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Optimization-Driven Synthetic Data Generation for Surrogate Models with Cross-Domain Application: A Concept Study with Compressor Blade Fillets

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/
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:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Forsthofer, NicolaiUNSPECIFIEDhttps://orcid.org/0009-0007-0230-2079173629694
Schmeink, JensUNSPECIFIEDhttps://orcid.org/0000-0001-8782-4931UNSPECIFIED
Siggel, MartinUNSPECIFIEDhttps://orcid.org/0000-0002-3952-4659UNSPECIFIED
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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