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Reflection of shock wave from a compression corner in a particle-laden gas region

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Abstract

We investigated in this paper the progression of a shock-wave reflected from a compression corner in a particle-laden gas medium using a TVD class numerical technique and a MacCormack scheme. For a gas-only flow, the numerical results agreed well with the existing experimental data, suggesting that the gas phase is correctively solved. The effect of particle size and mass fraction ratio is investigated for a dilute gas-particle flow. It has been shown that the shock-wave diffraction and the flow configuration after the shock can become remarkably different from the gas-only flow depending on the particle parameters. Relaxation phenomenon due to the momentum drag and the heat exchange between the gas and the particle phases is explained.

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Authors and Affiliations

  1. Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology, P.O. Box 150, 130-650, Cheongryang Seoul, Republic of Korea

    Seung-Woo Kim & Keun-Shik Chang

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  1. Seung-Woo Kim
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  2. Keun-Shik Chang
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Graduate Student of Korea Advanced Institute of Science and Technology

This article was processed using Springer-Verlag TEX Shock Waves macro package 1990.

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Kim, SW., Chang, KS. Reflection of shock wave from a compression corner in a particle-laden gas region. Shock Waves 1, 65–73 (1991). https://doi.org/10.1007/BF01414869

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  • DOI: https://doi.org/10.1007/BF01414869

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