Numerical Simulations of a Counter-rotating Vortex Pair

Collaborator: Jim Rottman
Graduate Student Researchers: Hideaki Tsutsui, Julie Crockett


Description

The evolution of a pair of counter-rotating parallel vortices is investigated using three-dimensional direct numerical simulations. Such a flow may be encountered in the wake of an aircraft. The strong vortices of a large aircraft, particularly during take-off and landing, can pose a serious threat to following aircraft and is a limiting factor for airport traffic. The study of the mechanisms by which these vortices decay and breakdown is therefore of great practical importance. The dynamics of coherent vortices are also of fundamental interest as they are the basic elements of turbulent flows.


The inherent instabilities in the flow can promote vortex decay and result in their destruction. In general, a counter-rotating vortex pair may exhibit a short wave (elliptic) instability and a long wave (Crow) instability. The short wave instability is associated with the ellipticity of the streamlines in the vortex cores due to the strain induced by one vortex on the other. The vortices exhibit a sinusoidal antisymmetric deformation with wavelength on the order of the initial vortex spacing, bo. The Crow instability exhibits a symmetric deformation with wavelength of order 10(bo). This study focuses on the short wave instability. This instability has been observed in the unstratified laboratory experiments of Leweke and Williamson (1998).

The objective of our current research is to investigate the effects of stable density stratification on the short wave instability and subsequent breakdown of the flow. To fully investigate the associated physics, three-dimensional simulations with high spatial resolution are required.

Our simulation results show an earlier onset and higher growth rate with stable stratification. This is due to the enhanced strain that occurs when the vortices move closer together as a result of the generated baroclinic torque. With relatively weak stratification, the wavelength of the instability remains comparable to that in the unstratified case and a significant increase in the growth rate is exhibited. For stronger stratification, the form of the instability becomes more complex and the growth rate is less than that for weak stratification.


Development of vortex pair in strongly stratified fluid (Re = 2400, Fr=1).

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