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Pressure and velocity measurements in a three-dimensional wall jetThe effects on the flow fields of varying the ratio of the velocity at the exit plane of the nozzle to the outer tunnel flow are reported. The pressure-velocity correlations are taken and some trends are discussed. Emphasis is placed on comparing the coherence between the fluctuating pressure and velocity fields at various locations in the different flow configurations.
Document ID
19800001887
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Catalano, G. D. (Air Force Flight Dynamics Lab. Wright-Patterson AFB, OH, United States)
Morton, J. B. (Virginia Univ.)
Humpris, R. R. (Virginia Univ.)
Date Acquired
August 10, 2013
Publication Date
September 1, 1979
Publication Information
Publication: NASA. Ames Res. Center Workshop on Thrust Augmenting Ejectors
Subject Category
Aerodynamics
Meeting Information
Meeting: AIAA 17th Aerospace Sciences Meeting
Location: New Orleans
Start Date: January 15, 1979
End Date: January 17, 1979
Accession Number
80N10126
Funding Number(s)
CONTRACT_GRANT: NSF 75-22488
CONTRACT_GRANT: NGR-47-005-219
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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