Aeroelastic instability in a jet-plate interaction

Maxime Antoine; Pascal Hémon; Emmanuel de Langre

doi:10.1016/j.crme.2007.07.006

Aeroelastic instability in a jet-plate interaction

Maxime Antoine
, Pascal Hémon
, Emmanuel de Langre

Département de mécanique
Laboratoire d'Hydrodynamique de l'Ecole Polytechnique

Résultats de recherche: Contribution à un journal › Article › Revue par des pairs

1 Citation (Scopus)

Résumé

A flexible sheet subject to a normal impinging air jet can oscillate. We present a simple experiment that shows that added damping generated by the jet is responsible for this aeroelastic instability. The cases of planar jet and circular jet are studied. A model is presented to describe this instability and the results agree well with the experimental observations. The nozzle geometry is found to be a dominant parameter that drives the critical distance between the jet and the sheet, under which the instability develops. To cite this article: M. Antoine et al., C. R. Mecanique 335 (2007).

langue originale	Anglais
Pages (de - à)	691-695
Nombre de pages	5
journal	Comptes Rendus - Mecanique
Volume	335
Numéro de publication	11
Les DOIs	https://doi.org/10.1016/j.crme.2007.07.006
état	Publié - 1 nov. 2007

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10.1016/j.crme.2007.07.006

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title = "Aeroelastic instability in a jet-plate interaction",

abstract = "A flexible sheet subject to a normal impinging air jet can oscillate. We present a simple experiment that shows that added damping generated by the jet is responsible for this aeroelastic instability. The cases of planar jet and circular jet are studied. A model is presented to describe this instability and the results agree well with the experimental observations. The nozzle geometry is found to be a dominant parameter that drives the critical distance between the jet and the sheet, under which the instability develops. To cite this article: M. Antoine et al., C. R. Mecanique 335 (2007).",

keywords = "Aeroelasticity, Fluid-structure interactions, Instability, Jet, Stability",

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T1 - Aeroelastic instability in a jet-plate interaction

AU - Antoine, Maxime

AU - Hémon, Pascal

AU - de Langre, Emmanuel

PY - 2007/11/1

Y1 - 2007/11/1

N2 - A flexible sheet subject to a normal impinging air jet can oscillate. We present a simple experiment that shows that added damping generated by the jet is responsible for this aeroelastic instability. The cases of planar jet and circular jet are studied. A model is presented to describe this instability and the results agree well with the experimental observations. The nozzle geometry is found to be a dominant parameter that drives the critical distance between the jet and the sheet, under which the instability develops. To cite this article: M. Antoine et al., C. R. Mecanique 335 (2007).

AB - A flexible sheet subject to a normal impinging air jet can oscillate. We present a simple experiment that shows that added damping generated by the jet is responsible for this aeroelastic instability. The cases of planar jet and circular jet are studied. A model is presented to describe this instability and the results agree well with the experimental observations. The nozzle geometry is found to be a dominant parameter that drives the critical distance between the jet and the sheet, under which the instability develops. To cite this article: M. Antoine et al., C. R. Mecanique 335 (2007).

KW - Aeroelasticity

KW - Fluid-structure interactions

KW - Instability

KW - Jet

KW - Stability

UR - https://www.scopus.com/pages/publications/36049038017

U2 - 10.1016/j.crme.2007.07.006

DO - 10.1016/j.crme.2007.07.006

M3 - Article

AN - SCOPUS:36049038017

SN - 1631-0721

VL - 335

SP - 691

EP - 695

JO - Comptes Rendus - Mecanique

JF - Comptes Rendus - Mecanique

IS - 11

ER -

Aeroelastic instability in a jet-plate interaction

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