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Effect of Nozzle Configurations on Unsymmetrical Supersonic Flows

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Shock Waves @ Marseille I

Abstract

In the present study, to analyze the effects of the flow Mach number at nozzle entrance and the divergence angle of the nozzle on the flow; six kinds of nozzle with different divergence angles and wall lengths were used. Furthermore, the appearance and oscillation of a pseudo-shock wave was investigated. A Schlieren system, and a Mach-Zehnder interferometer composed of an Argon laser (CW) as the light source with both an acoustic-optic modulator (AOM) and an electro-optic modulator (EOM) were used to visualize the flow.

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References

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Author information

Authors and Affiliations

  1. Department of Mechanical Systems Engineering, Tokyo Noko University, Koganei-shi, Tokyo 184, Japan

    Y. Watanabe, S. Matsuo & F. Higashino

Authors
  1. Y. Watanabe
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  2. S. Matsuo
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  3. F. Higashino
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Editor information

Editors and Affiliations

  1. Centre Saint-Jérôme, Université de Provence, Case 321, F-13397, Marseille Cedex 20, France

    Raymond Brun  & Lucien Z. Dumitrescu  & 

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© 1995 Springer-Verlag Berlin Heidelberg

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Watanabe, Y., Matsuo, S., Higashino, F. (1995). Effect of Nozzle Configurations on Unsymmetrical Supersonic Flows. In: Brun, R., Dumitrescu, L.Z. (eds) Shock Waves @ Marseille I. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-78829-1_19

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  • DOI: https://doi.org/10.1007/978-3-642-78829-1_19

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-78831-4

  • Online ISBN: 978-3-642-78829-1

  • eBook Packages: Springer Book Archive

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