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Subproject C6: Aeroelasticity of Multi-Stage Axial Compressors

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Subproject C6: Aeroelasticity of Multi-Stage Axial Compressors
Alternative Title
Influence of Regeneration-Induced
Mistuning on the Aeroelasticity of
Multi-Stage Axial Compressors
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6
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CC Attribution - NonCommercial - ShareAlike 3.0 Germany:
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Abstract
The aeroelasticity of mistuned axial compressors with multiple stages is investigated. By using an improved simulation methodology, the influence of regeneration on the vibration behavior of compressor blisks is analyzed. The focus is on the structural and aerodynamic coupling of compressor blades between different stages.