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Investigation of blown boundary layers with an improved wall jet systemThe behavior of two dimensional incompressible turbulent wall jets submerged in a boundary layer when they are used to prevent boundary layer separation on plane surfaces is investigated. The experimental set-up and instrumentation are described. Experimental results of zero pressure gradient flow and adverse pressure gradient flow are presented. Conclusions are given and discussed.
Document ID
19800004749
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Saripalli, K. R.
(Southern Methodist Univ. Dallas, TX, United States)
Simpson, R. L.
(Southern Methodist Univ. Dallas, TX, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1979
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-162512
Report Number: NASA-CR-162512
Accession Number
80N13004
Funding Number(s)
CONTRACT_GRANT: NSG-1548
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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