Forsthofer, Nicolai and Schmeink, Jens and 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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Abstract
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.
| Item URL in elib: | https://elib.dlr.de/209426/ | ||||||||||||||||
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| Document Type: | Conference or Workshop Item (Speech) | ||||||||||||||||
| Title: | Optimization-Driven Synthetic Data Generation for Surrogate Models with Cross-Domain Application: A Concept Study with Compressor Blade Fillets | ||||||||||||||||
| Authors: |
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| Date: | July 2024 | ||||||||||||||||
| Journal or Publication Title: | AIAA Aviation Forum and ASCEND, 2024 | ||||||||||||||||
| Refereed publication: | Yes | ||||||||||||||||
| Open Access: | No | ||||||||||||||||
| Gold Open Access: | No | ||||||||||||||||
| In SCOPUS: | Yes | ||||||||||||||||
| In ISI Web of Science: | No | ||||||||||||||||
| DOI: | 10.2514/6.2024-4303 | ||||||||||||||||
| Publisher: | American Institute of Aeronautics and Astronautics | ||||||||||||||||
| Series Name: | AIAA 2024-4303 | ||||||||||||||||
| ISBN: | 978-162410716-0 | ||||||||||||||||
| Status: | Published | ||||||||||||||||
| Keywords: | Gas Turbine, Jet Engine, Compressor, Fillets, Structural Mechanics, Optimization | ||||||||||||||||
| Event Title: | AIAA Aviation Forum and Exposition | ||||||||||||||||
| Event Location: | Las Vegas, USA | ||||||||||||||||
| Event Type: | international Conference | ||||||||||||||||
| Event Start Date: | 29 July 2024 | ||||||||||||||||
| Event End Date: | 2 August 2024 | ||||||||||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||||||||||
| HGF - Program: | Aeronautics | ||||||||||||||||
| HGF - Program Themes: | Clean Propulsion | ||||||||||||||||
| DLR - Research area: | Aeronautics | ||||||||||||||||
| DLR - Program: | L CP - Clean Propulsion | ||||||||||||||||
| DLR - Research theme (Project): | L - Virtual Engine | ||||||||||||||||
| Location: | Stuttgart | ||||||||||||||||
| Institutes and Institutions: | Institute of Structures and Design > Design and Manufacture Technologies Institute of Propulsion Technology > Engine | ||||||||||||||||
| Deposited By: | Forsthofer, Nicolai | ||||||||||||||||
| Deposited On: | 12 Dec 2024 13:21 | ||||||||||||||||
| Last Modified: | 12 Dec 2024 13:21 |
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