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Properties of a half-delta wing vortexThe mean flow and turbulence structure of a single longitudinal vortex generated by a half-delta wing placed at a small angle of attack were investigated. Particular consideration was given to the near-field properties of the generator in order to establish the role of the generator wake in the initial rolling-up of the vortex, as well as to the far-field properties so that the approach to equilibrium could be studied. Measurements were made on fine cross-plane grids at seven streamwise locations using hot cross wires. The results show that the point of maximum vorticity and the generator wake do not merge until a streamwise distance equivalent to three generator heights is reached. Comparison with previous data on vortices produced by double-branched generators confirmed that the present vortex had achieved a fully developed state, and at a relatively short streamwise distance.
Document ID
19880051758
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mehta, Rabindra D.
(Stanford University CA, United States)
Cantwell, Elizabeth R.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Aerodynamics
Accession Number
88A38985
Funding Number(s)
CONTRACT_GRANT: NCC2-294
Distribution Limits
Public
Copyright
Other

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