Effects of casing treatment on behavior of tip leakage flow in an isolated axial compressor rotor blade row
Author:
Publisher
Informa UK Limited
Subject
General Engineering
Link
http://www.tandfonline.com/doi/pdf/10.1080/02533839.2012.747058
Reference24 articles.
1. Bae, J and Breuer, KS. 2004. Periodic unsteadiness of compressor tip clearance vortex.ASME Turbo Expo 2004, GT 2004-53015
2. Flow in a Centrifugal Pump Impeller at Design and Off-Design Conditions—Part II: Large Eddy Simulations
3. Time Resolved Experimental Investigations of an Axial Compressor With Casing Treatment
4. Unsteady tip clearance flow pattern in an isolated axial compressor rotor with micro tip injection
5. Circumferential propagation of tip leakage flow unsteadiness for a low-speed axial compressor
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1. Axial transonic compressor performance enhancement with circumferential grooves;MECH SCI;2020
2. Performance improvement of axial compressor by introduction of circumferential grooves;Energy Sources, Part A: Recovery, Utilization, and Environmental Effects;2020-04-27
3. Numerical study of the effect of the tip gap size and using a single circumferential groove on the performance of a multistage compressor;J COMPUT APPL MECH;2019
4. Stall margin improvement of a centrifugal compressor utilizing various stepped tip gap configurations;Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy;2014-06-26
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