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Tekkaya, A. Erman |
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Förster, Peter |
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Mudimu, George T. |
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Shibata, Lillian Marie |
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Talabbeydokhti, Nasser |
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Laffite, Ernesto Dante Rodriguez |
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Schöpke, Benito |
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Gobis, Anna |
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Alfares, Hesham K. |
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Münzel, Thomas |
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Joy, Gemini Velleringatt |
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Oubahman, Laila |
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Filali, Youssef |
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Philippi, Paula |
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George, Alinda |
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Lucia, Caterina De |
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Avril, Ludovic |
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Belachew, Zigyalew Gashaw |
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Kassens-Noor, Eva | Darmstadt |
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Cho, Seongchul |
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Tonne, Cathryn |
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Hosseinlou, Farhad |
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Ganvit, Harsh |
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Schmitt, Konrad Erich Kork |
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Grimm, Daniel |
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Scherer, Julian
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Publications (10/10 displayed)
- 2023Pre-hospital and Hospital Trauma Care during the Covid-19 Lockdown – Experience in a Metropolitan European Level 1 Trauma Centrecitations
- 2023Fractures of the Lower Extremity after E-Bike, Bicycle, and Motorcycle Accidents: A Retrospective Cohort Study of 624 Patientscitations
- 2016DLR Project Digital-X: towards virtual aircraft design and flight testing based on high-fidelity methodscitations
- 2016A cooperative approach to multi-level multi-disciplinary aircraft optimization
- 2016Automated Sizing Process of a complete Aircraft Structure for the Usage within a MDO Process
- 2015A Parametrical Transport Aircraft Fuselage Model for Preliminary Sizing and Beyond
- 2014Entwicklung einer Softwareplattform für die Multidisziplinäre Optimierung eines Gesamtflugzeugs
- 2014"DLR-Projekt Digital-X" Auf dem Weg zur virtuellen Flugzeugentwicklung und Flugerprobung auf Basis höherwertiger Verfahren
- 2013A Finite Element Based Tool Chain for Structural Sizing of Transport Aircraft in Preliminary Aircraft Design
- 2013Development of a Multidisciplinary Process Chain for the Preliminary Design of Aircraft Structures
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conferencepaper
Automated Sizing Process of a complete Aircraft Structure for the Usage within a MDO Process
Abstract
The paper gives an overview of an automated sizing process of a complete aircraft structure which is part of a multidisciplinary optimization process that has been developed at the German Aerospace Center (DLR). It covers all aspects of aircraft model generation, model analysis and the implemented sizing concepts. Where the main focus concentrates on metallic based sizing within the global optimization process, an alternative composite sizing concept is also described in detail. Furthermore, exemplary results of the automated sizing process will be illustrated.
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