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An analytical and experimental study of sound propagation and attenuation in variable-area ductsThe performance of sound suppression techniques in ducts that produce refraction effects due to axial velocity gradients was evaluated. A computer code based on the method of multiple scales was used to calculate the influence of axial variations due to slow changes in the cross-sectional area as well as transverse gradients due to the wall boundary layers. An attempt was made to verify the analytical model through direct comparison of experimental and computational results and the analytical determination of the influence of axial gradients on optimum liner properties. However, the analytical studies were unable to examine the influence of non-parallel ducts on the optimum linear conditions. For liner properties not close to optimum, the analytical predictions and the experimental measurements were compared. The circumferential variations of pressure amplitudes and phases at several axial positions were examined in straight and variable-area ducts, hard-wall and lined sections with and without a mean flow. Reasonable agreement between the theoretical and experimental results was obtained.
Document ID
19790017674
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Nayfeh, A. H.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Kaiser, J. E.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Marshall, R. L.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Hurst, L. J.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1978
Subject Category
Acoustics
Report/Patent Number
NASA-CR-135392
Report Number: NASA-CR-135392
Accession Number
79N25845
Funding Number(s)
CONTRACT_GRANT: NAS3-18553
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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