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Titlebook: AeroStruct: Enable and Learn How to Integrate Flexibility in Design; Contributions to the Ralf Heinrich Conference proceedings 2018 Springe

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期刊全称AeroStruct: Enable and Learn How to Integrate Flexibility in Design
期刊简称Contributions to the
影响因子2023Ralf Heinrich
视频video
发行地址Offers a timely report on simulation methods in aerospace science.Describes cutting-edge processes for multidisciplinary aircraft design and optimization.Presents a good balance of theory and practice
学科分类Notes on Numerical Fluid Mechanics and Multidisciplinary Design
图书封面Titlebook: AeroStruct: Enable and Learn How to Integrate Flexibility in Design; Contributions to the Ralf Heinrich Conference proceedings 2018 Springe
影响因子This book reports on the German research initiative AeroStruct, a three-year collaborative project between universities and the aircraft industry. It describes the development of an integrated multidisciplinary simulation environment for aircraft analysis and optimization using high-fidelity methods. This system is able to run at a high level of automatism, thus representing a step forward with respect to previous ones. Its special features are: a CAD description that is independent from the disciplines involved, an automated CFD mesh generation and an automated structure model generation including a sizing process. The book also reports on test cases by both industrial partners and DLR demonstrating the advantages of the new environment and its suitability for the industry. These results were also discussed during the AeroStruct closing Symposium, which took place on 13-14 October 2015 at the DLR in Braunschweig, Germany. The book provides expert readers with a timely report on multidisciplinary aircraft design and optimization. Thanks to a good balance between theory and practice, it is expected to address an audience of both academics and professional, and to offer them new idea
Pindex Conference proceedings 2018
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Zusammenfassung der Arbeitsergebnisseatic divergence has to be avoided by using anisotropic properties of stiffened panels made of CFRP (carbon fibre reinforced plastic). The structural design includes parametric model generation and automated sizing of composite wings. An analytical formulation of stiffened panels is used to investiga
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Bilanz der Verwaltungsreform in Deutschlandsign and optimization process. The optimization procedure is based on the Three-Columns-Concept, using a state-of the-art Finite-Element-Method (FEM) software for structural analysis purposes embedded into a multidisciplinary optimization software. The optimization model is formulated for traditiona
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Personal und Personalcontrollingol modules for considering the influence of flight control functions in preliminary aircraft design. In order to improve the methods used for the design process, an automated tool chain was set up, that builts a flight-mechanical model of the airplane, calculates controller parameters according to c
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