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Acoustic plane waves normally incident on a clamped panel in a rectangular ductThe theory of acoustic plane wave normally incident on a clamped panel in a rectangular duct is developed. The coupling theory between the elastic vibrations of the panel (plate) and the acoustic wave propagation in infinite space and in the rectangular duct is considered. The partial differential equation which governs the vibration of the panel (plate) is modified by adding to its stiffness (spring) forces and damping forces, and the fundamental resonance frequency and the attenuation factor are discussed. The noise reduction expression based on the theory is found to agree well with the corresponding experimental data of a sample aluminum panel in the mass controlled region, the damping controlled region, and the stiffness controlled region. All the frequency positions of the upward and downward resonance spikes in the sample experimental data are identified theoretically as resulting from four cross interacting major resonance phenomena: the cavity resonance, the acoustic resonance, the plate resonance, and the wooden back panel resonance.
Document ID
19790023884
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Unz, H.
(Kansas Univ. Center for Research, Inc. Lawrence, KS, United States)
Roskam, J.
(Kansas Univ. Center for Research, Inc. Lawrence, KS, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1979
Subject Category
Acoustics
Report/Patent Number
KU-FRL-417-11
NASA-CR-162278
Report Number: KU-FRL-417-11
Report Number: NASA-CR-162278
Accession Number
79N32055
Funding Number(s)
CONTRACT_GRANT: NSG-1301
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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