1-4 of 4
Keywords: shrouded stator
Close
Follow your search
Access your saved searches in your account

Would you like to receive an alert when new items match your search?
Close Modal
Sort by
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
...Abstract Abstract The flow in shrouded stator cavities can be quite complex with axial, radial, and circumferential variations. As the leakage flow recirculates and is re-injected into the main flow path upstream of the stator, it deteriorates the near-hub flow field and, thus, degrades...
Proceedings Papers

Proc. ASME. GT2020, Volume 2A: Turbomachinery, V02AT32A036, September 21–25, 2020
Paper No: GT2020-14908
...Abstract Abstract In axial compressors, shrouded stator cavity flows are responsible for performance degradation due to their interaction with the power stream. The present paper aims at exploring the possibility of employing a single stage high pressure axial compressor as a test vehicle...
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...