Forsthofer, Nicolai und Schmeink, Jens und Siggel, Martin (2024) Optimization-Driven Synthetic Data Generation for Surrogate Models with Cross-Domain Application: A Concept Study with Compressor Blade Fillets. In: AIAA Aviation Forum and ASCEND, 2024. American Institute of Aeronautics and Astronautics. AIAA Aviation Forum and Exposition, 2024-07-29 - 2024-08-02, Las Vegas, USA. doi: 10.2514/6.2024-4303. ISBN 978-162410716-0.
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Kurzfassung
This study presents a surrogate modeling framework for the dimensioning of compressor blade components demonstrated with an application for the design of compressor blade fillets. The compressor blade, a critical component, demands a highly specialized design approach, where the fillet is of particular interest due to its impact on the part's aerodynamic and structural performance. Our research introduces a fast, robust, and reliable method that employs machine learning techniques to enhance the compressor blade fillet design process. The method extends upon a validated prototype process for compressor blisks, as outlined in previous work. Significant advancements to the prototype are achieved in two primary aspects of this process. First, enhancements to the optimization algorithm. For this task we use a specialized open-source framework for multidisciplinary design, analysis, and optimization to balance the conflicting demands of structural durability and minimizing fillet size. The second major enhancement pertains to the automation of data pipelines, covering the data generation, processing, training and validation.
elib-URL des Eintrags: | https://elib.dlr.de/209426/ | ||||||||||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||
Titel: | Optimization-Driven Synthetic Data Generation for Surrogate Models with Cross-Domain Application: A Concept Study with Compressor Blade Fillets | ||||||||||||||||
Autoren: |
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Datum: | Juli 2024 | ||||||||||||||||
Erschienen in: | AIAA Aviation Forum and ASCEND, 2024 | ||||||||||||||||
Referierte Publikation: | Ja | ||||||||||||||||
Open Access: | Nein | ||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||
In SCOPUS: | Ja | ||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||
DOI: | 10.2514/6.2024-4303 | ||||||||||||||||
Verlag: | American Institute of Aeronautics and Astronautics | ||||||||||||||||
Name der Reihe: | AIAA 2024-4303 | ||||||||||||||||
ISBN: | 978-162410716-0 | ||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||
Stichwörter: | Gas Turbine, Jet Engine, Compressor, Fillets, Structural Mechanics, Optimization | ||||||||||||||||
Veranstaltungstitel: | AIAA Aviation Forum and Exposition | ||||||||||||||||
Veranstaltungsort: | Las Vegas, USA | ||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||
Veranstaltungsbeginn: | 29 Juli 2024 | ||||||||||||||||
Veranstaltungsende: | 2 August 2024 | ||||||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||
HGF - Programm: | Luftfahrt | ||||||||||||||||
HGF - Programmthema: | Umweltschonender Antrieb | ||||||||||||||||
DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||
DLR - Forschungsgebiet: | L CP - Umweltschonender Antrieb | ||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | L - Virtuelles Triebwerk | ||||||||||||||||
Standort: | Stuttgart | ||||||||||||||||
Institute & Einrichtungen: | Institut für Bauweisen und Strukturtechnologie > Bauteilgestaltung und Fertigungstechnologien Institut für Antriebstechnik > Triebwerk | ||||||||||||||||
Hinterlegt von: | Forsthofer, Nicolai | ||||||||||||||||
Hinterlegt am: | 12 Dez 2024 13:21 | ||||||||||||||||
Letzte Änderung: | 12 Dez 2024 13:21 |
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