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)


Shock Wave Shear Layer Blast Wave Inertial Frame Vortex Sheet 
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  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

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