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Article Dans Une Revue AIAA Paper Année : 2011

Global linear stability of a model subsonic jet

Résumé

The global stability of a subsonic jet is investigated using a model base flow designed to fit experimental results for turbulent mean flows. Eigenmodes are computed for axisymmetric perturbations in order to investigate the nature of typically observed large-scale coherent oscillations ("preferred mode"). We do not find evidence that this preferred mode corre- sponds to the least damped global mode. Non-modal stability is also considered through the computation of optimal perturbations. Although non-axisymmetric perturbations (in particular for azimuthal wavenumber m = 1) are subject to larger transient growth, these reach their peak amplitude far downstream of the potential core, and therefore they are less likely to be observed.
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Dates et versions

hal-00716674 , version 1 (11-07-2012)

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  • HAL Id : hal-00716674 , version 1

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Xavier Garnaud, Lutz Lesshafft, Patrick Huerre. Global linear stability of a model subsonic jet. AIAA Paper, 2011, pp.2011-3608. ⟨hal-00716674⟩
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