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Calibration of the Ames Anechoic Facility. Phase 1: Short range planA calibration was made of the acoustic and aerodynamic characteristics of a small, open-jet wind tunnel in an anechoic room. The jet nozzle was 102 mm diameter and was operated subsonically. The anechoic-room dimensions were 7.6 m by 5.5 m by 3.4 m high (wedge tip to wedge tip). Noise contours in the chamber were determined by various jet speeds and exhaust collector positions. The optimum nozzle/collector separation from an acoustic standpoint was 2.1 m. Jet velocity profiles and turbulence levels were measured using pressure probes and hot wires. The jet was found to be symmetric, with no unusual characteristics. The turbulence measurements were hampered by oil mist contamination of the airflow.
Document ID
19820008218
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Hickey, D.
(NASA Ames Research Center Moffett Field, CA, United States)
Soderman, P. T.
(NASA Ames Research Center Moffett Field, CA, United States)
Karamcheti, K.
(NASA Ames Research Center Moffett Field, CA, United States)
Koutsoyannis, S. P.
(NASA Ames Research Center Moffett Field, CA, United States)
Hopkins, R.
(NASA Ames Research Center Moffett Field, CA, United States)
Mclachlan, B.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1980
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-TM-84081
Accession Number
82N16091
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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