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Induced velocity field of a jet in a crossflowAn experimental investigation of a subsonic round jet exhausting perpendicularly from a flat plate into a subsonic crosswind of the same temperature was conducted. Velocity and pressure measurements were made in planes perpendicular to the path of the jet for ratios of jet velocity to crossflow velocity ranging from 3 to 10. The results of these measurements are presented in tabular and graphical forms. A pair of diffuse contrarotating vortices is identified as a significant feature of the flow, and the characteristics of the vortices are discussed.
Document ID
19780018449
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Fearn, R. L. (Florida Univ. Gainesville, United States)
Weston, R. P. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1978
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TP-1087
L-11624
Report Number: NASA-TP-1087
Report Number: L-11624
Accession Number
78N26392
Funding Number(s)
PROJECT: RTOP 505-11-24-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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