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Shock Waves pp 467-472 | Cite as

Analytical solution of flow field for weak Mach reflection over plane surface

  • A. Sakurai
  • F. Takayama
Conference paper

Abstract

Concerned here with the analytical solution of flow field of single weak Mach reflection caused by an advancing plane shock wave over a simple wedge surface. We develop an improvement of Lighthill’s linearized theory in the correction due to the non-linearity of the flow field through a singular perturbation. Obtained expressions including the one for the triple point path are compared resonably well with existing experimental, computational and theoretical results.

Keywords

Shock Wave Flow Field Singular Perturbation Mach Stem Weak Shock Wave 
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.

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References

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    Adachi, et al.: ‘Benchmark Test of Reflection of Weak Shock Waves from Wedges’. In: Proc. 21st Int. Symp on Shock Waves, 1997, (Panther Publishing, Australia 1997) pp. 883–840Google Scholar
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Copyright information

© Tsinghua University Press and Springer-Verlag Berlin Heidelberg 2005

Authors and Affiliations

  • A. Sakurai
    • 1
  • F. Takayama
    • 2
  1. 1.Tokyo Denkt UniversityTokyoJapan
  2. 2.Iwaki Meisei UniversityFukushimaJapan

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