Instability mechanisms in meandering streamwise vortex pairs of upswept afterbody wakes

نویسندگان

چکیده

Wakes of upswept afterbodies are often characterized by counter-rotating streamwise vortex pairs which meander in space. One application concerns aft regions cargo aircraft, a relatively flat base. Here we consider canonical configuration comprised cylinder with basal surface. The resulting longitudinal vortices, much closer to each other than wing-tip can adversely influence paratrooper and drop operations as well trailing aircraft. unsteady dynamics these vortices examined using spatio-temporally resolved Large-Eddy Simulations (LES) stability considerations. Emphasis is placed on understanding the potential instability responsible for meandering, was observed, quantified at representative location downstream body. then successfully mapped matched Batchelor pair, spatial temporal analyses performed both computational domain. Both reveal dipole structures associated |m|=1 elliptic modes dominant afterbody vortices. A short-wave mode found dominate meandering motion pair; this stable case an isolated vortex. Further, strain due axial velocity plays key role therefore breakdown. low frequency unstable (Strouhal number StD≃0.3 based diameter) consistent spectral analysis LES. Stability very low-wavenumber do not exhibit any suggesting absence Crow instability.

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ژورنال

عنوان ژورنال: European Journal of Mechanics B-fluids

سال: 2022

ISSN: ['1873-7390', '0997-7546']

DOI: https://doi.org/10.1016/j.euromechflu.2022.07.006