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W-8 Acoustic Casing Treatment Test OverviewDuring February 2017, aerodynamic and acoustic testing was performed on a scale-model high bypass ratio turbofan rotor, R4, in an internal flow component test facility. An overview of the testing completed is presented.
Document ID
20170005682
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Bozak, Rick (NASA Glenn Research Center Cleveland, OH United States)
Podboy, Gary (NASA Glenn Research Center Cleveland, OH United States)
Dougherty, Robert (Optinav, Inc. Bellevue, WA, United States)
Date Acquired
June 21, 2017
Publication Date
April 11, 2017
Subject Category
Acoustics
Aerodynamics
Report/Patent Number
GRC-E-DAA-TN41420
Report Number: GRC-E-DAA-TN41420
Meeting Information
Meeting: Acoustics Technical Working Group (ATWG) Meeting
Location: Hampton, VA
Country: United States
Start Date: April 11, 2017
End Date: April 12, 2017
Funding Number(s)
WBS: WBS 08176.02.03.50.03.06
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Propulsion
Aeroacoustics
Acoustics

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