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Investigation of blown boundary layers with an improved wall jet systemMeasurements were made in a two dimensional incompressible wall jet submerged under a thick upstream boundary layer with a zero pressure gradient and an adverse pressure gradient. The measurements included mean velocity and Reynolds stresses profiles, skin friction, and turbulence spectra. The measurements were confined to practical ratios (less than 2) of the jet velocity to the free stream velocity. The wall jet used in the experiments had an asymmetric velocity profile with a relatively higher concentration of momentum away from the wall. An asymmetric jet velocity profile has distinct advantages over a uniform jet velocity profile, especially in the control of separation. Predictions were made using Irwin's (1974) method for blown boundary layers. The predictions clearly show the difference in flow development between an asymmetric jet velocity profile and a uniform jet velocity profile.
Document ID
19810003849
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
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
November 1, 1980
Publication Information
Publisher: NASA
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-3340
Report Number: NASA-CR-3340
Accession Number
81N12360
Funding Number(s)
CONTRACT_GRANT: NSG-1548
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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