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Exit Boundary Layer Data for Three Rectangular Nozzles at High Subsonic Mach NumbersExit boundary layer characteristics were measured for three rectangular nozzles to aid numerical simulations. These results are summarized in this presentation.
Document ID
20220008149
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Khairul Zaman (Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
May 24, 2022
Subject Category
Aerodynamics
Meeting Information
Meeting: TTT Monthly Status Meeting
Location: Cleveland, Ohio
Country: US
Start Date: May 3, 2022
Sponsors: Glenn Research Center
Funding Number(s)
WBS: 109492.02.03.09.01.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
Jets
Plume development
Aeroacoustics
Jet noise

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