Skip to main content
SpringerLink
Log in
Book cover

30th International Symposium on Shock Waves 1 pp 71–75Cite as

Adaptation of the Transpiration Method to Simulate the Fluid–Structure Interaction Phenomena for a Flexible Overexpanded Rocket Nozzle

  • Conference paper
  • First Online:

  • 2039 Accesses

Abstract

The aim of this paper is to present a new aeroelastic stability model taking into account the viscous effects for a supersonic nozzle flow in overexpanded regimes. This model is inspired from the Pekkari model which was developed initially for perfect fluid flow. The new model called the “modified Pekkari model” (MPM) considers a more realistic wall pressure profile for the case of a free shock separation (FSS) inside the supersonic nozzle using the free interaction theory of Chapman. The main results are presented in a comparative manner using existing models (Pekkari model and its extended version) and the modified Pekkari model developed in this work.

This is a preview of subscription content, log in via an institution.

Chapter
USD   29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD   259.00
Price excludes VAT (USA)
  • Available as EPUB and PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD   329.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info
Hardcover Book
USD   329.99
Price excludes VAT (USA)
  • Durable hardcover edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Purchases are for personal use only

Learn about institutional subscriptions

References

  1. Bekka, N.: Problématique des ondes de choc dans les tuyères supersoniques et leur interaction avec la structure. Ph.D. thesis, Université d’Evry Val d’Essonne (2014)

    Google Scholar 

  2. Lefrançois, E.: Etude numérique du décollement de jet et du phénomène de charges latérales au sein des moteurs fusée avec prise en compte de l’aéroélasticité, Rapport de post-doctorat. CORIA/CNES (2000)

    Google Scholar 

  3. Mouronval, A.-S.: Etude numérique des phénomènes aéroélastiques en aérodynamique supersonique. Application aux tuyères propulsives. Ph.D. thesis, INSA de Rouen (2004)

    Google Scholar 

  4. Pekkari, L.O.: Aeroelastic analysis of side-loads in supersonic nozzles with separated flow. AIAA Paper 94-3377 (1994)

    Google Scholar 

  5. Pekkari, L.O.: Aeroelastic stability of supersonic nozzles with separated flow. AIAA Paper 93-2588 (1993)

    Google Scholar 

  6. Lefrançois, E.: Numerical validation of a stability model for a flexible over-expanded rocket nozzle. Int. J. Numer. Methods Fluids 49(4), 349–369 (2005)

    Article  MATH  Google Scholar 

  7. Chapman, D.R., Huehn, D.M., Larson, H.K.: Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition. Technical Report NACA TR 1356, NACA (1958)

    Google Scholar 

  8. Ashley, H., Zartarian, G.: Piston theory, a new aerodynamic tool for the aeroelastician. J. Aeronaut. Sci. 23(12), 1109–1118 (1956)

    Article  MathSciNet  Google Scholar 

Download references

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
    View author publications

    You can also search for this author in PubMed Google Scholar

  2. M. Sellam
    View author publications

    You can also search for this author in PubMed Google Scholar

  3. A. Chpoun
    View author publications

    You can also search for this author in PubMed Google Scholar

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

Rights and permissions

Reprints and permissions

Copyright information

© 2017 Springer International Publishing AG

About this paper

Cite this paper

Bekka, N., Sellam, M., Chpoun, A. (2017). Adaptation of the Transpiration Method to Simulate the Fluid–Structure Interaction Phenomena 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_11

Download citation

  • DOI: https://doi.org/10.1007/978-3-319-46213-4_11

  • Published:

  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-46211-0

  • Online ISBN: 978-3-319-46213-4

  • eBook Packages: EngineeringEngineering (R0)

Publish with us

Policies and ethics

Search

Navigation