GT2021-58742 Endwall Boundary Layer Development in a Multistage Low-Speed Compressor With Tandem Stator Vanes

GT2021-58742 Endwall Boundary Layer Development in a Multistage Low-Speed Compressor With Tandem Stator Vanes

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Veröffentlicht in:ASME Turbo Expo (2021 : Online) Proceedings of ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition ; Volume 2, A: Turbomachinery: Axial flow fan and compressor aerodynamics
1. Verfasser: Hopfinger, Michael (VerfasserIn)
Weitere Verfasser: Gümmer, Volker (VerfasserIn)
Pages:2021
Format: UnknownFormat
Sprache:eng
Veröffentlicht: 2021
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