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30th International Symposium on Shock Waves 1 pp 67–70Cite as

New Modified Pekkari Model to Analyse the Aeroelastic Stability Behaviour for a Flexible Overexpanded Rocket Nozzle

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Abstract

The aim of this study is to develop a new approach for the aeroelastic stability analysis of a flexible overexpanded rocket nozzle using numerical fluid–structure coupling via the transpiration method. The method consists of a weak coupling between two numerical codes; one is dedicated to the computational structural dynamics (CSD) and the other to the computational fluid dynamics (CFD). The main results issued from the coupled computation are compared with those of the aeroelastic stability models developed in previous works.

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Author information

Authors and Affiliations

  1. Laboratoire de Mécanique et d’Energétique d’Evry LMEE, Université d’Evry Val d’Essonne, 40 rue du Pelvoux, 91020, Evry Cedex, France

    N. Bekka, M. Sellam & A. Chpoun

Authors
  1. N. Bekka
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  2. M. Sellam
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  3. A. Chpoun
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Corresponding author

Correspondence to N. Bekka .

Editor information

Editors and Affiliations

  1. Department of Mechanical Engineering, Ben Gurion University of the Negev, Beer Sheva, Israel

    Gabi Ben-Dor

  2. Department of Mechanical Engineering, Ben-Gurion University of the Negev, Beer Sheva, Israel

    Oren Sadot

  3. Department of Mechanical Engineering, Ben Gurion University of the Negev, Beer Sheva, Israel

    Ozer Igra

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© 2017 Springer International Publishing AG

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Bekka, N., Sellam, M., Chpoun, A. (2017). New Modified Pekkari Model to Analyse the Aeroelastic Stability Behaviour for a Flexible Overexpanded Rocket Nozzle. In: Ben-Dor, G., Sadot, O., Igra, O. (eds) 30th International Symposium on Shock Waves 1. Springer, Cham. https://doi.org/10.1007/978-3-319-46213-4_10

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  • DOI: https://doi.org/10.1007/978-3-319-46213-4_10

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  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-46211-0

  • Online ISBN: 978-3-319-46213-4

  • eBook Packages: EngineeringEngineering (R0)

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