Flow Structure in a Model of Aircraft Trailing Vortices

James Faddy

Graduate Aeronautical Laboratories
Caltech

Abstract-
We consider a model of incompressible trailing vortices consisting of an array of counter-rotating structures in a doubly periodic domain, infinite in the vertical direction. The two-dimensional vortex array of Mallier and Maslowe is combined with an axial velocity profile chosen proportional to the initial axial vorticity to provide an initial condition for the vortex wake. This base flow is a weak solution of the 2D-3C steady Euler equations thus allowing its linear stability properties to be investigated. These are used to interpret several stages in the development of vortex structure observed in 3D-3C DNS at Reynolds numbers of O(1000). For sufficiently high axial velocity, its effect can be seen, in that each vortex in the linear array first develops helical structures before undergoing a period of relaminarization. At later times the more slowly growing co-operative elliptical instabilities become apparent; however, the helical structure persists and the observed vortical structures remain coherent for longer periods than in the absence of axial velocity. Using the stretched vortex subgrid model, large-eddy simulation runs are performed at higher Reynolds numbers and a mixing transition identified at about Re =1-2 x 10^4. Similar phenomena are observed in these simulations as are seen in the DNS. Finally, a model for the average axial pressure gradient present in the true spatially evolving wake, but absent in the numerical simulations is formulated and its affect investigated.


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