Skip to main content
Book cover

Shock Waves pp 837–842Cite as

Investigation on detonation in 2H2/O2 mixture initiated by AgN3

  • Conference paper
  • First Online:
  • 93 Accesses

Abstract

Gas detonation in 2H2/O2 mixture initiated by high explosive AgN3 is numerically studied in this paper. Fully 3D Navier-Stokes equations are solved by upper wind TVD scheme. Self-similar solution is used to simulate ignition of AgN3 by neglecting its detailed chemistry. The flow field near explosion center must be simplified because of the high temperature. Chemical source term is treated by point-implicit method to avoid the stiffness. 12species/23steps model is used to describe the chemistry of 2H2/O2 mixture. Contours of pressure, temperature, and species mass fraction are obtained. The results indicate that the self-sustained propagating spherical detonation wave can be generated, and DDT process is shortened for large shock Mach number Ms. The detonation wave reflects as shock waves on side and end walls. For different Ms (2.0∼3.5), the parameters of steady detonation are the same but flow field near the explosion center is different. The computed detonation parameters are less than those got from C-J theory.

Supported by National Nature Science Foundation

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

Buying options

Chapter
USD   29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD   299.00
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever

Tax calculation will be finalised at checkout

Purchases are for personal use only

Learn about institutional subscriptions

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

References

  1. D.C. Bull, J.E. Eisworth, G. Hooper: Astronautica Acata. 15, 997 (1978)

    Article  ADS  Google Scholar 

  2. V.P. Korobeinikov, V.A. Levin, V.V. Markov et al.: Propagation of blast wave in a combustible gas. Astronautica Acta 17, 529 (1972)

    Google Scholar 

  3. J.H. Lee: Annual Review of Fluid Mechanics 16, 311 (1984)

    Article  ADS  Google Scholar 

  4. M.A. Sussman: Computational study of unsteady shock induced combustion of hydrogen-air mixture. AIAA-94-3010 (1994)

    Google Scholar 

  5. K. Tanaka, A. Takahashi, K. Tokuhashi et al.: ‘Numerical Study on the Direct Initiation in Hydrogen-air Mixture’. In: Private communication, (2001)

    Google Scholar 

  6. H.C. Yee: Upwind and symmetric shock-capturing schemes. NASA 89464 (1987)

    Google Scholar 

  7. P.A. Thompson: Compressible-Fluid Dynamics. (McGRAW-Hill book Co., 1972) pp.347–355

    Google Scholar 

  8. R.J. Kee, F.M. Rupley, J.A. Miller:Chemkin-II: a Fortran Chemical Kinetics Package for the Analysis of Gas-phase Chemical Kinetics. (SAND 898009B 1989)

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Editor information

Editors and Affiliations

Rights and permissions

Reprints and permissions

Copyright information

© 2005 Tsinghua University Press and Springer-Verlag Berlin Heidelberg

About this paper

Cite this paper

Xu, S.L., Takayama, K., Sun, M.Y. (2005). Investigation on detonation in 2H2/O2 mixture initiated by AgN3 . In: Jiang, Z. (eds) Shock Waves. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-27009-6_126

Download citation

  • DOI: https://doi.org/10.1007/978-3-540-27009-6_126

  • Published:

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-540-22497-6

  • Online ISBN: 978-3-540-27009-6

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

Publish with us

Policies and ethics