Skip to main content

On the Problem of Shock Wave Structure

  • Conference paper
  • First Online:
31st International Symposium on Shock Waves 1 (ISSW 2017)

Included in the following conference series:

  • 1466 Accesses

Abstract

We consider the problem of internal structure of the triple point appearing in Mach reflection, which is considered to be important for the cause study of the von Neumann paradox as well as the shock reflection itself in rarefied gas. We investigate it in an adequately made finite region near the triple point and use analytical approach rather than numerical to have a solution of 2D Navier-Stokes equations system, by which we can avoid the difficulties such as the need for ever finer mesh size for the region not known in the beginning. We consider first one-dimensional flow in a finite region, which gives a flow with a hump unlike conventional one of monotonous change for the infinite region. Then we seek a solution of the 2D Navier-Stokes equations system in polar coordinates to the flow field between two curved boundaries. Results show the incoming parallel flow bents to the direction of the slip flow and the density distribution along the streamline increases similar to that for one-dimensional shock structure but a small hump as the solution over to the flow for a finite range.

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 259.00
Price excludes VAT (USA)
  • Available as EPUB and PDF
  • Read on any device
  • Instant download
  • Own it forever
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

Institutional subscriptions

References

  1. J. Sternberg, Phys. Fluids 2(2), 179 (1959)

    Article  Google Scholar 

  2. G. Birkhoff, Hydrodynamics: A Study in Logic and Similitude, 1st edn (Princeton UP, 1950), p. 24

    Google Scholar 

  3. H. Chen et al., J. Spacecraft Rockets 53(4), 619 (2016)

    Article  Google Scholar 

  4. R. Becker, Z. Physik 8, 321 (1922)

    Article  Google Scholar 

  5. G.I. Taylor, Aerodynamic Theory, ed. by W. F. Durand, III, 218–222, Springer, Berlin (1932).

    Google Scholar 

  6. A. Sakurai, M. Tsukamoto, S. Kobayashi, On a problem of shock wave structure (in Japanese), Japan Symp. Shock Waves, 1C1-3 (2017)

    Google Scholar 

  7. A. Sakurai, J. Phys. Soc. Jpn. 19, 1440 (1964)

    Article  Google Scholar 

  8. A. Sakurai, Flow field behind Mach reflection and the Neumann paradox, ISSW30, Program and Abstracts, 31 (2015)

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to A. Sakurai .

Editor information

Editors and Affiliations

Appendix: Solution of Triple-Point Singularity [7, 8]

Appendix: Solution of Triple-Point Singularity [7, 8]

This is a r-power expansion solution of Eq. (6) in angler region between the reflected and Mach stems satisfying the shock boundary condition at the two shock lines so that it is singular at the triple point r = 0, which in fact represents the flow in the non-R-H zone caused by shock lines with different shock values meeting there. Some of the results relevant to this study are

$$ {\displaystyle \begin{array}{l}{\tilde{V}}_{\theta }={\tilde{V}}_{\theta}^{(0)}+r{\tilde{V}}_{\theta}^{(1)},{\tilde{V}}_r={\tilde{V}}_r^{(0)}+r{\tilde{V}}_r^{(1)},\tilde{\rho}={\tilde{\rho}}^{(0)}+r{\tilde{\rho}}^{(1)},\tilde{p}={\tilde{p}}^{(0)}+\mathrm{r}{\tilde{\mathrm{p}}}^{(1)}\\ {}{\tilde{V}}_{\theta}^{(0)}{=}\tilde{A}\left(1{+} k\theta \right)\sin \left(\theta {+}{\theta}_0\right),{\tilde{V}}_r^{(0)}=-\tilde{A}\left[\left(1{+} k\theta \right)\cos \left(\theta {+}{\theta}_0\right){+}k/7\sin \left(\theta {+}{\theta}_0\right)\right]\\ {}{\tilde{\rho}}^{(0)}=E{\left(1+ k\theta \right)}^{-6/7},{\tilde{p}}^{(0)}={\tilde{\rho}}^{(0)}\left( F\theta +G\right),\\ {}{\tilde{V}}_{\theta}^{(1)}=-\left(1/2\right)\tilde{A}{}_1\;\sin \left(\theta +{\theta}_0-2\alpha \right)\sin \left(\theta +{\theta}_0\right)+{S}_1\left(\theta \right)\\ {}{\tilde{V}}_r^{(1)}=-\left(1/2\right)\tilde{A}{}_1\;\cos \left(\theta -{\theta}_0-2\alpha \right)\sin \left(\theta +{\theta}_0\right)+{S}_2\left(\theta \right),\\ {}{S}_1\left(-{\theta}_0\right)={S}_1\left(-{\theta}_0\right)={\tilde{\rho}}^{(1)}\left(-{\theta}_0\right)={\tilde{p}}^{(1)}\left(-{\theta}_0\right)=0\end{array}} $$

Rights and permissions

Reprints and permissions

Copyright information

© 2019 Springer International Publishing AG, part of Springer Nature

About this paper

Check for updates. Verify currency and authenticity via CrossMark

Cite this paper

Sakurai, A., Kobayashi, S. (2019). On the Problem of Shock Wave Structure. In: Sasoh, A., Aoki, T., Katayama, M. (eds) 31st International Symposium on Shock Waves 1. ISSW 2017. Springer, Cham. https://doi.org/10.1007/978-3-319-91020-8_108

Download citation

  • DOI: https://doi.org/10.1007/978-3-319-91020-8_108

  • Published:

  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-91019-2

  • Online ISBN: 978-3-319-91020-8

  • eBook Packages: EngineeringEngineering (R0)

Publish with us

Policies and ethics