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Measurements of a zero-pressure-gradient boundary layer blown by an asymmetric jetMeasurements were made in a two-dimensional wall jet submerged under a thick upstream boundary layer and advancing into a zero-pressure-gradient flow with the ratios of jet velocity to the freestream velocity confined to a practical range (less than 2). The effect on the flow development of an asymmetric wall-jet velocity profile with a relatively higher concentration of momentum away from the wall was investigated. The flow was computed using an existing method for blown boundary layers, and the results show good agreement with experimental data.
Document ID
19850046926
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Saripalli, K. R.
(McDonnell Douglas Research Laboratories, St. Louis, MO; Southern Methodist University Dallas, TX, United States)
Simpson, R. L.
(Virginia Polytechnic Institute and State University Blacksburg, VA; Southern Methodist University, Dallas, TX, United States)
Date Acquired
August 12, 2013
Publication Date
April 1, 1985
Publication Information
Publication: AIAA Journal
Volume: 23
ISSN: 0001-1452
Subject Category
Aerodynamics
Accession Number
85A29077
Funding Number(s)
CONTRACT_GRANT: NSG-1548
Distribution Limits
Public
Copyright
Other

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