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CST Inlet Treatment ModelingModeling of varying liner properties in Actran through the use of the Grazing Flow Impedance Tube (GFIT) geometry.
Document ID
20210012676
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Aikaterini Stylianides (Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
March 29, 2021
Subject Category
Aeronautics (General)
Meeting Information
Meeting: Spring 2021 NASA Acoustics Technical Working Group
Location: Virtual
Country: US
Start Date: April 13, 2021
End Date: April 15, 2021
Sponsors: National Aeronautics and Space Administration
Funding Number(s)
WBS: 110076.02.03.04.40.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
supersonic, acoustics, inlet

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