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Vortex interaction with a leading-edge of finite thicknessVortex interaction with a thick elliptical leading-edge at zero relative offset produces a pronounced secondary vortes of opposite sense that travels with the same phase speed as the primaty vortex along the lower surface of the edge. The edge thickness (scale) relative to the incident vorticity field has a strong effect on the distortion of the incident primary vortex during the impingement processs. When the thickness is sufficiently small, there is a definite severing of the incident vortex and the portion of the incident vortex that travels along the upper part of the elliptical surface has a considerably larger phase speed than that along the lower surface; this suggests that the integrated loading along the upper surface is more strongly correlated. When the thickness becomes too large, then most, if not all, of the incident vortex passes below the leading-edge. On the other hand, the relative tranverse offset of the edge with respect to the center of the incident vortex has a significant effect on the secondary vortex formation.
Document ID
19880003925
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Sohn, D.
(Lehigh Univ. Bethlehem, PA, United States)
Rockwell, Donald
(Lehigh Univ. Bethlehem, PA, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1987
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:182341
NASA-CR-182341
Report Number: NAS 1.26:182341
Report Number: NASA-CR-182341
Accession Number
88N13307
Funding Number(s)
CONTRACT_GRANT: NAG1-461
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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