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Pressure probe and hot-film probe rsponses to acoustic excitation in mean flowAn experiment was conducted to compare the relative responses of a hot-film probe and a pressure probe positioned in a flow duct carrying mean flow and progressive acoustic waves. The response of each probe was compared with that of a condenser-type microphone flush mounted in the duct wall for flow Mach numbers up to about 0.5. The response of the pressure probe was less than that of the flush-mounted microphone by not more than about 2.1 dB at the highest centerline Mach number. This decreased response of the probe can likely be attributed to flow-induced impedance changes at the probe sensor orifices. The response of the hot-film probe, expressed in terms of fluctuating pressure, was greater than that of the flush-mounted microphone by as much as 6.0 dB at the two higher centerline Mach numbers. Removal of the contribution from fluctuating temperature in the hot-film analytical model greatly improved the agreement between the two transducer responses.
Document ID
19860017571
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Parrott, T. L.
(NASA Langley Research Center Hampton, VA, United States)
Jones, M. G.
(PRC Kentron, Inc. Hampton, Va., United States)
Date Acquired
September 5, 2013
Publication Date
June 1, 1986
Subject Category
Acoustics
Report/Patent Number
L-16079
NAS 1.60:2581
NASA-TP-2581
Report Number: L-16079
Report Number: NAS 1.60:2581
Report Number: NASA-TP-2581
Accession Number
86N27043
Funding Number(s)
PROJECT: RTOP 505-31-33-13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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