GT2022-81689 Evaluating the Aerodynamic Damping at Shock Wave Boundary Layer Interacting Flow Conditions With Harmonic Balance

GT2022-81689 Evaluating the Aerodynamic Damping at Shock Wave Boundary Layer Interacting Flow Conditions With Harmonic Balance

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Veröffentlicht in:ASME Turbo Expo (67. : 2022 : Rotterdam) Proceedings of ASME Turbo Expo 2022: Turbomachinery Technical Conference and Exposition (GT 2022) ; Volume 8, A: Structures and dynamics: Aerodynamics excitation and damping; bearing and seal dynamics; emerging methods in engineering design, analysis, and additive manufacturing; fatigue, fracture, and life prediction
1. Verfasser: Heners, Jan Philipp (VerfasserIn)
Weitere Verfasser: Carraro, Thomas (VerfasserIn), Frey, Christian (VerfasserIn), Grüber, Björn (VerfasserIn)
Pages:2022
Format: UnknownFormat
Sprache:eng
Veröffentlicht: 2022
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