Bandwidth Attenuation with a Folded Cavity Liner in a Circular Flow Duct
Author:
Affiliation:
1. Boeing Military Airplane Company, Wichita, Kansas
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.50818
Reference15 articles.
1. Acoustics of Aircraft Engine-Duct Systems
2. Analytical and experimental studies of folded cavity duct acoustic liners
3. A finite element method for damped acoustic systems: An application to evaluate the performance of reactive mufflers
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