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Shock Wave – Boundary Layer Interaction in Reactive H2/O2 Mixture

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29th International Symposium on Shock Waves 1 (ISSW 2013)

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Abstract

Shock wave - boundary layer interaction (SWBLI) has been widely discussed over the decades. SWBLI is usually associated with high speed fights, airfoils etc. However, phenomena mentioned above are linked to non-reactive environment. As for reactive mixtures, SWBLI have been observed in reflected shocks studies and ram accelerators.

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Author information

Authors and Affiliations

  1. Dept. Mechanical Engineering, Aoyama Gakuin University, Kanagawa-ken, Sagamihara-shi, Chuo-ku, Fuchinobe 5-10-1, J323, Japan

    E. Dziemińska & A. K. Hayashi

Authors
  1. E. Dziemińska
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  2. A. K. Hayashi
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Editor information

Editors and Affiliations

  1. Department of Engineering Physics, University of Wisconsin, Madison, USA

    Riccardo Bonazza

  2. Department of Mechanical Engineering, Georgia Institute of Technology, Atlanta, Georgia, USA

    Devesh Ranjan

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© 2015 Springer International Publishing Switzerland

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Dziemińska, E., Hayashi, A.K. (2015). Shock Wave – Boundary Layer Interaction in Reactive H2/O2 Mixture. In: Bonazza, R., Ranjan, D. (eds) 29th International Symposium on Shock Waves 1. ISSW 2013. Springer, Cham. https://doi.org/10.1007/978-3-319-16835-7_40

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