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Transitional Boundary Layers Under the Influence of High Free Stream Turbulence, Intensive Wall Cooling and High Pressure Gradients in Hot Gas CirculationThe requirements for fundamental experimental studies of the influence of free stream turbulence, pressure gradients and wall cooling are discussed. Under turbine-like free stream conditions, comprehensive tests of transitional boundary layers with laminar, reversing and turbulent flow increments were performed to decouple the effects of the parameters and to determine the effects during mutual interaction.
Document ID
19870007550
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Rued, Klaus (NASA Headquarters Washington, DC United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1987
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-88524
NAS 1.15:88524
Accession Number
87N16983
Funding Number(s)
CONTRACT_GRANT: NASW-4004
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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