Pressure and velocity fluctuations characteristics of the tip clearance flow in an axial compressor stage at the near-stall condition
Author:
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference45 articles.
1. Tip Leakage Flow in Axial Compressors;Storer,1991
2. Analysis of tip-leakage flow in an axial fan at varying tip-gap sizes and operating conditions;Moghadam;Comput. Fluids,2019
3. Interaction mechanisms between tip leakage flow and the passage vortex in a linear turbine rotor cascade;Yamamoto;J. Turbomach.,1988
4. The role of tip leakage flow in spike-type rotating stall inception;Hewkin-Smith,2017
5. Squealer tip leakage flow characteristics in transonic condition;Li;J. Eng. Gas Turbines Power,2014
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1. Effect of Tip Gap Size on the Tip Flow Structure and Turbulence Generation in a Low Reynolds Number Compressor Cascade;Journal of Fluids Engineering;2024-05-03
2. Diagnosis of unsteady disturbance characteristics induced by the tip leakage vortex in a compressor based on data-driven modal decomposition methods;Physics of Fluids;2024-05-01
3. Spatiotemporal characteristics of rotating stall in a centrifugal compressor with a volute at low-flow rate conditions;Physics of Fluids;2024-03-01
4. Axial clearance measurement method based on wavelength division multiplexing with all-fiber microwave photonic mixing;Optics Express;2024-01-17
5. Role of wall roughness on interaction of leakage flow and main flow in a mixed flow pump with tip clearance;Physics of Fluids;2024-01-01
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