Abstract
The growth of short-wave elliptical instabilities in a Lamb-Oseen vortex pair subject to non-uniform strain fields at close vortex spacing is considered using direct numerical simulation at a Reynolds number Re = 20000. A linear stability analysis demonstrates that with reduced vortex spacing the growth rate of all axial wave-numbers is enhanced relative to that of the fastest-growing mode. A coupling of vortices is observed at close vortex spacing, which may lead to improved non-linear instability growth, and the development of fluid cross-over regions. These fluid cross-over regions are shown to be products of a linear growth regime.
Original language | English |
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Pages (from-to) | 276-283 |
Number of pages | 8 |
Journal | Progress in Computational Fluid Dynamics |
Volume | 10 |
Issue number | 5-6 |
DOIs | |
Publication status | Published - 2010 |
Keywords
- aircraft wakes
- elliptic instability
- fluid cross-over
- growth rate
- Lamb-Oseen
- linear stability analysis
- vortex pair