The Influence of Tip Clearance Momentum Flux on Stall Inception in a High-Speed Axial Compressor
Author:
Affiliation:
1. e-mail: Hessert Laboratory, Department of Mechanical and Aerospace Engineering, University of Notre Dame, Notre Dame, IN 46556
2. Institute of Engineering Thermophysics, Chinese Academy of Science, Beijing 100190, China
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.4007800/6296003/turb_135_05_051005.pdf
Reference15 articles.
1. Spike-Type Compressor Stall Inception, Detection and Control;Annu. Rev. Fluid Mech.,2010
2. Criteria for Spike Initiated Rotating Stall;ASME J. Turbomach.,2008
3. Tip Clearance Flow Induced Endwall Boundary Layer Separation in a Single Stage Axial-Flow Low-Speed Compressor,2000
4. Investigation of Tip-Flow Based Stall Criteria Using Rotor Casing Visualization,2008
5. Pre-stall Behavior of a Transonic Axial Compressor Stage Via Time-Accurate Numerical Simulation,2007
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