journal: An Official Journal of the Council of European Aerospace Societies. September 2016 7(3):499-519

المؤلفون: Méheut, Michaël, Arnoult, Guillaume, Atinault, Olivier, Bennehard, Quentin, François, Christophe

المساهمون: GREC, christine

مصطلحات موضوعية: DISTRIBUTED PROPULSION, [SPI] Engineering Sciences [physics], STRUT-BRACED WING, BENDED WING BODY, AERODYNAMIC DESIGN, [MATH] Mathematics [math], [INFO] Computer Science [cs], OPTIMIZATION, [PHYS] Physics [physics]

وصف الملف: application/pdf

URL الوصول: https://explore.openaire.eu/search/publication?articleId=od_______166::760be876df1bfa24640e9a8a4b1b4d8a
https://hal.archives-ouvertes.fr/hal-03771567

المؤلفون: Gerald G. Carrier, Guillaume Arnoult, Nicolo Fabbiane, Jean-Sebastien Schotte, Christophe David, Sébastien Defoort, Emmanuel Benard, Martin Delavenne

المساهمون: André, Cécile

المصدر: AIAA SCITECH 2022 Forum

مصطلحات موضوعية: AIRCRAFT DESIGN, STRUCTURES, [SPI] Engineering Sciences [physics], STRUT-BRACED WING, Aile haubanée, Conception avion, Structure, AERODYNAMICS, CONCEPTUAL, Aérodynamique, [PHYS] Physics [physics]

وصف الملف: application/pdf

URL الوصول: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::339c72bf5319acb92527ec4a337aecc6

المؤلفون: Pareja González, Irene

مصطلحات موضوعية: Finite Element Model, Diseño estructural y optimización, Structural Design and Optimization, Máster Universitario en Ingeniería Aeronáutica-Màster Universitari en Enginyeria Aeronàutica, Ala reforzada con puntal, Modelo de elementos finitos, INGENIERIA AEROESPACIAL, High-Fidelity Structural Model, Modelo estructural de alta fidelidad, Strut-Braced Wing

وصف الملف: application/pdf

URL الوصول: https://explore.openaire.eu/search/publication?articleId=od______1560::e6a1fb6329d12b743309cd851160cef2
https://hdl.handle.net/10251/178361

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المؤلفون: Iwanizki, Michael, Wöhler, Sebastian, Fröhler, Benjamin, Zill, Thomas, Méheut, Michaël, Defoort, Sébastien, Carini, Marco, Gauvrit-Ledogar, Julie, Liaboeuf, Romain, Tremolet, Arnault, Paluch, Bernard, Kanellopoulos, Stylianos

المساهمون: Deutsches Zentrum für Luft- und Raumfahrt [Braunschweig] (DLR), Deutsches Zentrum für Luft- und Raumfahrt (DLR), DAAA, ONERA, Université Paris Saclay [Meudon], ONERA-Université Paris-Saclay, ONERA / DTIS, Université de Toulouse [Toulouse], ONERA-PRES Université de Toulouse, DTIS, ONERA, Université Paris Saclay [Palaiseau], DMAS, ONERA [Lille], ONERA

المصدر: 3AF Aerospace Europe Conference 2020
3AF Aerospace Europe Conference 2020, Feb 2020, BORDEAUX, France

مصطلحات موضوعية: Large Fuselage, TAILESS AIRCRAFT, Blended Wing Body, JOINDED WING, AILE HAUBANEE, AVION SANS EMPENNAGE, CONCEPTION AVANT-PROJET, Forward Swept Wing, [SPI]Engineering Sciences [physics], AILE JOINTIVE, Clean Sky 2, AILE A FLECHE INVERSE, 3-Surfaces, [PHYS]Physics [physics], ETUDE CONCEPTUELLE, AILE VOLANTE, Overall Aircraft Design, MICADO, RCE, Strut Braced Wing, Conceptual Design, FUSELAGE LARGE, Tailless Aircraft, 3 SURFACES, ANALYSE DE PERFORMANCE, Performance Analysis, CPACS, MYSTIC, Joined Wing

URL الوصول: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::c66843bf65520665caa9ce8493df56ad
https://elib.dlr.de/136281/

مصطلحات موضوعية: Structural Optimization, Strut Braced Wing, Aeroelasticity, Fatigue Loads, Gust loads

URL الوصول: https://explore.openaire.eu/search/publication?articleId=dris___00893::9744d1f94d0ded7f832cd175f78ba1c8
http://resolver.tudelft.nl/uuid:90c40daf-d41d-4931-a4ac-3d7ea4b90476