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Noise radiation directivity from a wind-tunnel inlet with inlet vanes and duct wall liningsThe acoustic radiation patterns from a 1/15th scale model of the Ames 80- by 120-Ft Wind Tunnel test section and inlet have been measured with a noise source installed in the test section. Data were acquired without airflow in the duct. Sound-absorbent inlet vanes oriented parallel to each other, or splayed with a variable incidence relative to the duct long axis, were evaluated along with duct wall linings. Results show that splayed vans tend to spread the sound to greater angles than those measured with the open inlet. Parallel vanes narrowed the high-frequency radiation pattern. Duct wall linings had a strong effect on acoustic directivity by attenuating wall reflections. Vane insertion loss was measured. Directivity results are compared with existing data from square ducts. Two prediction methods for duct radiation directivity are described: one is an empirical method based on the test data, and the other is a analytical method based on ray acoustics.
Document ID
19860060768
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Soderman, P. T.
(NASA Ames Research Center Moffett Field, CA, United States)
Phillips, J. D.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 12, 2013
Publication Date
July 1, 1986
Subject Category
Acoustics
Report/Patent Number
AIAA PAPER 86-1896
Accession Number
86A45506
Distribution Limits
Public
Copyright
Other

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