Non-linear Identification Applied to Broadband Turbomachinery Noise
Author:
Affiliation:
1. Triinity College Dublin
2. Trinity College Dublin
3. German Aerospace Center (DLR)
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-3805
Reference21 articles.
1. 1Karchmer, A. M. and Reshotko, M. "Core noise source diagnostics on a turbofan engine using correlation and coherence techniques," Tech. Rep. TM X-73535, NASA, 1976.
2. 3Reshotko, M. and Karchmer, A. M. "Core noise measurements from a small general aviation turbofan engine," Tech. Rep. TM81610, NASA, 1980.
3. 5Karchmer, A. M. "Conditioned pressure spectra and coherence measurements in the core of a turbofan engine," Tech. Rep. TM82688, NASA,1981, AIAA Paper81-2052.
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