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The interaction between a strong longitudinal vortex and a turbulent boundary layerThis paper presents the preliminary results of a long-term investigation of the interaction of strong longitudinal vortices with turbulent boundary layers. A pair of trailing vortices is generated by a delta wing, which is mounted ahead of a flat plate so that the trailing vortices merge with the boundary layer on the upper surface of the flat plate, while the non-rolled-up part of the delta-wing wake passes below the plate. This approximates an aircraft wing with a close-coupled canard. The measurements show how the boundary-layer fluid is first subjected to large cross flow and is then transported away from the plate to circulate around the vortex core.
Document ID
19860053699
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cutler, A. D.
(Imperial Coll. of Science and Technology London, United Kingdom)
Bradshaw, P.
(Imperial College of Science and Technology London, United Kingdom)
Date Acquired
August 12, 2013
Publication Date
May 1, 1986
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 86-1071
Report Number: AIAA PAPER 86-1071
Accession Number
86A38437
Funding Number(s)
CONTRACT_GRANT: NASW-581
Distribution Limits
Public
Copyright
Other

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