Advertisement

The effect of viscosity on the mach stem length in unsteady strong shock reflection

  • Hans Hornung
I. Compressibility and Sound
Part of the Lecture Notes in Physics book series (LNP, volume 235)

Keywords

Shock Wave Shear Layer Blast Wave Inertial Frame Vortex Sheet 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

References

  1. [1]
    Hornung, H.: “Regular and Mach reflection of shock waves.” To be published in Ann. Rev. Fluid Mech. (1986)Google Scholar
  2. [2]
    Walenta, Z. A.: “Formation of the Mach-type reflection of shock waves.” Arch. Mech. 35, (1983) 187–196Google Scholar
  3. [3]
    Schmidt, B.: “Stoßwellenübergang von regulärer Reflektion zur Mach Reflektion auf der Flanke eines Keils.” ZAMM 65 (1985)Google Scholar
  4. [4]
    Hornung, H.G.; Taylor, J.R.: “Transition from regular to Mach reflection of shock waves. Part 1. The effect of viscosity in the pseudosteady case.” J. Fluid Mech. 123 (1982) 143–153Google Scholar
  5. [5]
    Becker, E.: “Instationäre Grenzschichten hinter Verdichtungsstößen und Expansionswellen.” In: “Progress in Aero. Sci.” eds. Ferri, Küchemann, Sterne, 1 (1961) 104–153Google Scholar
  6. [6]
    Henderson, L.F.; Gray, P.M.: “Experiments on the diffraction of strong blast waves.” Proc. Roy. Soc. Lond. A 377 (1981) 363–378Google Scholar

Copyright information

© Springer-Verlag 1985

Authors and Affiliations

  • Hans Hornung
    • 1
  1. 1.Institut für Experimentelle Strömungsmechanik DFVLR-AVAGöttingen

Personalised recommendations