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Drive Rig Mufflers for Model Scale Engine Acoustic TestingTesting of air breathing propulsion systems in the 9x15 foot wind tunnel at NASA Glenn Research Center depends on compressed air turbines for power. The drive rig turbines exhaust directly to the wind tunnel test section, and have been found to produce significant unwanted noise that reduces the quality of the acoustic measurements of the model being tested. In order to mitigate this acoustic contamination, a muffler can be attached downstream of the drive rig turbine. The modern engine designs currently being tested produce much less noise than traditional engines, and consequently a lower noise floor is required of the facility. An acoustic test of a muffler designed to mitigate this extraneous noise is presented, and a noise reduction of 8 dB between 700 Hz and 20 kHz was documented, significantly improving the quality of acoustic measurements in the facility.
Document ID
20100042194
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Stephens, David
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
October 21, 2010
Subject Category
Acoustics
Report/Patent Number
E-17577
Report Number: E-17577
Meeting Information
Meeting: Acoustic Technical Working Group Meeting
Location: Hampton, VA
Country: United States
Start Date: October 21, 2010
End Date: October 22, 2010
Funding Number(s)
WBS: WBS 699969.02,09.03.05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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