Department of Aerospace Engineering and Mechanics
University of Minnesota
Abstract-
Over the past several decades an increased awareness has grown
about the role coherent vortex structures play in incompressible
turbulent boundary layers. In this seminar, a physical model will be
outlined which gives a kinematic description of turbulent boundary layers
in terms of an assemblage of attached eddies. The formulation is used to
compute statistical quantities such as two-point space correlation
functions, spectra and Reynolds stresses. Quantitative comparisons are
made with experimental data and support is given for the scenario
where in the logarithmic region of the flow, the main structures are
long streamwise, spatially correlated trains or packets of eddies.
Related issues of Reynolds number scaling laws for the turbulence
intensities are also considered and some preliminary results from
high Reynolds number experiments on the salt-flats of Utah will be
presented.
A brief consideration will also be given to the potential use of this physical model for supersonic boundary layer flows. Visualization results will be presented using the DNS data of Martin and Candler of a Mach 4 turbulent boundary layer.
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