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Transfer-Function Determination for Infinite-Tube-Probe Pressure Transducers with Application to Turbofan Core/Combuster NoiseTurbofan hot-section unsteady pressure measurements are complicated by environmental limitations of current-generation sensors. Accurate direct measurements are normally not possible and engine-external measurement techniques, using sufficiently long sense lines, are utilized instead. Remote measurement comes at a cost, however, as it introduces a magnitude reduction within the line as well as a phase lag relative to the desired engine-internal measurement location. Determination, or validation, of a transfer function relating the engine internal pressure to the observed remote value is necessary. Transfer functions are examined for various configurations of the so-called infinite-tube-probe arrangement in order to optimize measurement performance. The experimental setup uses a normal-incidence tube that ordinarily is utilized for impedance eduction. Here, its downstream end instead is made up of a hard-wall termination instrumented with a flush-mounted microphone and a Kulite pressure transducer as well as a sense line connection. This allows the remote and direct measurements to be related under controlled conditions. Transfer-function measurements are presented and compared to predictions for several parametric variations.
Document ID
20190025927
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Boyle, Devin K.
(NASA Glenn Research Center Cleveland, OH, United States)
Henderson, Brenda S.
(NASA Glenn Research Center Cleveland, OH, United States)
Hultgren, Lennart S.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
June 14, 2019
Publication Date
June 1, 2019
Subject Category
Aircraft Propulsion And Power
Acoustics
Report/Patent Number
AIAA-2019-2588
GRC-E-DAA-TN68638
NASA/TM-2019-220245
Funding Number(s)
WBS: 081876.02.03.50.06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
Turbomachinery Noise
Aeroacoustics
Combuster Noise
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