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Modal content of noise generated by a coaxial jet in a pipeNoise generated by air flow through a coaxial obstruction in a long, straight pipe was investigated with concentration on the modal characteristics of the noise field inside the pipe and downstream of the restriction. Two measurement techniques were developed for separation of the noise into the acoustic duct modes. The instantaneous mode separation technique uses four microphones, equally spaced in the circumferential direction, at the same axial location. The time-averaged mode separation technique uses three microphones mounted at the same axial location. A matrix operation on time-averaged data produces the modal pressure levels. This technique requires the restrictive assumption that the acoustic modes are uncorrelated with each other. The measured modal pressure spectra were converted to modal power spectra and integrated over the frequency range 200-6000 Hz. The acoustic efficiency levels (acoustic power normalized by jet kinetic energy flow), when plotted vs. jet Mach number, showed a strong dependence on the ratio of restriction diameter to pipe diameter. The acoustic energy flow analyses based on the thermodynamic energy equation and on the results of Mohring both resulted in orthogonality properties for the eigenfunctions of the radial mode shape equation. These orthogonality relationships involve the eigenvalues and derivatives of the radial mode shape functions.
Document ID
19800024669
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kerschen, E. J.
(Stanford Univ. CA, United States)
Johnston, J. P.
(Stanford Univ. CA, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1978
Subject Category
Acoustics
Report/Patent Number
NASA-CR-163575
SU-JIAA-TR-11
Accession Number
80N33177
Funding Number(s)
CONTRACT_GRANT: NSF GK-37294
CONTRACT_GRANT: NSF ENG-76-00819
CONTRACT_GRANT: NSG-2007
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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