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Evaluation of the Langley 4- by 7-meter tunnel for propeller noise measurementsAn experimental and theoretical evaluation of the Langley 4- by 7- Meter Tunnel was conducted to determine its suitability for obtaining propeller noise data. The tunnel circuit and open test section are described. An experimental evaluation is performed using microphones placed in and on the tunnel floor. The reflection characteristics and background noise are determined. The predicted source (propeller) near-field/far-field boundary is given using a first-principles method. The effect of the tunnel-floor boundry layer on the noise from the propeller is also predicted. A propeller test stand used for part of his evaluation is also described. The measured propeller performance characteristics are compared with those obtained at a larger scale, and the effect of the test-section configuration on the propeller performance is examined. Finally, propeller noise measurements were obtained on an eight-bladed SR-2 propeller operating at angles of attack -8 deg, 0 deg, and 4.6 deg to give an indication of attainable signal-to-noise ratios.
Document ID
19850005244
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Block, P. J. W.
(NASA Langley Research Center Hampton, VA, United States)
Gentry, G. L., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
December 1, 1984
Subject Category
Acoustics
Report/Patent Number
L-15738
NAS 1.15:85721
NASA-TM-85721
Report Number: L-15738
Report Number: NAS 1.15:85721
Report Number: NASA-TM-85721
Accession Number
85N13553
Funding Number(s)
PROJECT: RTOP 535-03-12-08
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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