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Authors
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Funding
Funding for this research was provided by:
Bayerische Staatsministerium für Wirtschaft, Landesentwicklung und Energie (LABAY109C)
Technische Universität München
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Article History
Received: 19 August 2022
Revised: 23 January 2023
Accepted: 30 January 2023
First Online: 16 March 2023
Declarations
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: The authors declare that they have no conflict of interest.
: The implementation of the low-fidelity modeling methods is described in detail and the associated Python code can be obtained from the corresponding author on reasonable request. For the purpose of a realistic industrial application, the compressor blade optimization was performed in the design environment of <i>MTU Aero Engines</i> and is therefore unfortunately subject to strict confidentiality. Different simulation models and software may produce different results, but should yield similar trends.
