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Random Micron Surface Roughness Effects on Swept Wing Boundary Layer Transition
Document ID
20240010642
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Jenna Eppink
(Langley Research Center Hampton, United States)
Date Acquired
August 16, 2024
Subject Category
Aerodynamics
Meeting Information
Meeting: IUTAM Symposium on Laminar-Turbulent Transition
Location: Nagano
Country: JP
Start Date: September 2, 2024
End Date: September 6, 2024
Sponsors: International Union of Theoretical and Applied Mechanics
Funding Number(s)
WBS: 109492.02.07.05.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
surface roughness
boundary layer transition
stationary crossflow
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