Wavelet Analysis of Rotor-Tip Disturbances in an Axial-Flow Compressor
Author:
Affiliation:
1. Indiana Institute of Technology, Fort Wayne, Indiana 46803
2. Chinese Academy of Sciences, 100080 Beijing, People’s Republic of China
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/10.2514/1.9257
Reference16 articles.
1. Rotating Waves as a Stall inception Indication in Axial Compressors
2. Stall Inception in Axial Flow Compressors
3. 1997 Best Paper Award—Turbomachinery Committee: A Study of Spike and Modal Stall Phenomena in a Low-Speed Axial Compressor
4. Role of Blade Passage Flow Structurs in Axial Compressor Rotating Stall Inception
5. A Computational Model for Short-Wavelength Stall Inception and Development in Multistage Compressors
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