Performance enhancement in transonic axial compressors using blade tip injection coupled with casing treatment
Author:
Affiliation:
1. School of Mechanical Engineering, Sharif University of Technology, Tehran, Iran
2. Turbomachinery, Icing and Gas Turbine Instrumentation Group, School of Engineering, Cranfield University, Cranfield, UK
Abstract
Publisher
SAGE Publications
Subject
Mechanical Engineering,Energy Engineering and Power Technology
Link
http://journals.sagepub.com/doi/pdf/10.1243/095765005X28607
Reference9 articles.
1. Flow Phenomena in Compressor Casing Treatment
2. Compressor Stability Enhancement Using Discrete Tip Injection
3. 1997 Best Paper Award—Controls and Diagnostics Committee: Active Stabilization of Rotating Stall and Surge in a Transonic Single-Stage Axial Compressor
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1. Design optimization and flow analysis of discrete tip injection in a transonic compressor based on nonlinear harmonic method and endwall blockage attenuation;Physics of Fluids;2023-06-01
2. AERODYNAMIC PERFORMANCES OF A SINGLE-STAGE TRANSONIC AXIAL COMPRESSOR USING AN INCLINED CASING GROOVE;Australian Journal of Mechanical Engineering;2022-05-03
3. Comparative Study of Tip Injection in a Transonic and Subsonic Compressor;Journal of Turbomachinery;2021-12-24
4. Aeromechanic performance of a single-stage transonic axial compressor with recirculation-bleeding channels;Australian Journal of Mechanical Engineering;2020-10-16
5. Review of tip air injection to improve stall margin in axial compressors;Progress in Aerospace Sciences;2019-04
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