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Acoustic Results of Over the Rotor and Soft Vane Treatments on the Source Diagnostic Test Model in the NASA Glenn Research Center 9- by 15-foot Low-Speed Wind TunnelTwo novel fan noise reduction concepts were tested using the Source Diagnostic Test fan stage model in the NASA Glenn 9x15 Low Speed Wind Tunnel. One, referred to as over the rotor treatment, consisted of a number of different casing treatments some of which contained acoustic treatment. The other, known as soft vane, consisted of fan exit guide vanes whose interior volume contained acoustic treatment that was exposed to the vane suction side surface through a perforate.
Document ID
20230012371
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
David M Elliott
(Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
August 21, 2023
Publication Date
October 1, 2023
Subject Category
Acoustics
Report/Patent Number
E-20155
NASA/TM-20230012371
Funding Number(s)
WBS: 081876.02.03.50.10.02.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Aeroacoustics
Fan Noise
Acoustic Treatment
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