Response Surface Method Optimization of Uniform and Axially Segmented Duct Acoustics Liners
Author:
Affiliation:
1. University of Southampton, Highfield, England SO17 1BJ, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.17727
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1. Noise due to interaction of inlet turbulence with isolated stators and rotors
2. Noise generation by the interaction between ingested turbulence and a rotating fan
3. Broadband Self-Noise from a Ducted Fan
4. AEROACOUSTICS RESEARCH IN EUROPE: THE CEAS-ASC REPORT ON 2001 HIGHLIGHTS
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