A unique ducted fan test bed for active noise control and aeroacoustics research
Author:
Affiliation:
1. NASA, Lewis Research Center, Cleveland, OH
2. NYMA, Inc., Brook Park, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-1740
Reference37 articles.
1. Traversing Microphone System for Mode Measurement",NASA CR-168040,Nov 1982.
2. Inlet acoustic mode measurements using a continuously rotating rake
3. Hall, D. and Bridges,J. "ASophisticated, Multi-ChannelData Acquisition and Processing System forHigh FrequencyNoiseResearch". NASA CR-189137. March 1992.
4. Homyak, L., McArdle, J. and Heidelberg, L. "ACompactInflow Cont ol Device f or Simulating Flight Fan Noise". NASA TM-83349. April 1983.
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