High-fidelity simulations of a perturbed vortex pair in ground effect
ORAL
Abstract
The influence of a planar wall on the temporal development of the long-wavelength instability of a counter- rotating trailing vortex pair is studied computationally. The unsteady flow field is computed using high-fidelity implicit large-eddy simulations, where viscous and inviscid wall conditions are considered to further elucidate the effect of the wall on the vortex pair. The principal effect of the wall is to suppress the long-wavelength Crow instability growth rate as the vortex pair splits and moves along the planar boundary. The evolution of the perturbed vortex pair system is compared to an inviscid theoretical model for the perturbation development, which corroborates the temporary suppression of perturbation growth and shift of the maximum perturbation amplitude to a higher wavenumber. Inviscid simulations reveal that the perturbation inhibition process can be attributed to the rotation of the instability plane angle and to the diverging vortex center positions of the vortex pair, which are consistent with theoretical predictions and with the behavior of the vortex pair in a viscous fluid.
*This work was supported in part by Air Force Office of Scientific Research grant number FA9550-19-1-0095 monitored by Dr. Gregg Abate and by Office of Naval Research grant numbers N00014-23-1-2700 and N00014-23-1-2111 monitored by Dr. Yin Lu (Julie) Young. The high-performance computer time and resources provided by the DoD High Performance Computing Modernization Program are also gratefully acknowledged.
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Presenters
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Mark Augustus Herndon
- Lehigh University