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Keywords: shrouded stator
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Proceedings Papers

Proc. ASME. GT2022, Volume 10A: Turbomachinery — Axial Flow Fan and Compressor Aerodynamics, V10AT29A018, June 13–17, 2022
Paper No: GT2022-81904
... Abstract In axial compressor, the leakage flow from labyrinth cavity has a non-negligible influence on the aerodynamic performance and flow fields of shrouded stators due to its interaction with the main stream. A number of numerical researches have been carried out to predict and understand...
Proceedings Papers

Proc. ASME. GT2021, Volume 2A: Turbomachinery — Axial Flow Fan and Compressor Aerodynamics, V02AT31A041, June 7–11, 2021
Paper No: GT2021-60103
... Proceedings of ASME Turbo Expo 2021 Turbomachinery Technical Conference and Exposition1 GT2021 June 7-11, 2021, Virtual, Online1 GT2021-60103 DETAILS OF SHROUDED STATOR HUB CAVITY FLOW IN A MULTI-STAGE AXIAL COMPRESSOR PART 1: INTERACTIONS WITH THE PRIMARY FLOW Nitya Kamdar, Fangyuan Lou...
Proceedings Papers

Proc. ASME. GT2021, Volume 2A: Turbomachinery — Axial Flow Fan and Compressor Aerodynamics, V02AT31A042, June 7–11, 2021
Paper No: GT2021-60115
... Proceedings of ASME Turbo Expo 2021 Turbomachinery Technical Conference and Exposition GT2021 June 7-11, 2021, Virtual, Online GT2021-60115 DETAILS OF SHROUDED STATOR HUB CAVITY FLOW IN A MULTI-STAGE AXIAL COMPRESSOR PART 2: LEAKAGE FLOW CHARACTERISTICS IN STATOR WELLS Nitya Kamdar, Fangyuan Lou...
Proceedings Papers

Proc. ASME. GT2020, Volume 2A: Turbomachinery, V02AT32A036, September 21–25, 2020
Paper No: GT2020-14908
...NUMERICAL CHARACTERIZATION OF A HP COMPRESSOR STAGE EQUIPPED WITH A CLOSED SHROUDED STATOR CAVITY Cedric Babin von Karman Institute for Fluid Dynamics Rhode-St-Genèse, Belgium Michel Dumas Safran Aircraft Engines Moissy-Cramayel, France Xavier Ottavy Laboratoire de Mécanique des Fluides et d...
Proceedings Papers

Proc. ASME. GT2010, Volume 7: Turbomachinery, Parts A, B, and C, 75-85, June 14–18, 2010
Paper No: GT2010-22106
... 11 01 2011 This paper presents measurements conducted at a 4-stage low speed axial research compressor with cantilevered and shrouded stator vanes. The aim of the work is to compare these two design philosophies under rear stage conditions. To achieve blockage levels typical for rear...