Skip to main content

General Introduction

  • Chapter
  • First Online:
High Temperature Phenomena in Shock Waves

Part of the book series: Shock Wave Science and Technology Reference Library ((SHOCKWAVES,volume 7))

  • 1473 Accesses

Abstract

The production of high temperatures in gases constitutes one major feature of shock waves which represent one of the best means to transform kinetic energy into thermal energy. One of the most important consequences lies in the physical and chemical phenomena which may arise from these high temperatures such as rotational and vibrational excitation of molecules, dissociation, ionization and various chemical reactions, as well as associated radiation. Another fundamental feature proceeds from the fact that, in collisional regime (continuum), the shock wave may be considered as a discontinuity, so that the temperature rise is quasi-instantaneous. Thus, as the characteristic time required for the development of the physical and chemical phenomena is non-negligible, since it is related to collisions between elementary particles, the gaseous medium behind shock waves is in a non-equilibrium thermodynamic and chemical state.

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

Access this chapter

Chapter
USD 29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD 129.00
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD 169.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info
Hardcover Book
USD 169.99
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

Institutional subscriptions

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

References

  1. Gaydon, A.G., Hurle, I.R.: The Shock Tube in High Temperature Research. Chapman and Hall, London (1963)

    Google Scholar 

  2. Park, C.: Nonequilibrium Hypersonic Aerothermodynamics. J.Wiley, New-York (1990)

    Google Scholar 

  3. Vincenti, W.G., Krüger, C.H.: Introduction to Physical Gas Dynamics. R.G.Krieger, Florida (1965)

    Google Scholar 

  4. Stupochenko, Y.V., Losev, S.A., Osipov, A.I.: Relaxation in Shock Waves. Springer, Berlin (1967)

    Google Scholar 

  5. Oertel, H.: Stossrohre. Springer, Wien (1966)

    Google Scholar 

  6. Brun, R.: ntroduction to Reactive Gas Dynamics. Oxford Univ. Press, Oxford (2009)

    Book  Google Scholar 

  7. Belouaggadia, N., Armenise, I., Capitelli, M., Esposito, F., Brun, R.: J. Therm. Heat Transf. 24(4), 684 (2010)

    Article  Google Scholar 

  8. Ramjaun, D., Dumitrescu, M.P., Brun, R.: J. Therm. Heat Transf. 13(2), 219 (1999)

    Article  Google Scholar 

  9. Bird, G.A.: Rarefied Gas Dynamics, vol. 175. Tokyo Univ. Press, Tokyo (1984)

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Editor information

Editors and Affiliations

Rights and permissions

Reprints and permissions

Copyright information

© 2012 Springer Berlin Heidelberg

About this chapter

Cite this chapter

Brun, R. (2012). General Introduction. In: Brun, R. (eds) High Temperature Phenomena in Shock Waves. Shock Wave Science and Technology Reference Library, vol 7. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-25119-1_1

Download citation

  • DOI: https://doi.org/10.1007/978-3-642-25119-1_1

  • Published:

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-25118-4

  • Online ISBN: 978-3-642-25119-1

  • eBook Packages: Physics and AstronomyPhysics and Astronomy (R0)

Publish with us

Policies and ethics