Parametric Study of Injection Angle Effects on Stability Enhancement of Transonic Axial Compressors
Author:
Affiliation:
1. Amirkabir University of Technology, 15875-4413 Tehran, Iran
2. Cranfield University, Cranfield, England MK43 0AL, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.34817
Reference39 articles.
1. Short Length-Scale Rotating Stall Inception in a Transonic Axial Compressor: Criteria and Mechanisms
2. Breakdown of Tip Leakage Vortices in Compressors at Flow Conditions Close to Stall
3. Experimental and Computational Investigation of the Tip Clearance Flow in a Transonic Axial Compressor Rotor
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