An aeroacoustic mechanism to explain universal behavior in hypersonic wake flow oscillations

Fuente: arXiv
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Autores principales: Thasu, Premika S., Kumar, Gaurav, Duvvuri, Subrahmanyam
Formato: Preprint
Publicado: 2024
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author Thasu, Premika S.
Kumar, Gaurav
Duvvuri, Subrahmanyam
author_facet Thasu, Premika S.
Kumar, Gaurav
Duvvuri, Subrahmanyam
contents Recent experimental studies reveal that the near-wake region of a circular cylinder at hypersonic Mach numbers exhibits self-sustained flow oscillations. The oscillation frequency was found to have a universal behavior. Experimental observations suggest an aeroacoustic feedback loop to be the driving mechanism of oscillations. An analytical aeroacoustic model which predicts the experimentally observed frequencies and explains the universal behavior is presented here. The model provides physical insights and informs of flow regimes where deviations from universal behavior are to be expected.
format Preprint
id arxiv_https___arxiv_org_abs_2407_06449
institution arXiv
publishDate 2024
record_format arxiv
spellingShingle An aeroacoustic mechanism to explain universal behavior in hypersonic wake flow oscillations
Thasu, Premika S.
Kumar, Gaurav
Duvvuri, Subrahmanyam
Fluid Dynamics
Recent experimental studies reveal that the near-wake region of a circular cylinder at hypersonic Mach numbers exhibits self-sustained flow oscillations. The oscillation frequency was found to have a universal behavior. Experimental observations suggest an aeroacoustic feedback loop to be the driving mechanism of oscillations. An analytical aeroacoustic model which predicts the experimentally observed frequencies and explains the universal behavior is presented here. The model provides physical insights and informs of flow regimes where deviations from universal behavior are to be expected.
title An aeroacoustic mechanism to explain universal behavior in hypersonic wake flow oscillations
topic Fluid Dynamics
url https://arxiv.org/abs/2407.06449