Source Separation from Multiple Microphone Measurements in the Far Field of a Full Scale Aero Engine
Author:
Affiliation:
1. Honeywell Aerospace
2. Georgia Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-2809
Reference5 articles.
1. Rejection of flow noise using a coherence function method
2. Hsu, J. S. and Ahuja, K. K. "A Coherence-Based Technique to Separate Ejector Internal Mixing Noise from Farfield Measurements,"Proceedingsofthe4th AIAA/CEASAeroacousticsConference,June2-4,1998.
3. Aligned and Unaligned Coherence: A New Diagnostic Tool
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