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Study of separated flows over double wedges and cones

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Abstract

This paper reports results of flow diagnostics over a double wedge or cone at a stagnation enthalpy 4.8 MJ/kg. The experiment was carried out in a free piston shock tunnel at Interdisciplinary Shock Wave Research Center (ISWRC) at a nominal Mach number of 6.99. Schlieren and double exposure holographic interferometry were applied to visualize the flow fields. The flow fields induced separation over double wedge or cone were successfully visualized.

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References

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Author information

Authors and Affiliations

  1. Japan Aerospace Exploration Agency, 1-Koganezawa, Kimigaya, Kakuda, Miyagi, 981-1525, Japan

    T. Hashimoto

  2. Interdisciplinary Shock Wave Research Center, Institute of Fluid Science, Tohoku University, 2-1-1 Katahira, Aoba-ku, Sendai, Miyagi, 980-8577, Japan

    K. Takayama

Authors
  1. T. Hashimoto
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  2. K. Takayama
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Editor information

Editors and Affiliations

  1. Key Laboratory of High-Temperature Gas Dynamics Institute of Mechanics, Chinese Academy of Sciences, 15 Bei Si Huan Xi Rd., Beijing, 100080, P.R. China

    Z. Jiang

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© 2005 Tsinghua University Press and Springer-Verlag Berlin Heidelberg

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Hashimoto, T., Takayama, K. (2005). Study of separated flows over double wedges and cones. In: Jiang, Z. (eds) Shock Waves. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-27009-6_71

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  • DOI: https://doi.org/10.1007/978-3-540-27009-6_71

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  • 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)

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