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Breaking down the delta wing vortex: The role of vorticity in the breakdown processExperimental x-wire measurements of the flowfield above a 70 degree and 75 degree flat plate delta wing were performed at a Reynolds number of 250,000. Grids were taken normal to the wing at various chordwise locations for angles of attack of 20 degrees and 30 degrees. Axial and azimuthal vorticity distributions were derived from the velocity fields. The dependence of circulation on distance from the vortex core and on chordwise location was also examined. The effects of nondimensionalization in comparison with other experimental data is made. The results indicate that the circulation distribution scales with the local semispan and grows in a nearly linear fashion in the chordwise direction. The spanwise distribution of axial vorticity is severely altered through the breakdown region and the amount of vorticity present appears to reach a maximum immediately preceding breakdown. The axial velocity components with a negative sense, such as that found in the secondary vortex, seem to remain unaffected by changes in wing sweep or angle of attack, in direct contrast to the visible components. In addition, the inclusion of the local wing geometry into a previously derived correlation parameter allows the circulation of growing leading edge vortex flows to be reduced to a single curve.
Document ID
Document Type
Conference Paper
Nelson, R. C.
(Notre Dame Univ. IN, United States)
Visser, Kenneth Dale
(Notre Dame Univ. IN, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1991
Publication Information
Publication: AGARD, Vortex Flow Aerodynamics
Subject Category
Accession Number
Funding Number(s)
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