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Transitional Flow in the Wake of a Pseudorandom Roughness on a Supersonic Flat PlatePrediction of roughness-induced transition is a practical requirement for the optimized design of high-speed vehicles, which rely on a reduction of thermal stresses and drag for higher performance. This reduction is affected by boundary layer transition, which on real vehicles may be caused by unavoidable roughness such as inherent surface material roughness and deterioration or roughness in the form of sensing elements, fasteners, etc. A better understanding of transition resulting from roughness can help inform acceptable manufacturing tolerances or maintenance requirements on real vehicles.
Document ID
20240006013
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Amanda Chou
(Langley Research Center Hampton, Virginia, United States)
Andrew N Leidy
(Langley Research Center Hampton, Virginia, United States)
Michael A Kegerise
(Langley Research Center Hampton, Virginia, United States)
Rudolph A King
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
May 13, 2024
Publication Date
June 1, 2024
Subject Category
Fluid Mechanics and Thermodynamics
Funding Number(s)
WBS: 109492.02.07.05.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Peer Committee
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