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Sound separation probes for flowing duct noise measurementsIn order to understand the propagation of broadband sound from a device such as a jet engine, it is necessary to make fluctuating pressure measurements in the ducted airstream. However, in a flowing duct, fluctuating pressure energy can be due to both turbulence and sound travelling in the duct. By using the principal that sound waves and turbulent flow pressure perturbations travel at different velocities, a probe has been developed that provides the data necessary to separate the energy due to sound from that due to turbulence. A mini-computer based FFT analysis of the probe measurements provides the overall level of the broadband sound in the duct as well as the spectral distribution of the sound energy.
Document ID
19780033487
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Moore, M. T.
(General Electric Co., Aircraft Engine Group, Cincinnati Ohio, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1977
Subject Category
Aircraft Propulsion And Power
Meeting Information
Meeting: International Instrumentation Symposium
Location: Las Vegas, NV
Start Date: May 1, 1977
End Date: May 5, 1977
Accession Number
78A17396
Funding Number(s)
CONTRACT_GRANT: NAS3-18021
Distribution Limits
Public
Copyright
Other

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