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An Electrodynamic Aerobraking Experiment in a Rarefied Arc-Heated Flow

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31st International Symposium on Shock Waves 2 (ISSW 2017)

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Abstract

Our previous numerical study (Katsurayama et al. AIAA Paper 2008-4016) has predicted that an insulating boundary in a flow is necessary to activate electrodynamic braking in a rarefied flow: the insulating boundary can prevent the Hall effect from dissipating the current which is necessary for the electrodynamic braking. In order to validate this numerical prediction, the present study measures the total drag on a test model in a rarefied arc flow whose insulating boundary (that is an arc plume boundary) location is variable and compares the measured electrodynamic increases of the total drag with the computed values. As a result, the measured and computed total drags increase by applying the magnetic field, but contrary to the computational prediction, the measured electrodynamic increase of the total drag is insensitive to the insulating boundary location.

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Author information

Authors and Affiliations

  1. Yamaguchi University, Ube, Yamaguchi, Japan

    H. Katsurayama, N. Fukuda, T. Toyodome & Y. Katoh

  2. Kyushu University, Kasuga, Fukuoka, Japan

    K. Tomita

  3. Shizuoka University, Hamamatsu, Shizuoka, Japan

    M. Matsui

Authors
  1. H. Katsurayama
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  2. N. Fukuda
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  3. T. Toyodome
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  4. Y. Katoh
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  5. K. Tomita
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  6. M. Matsui
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Corresponding author

Correspondence to H. Katsurayama .

Editor information

Editors and Affiliations

  1. Department of Aerospace Engineering, Nagoya University, Nagoya, Japan

    Akihiro Sasoh

  2. Department of Energy and Environmental Engineering, Kyushu University, Kasuga, Fukuoka, Japan

    Toshiyuki Aoki

  3. Institute of Innovative Research, Tokyo Institute of Technology, Tokyo, Japan

    Masahide Katayama

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Katsurayama, H., Fukuda, N., Toyodome, T., Katoh, Y., Tomita, K., Matsui, M. (2019). An Electrodynamic Aerobraking Experiment in a Rarefied Arc-Heated Flow. In: Sasoh, A., Aoki, T., Katayama, M. (eds) 31st International Symposium on Shock Waves 2. ISSW 2017. Springer, Cham. https://doi.org/10.1007/978-3-319-91017-8_78

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  • DOI: https://doi.org/10.1007/978-3-319-91017-8_78

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  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-91016-1

  • Online ISBN: 978-3-319-91017-8

  • eBook Packages: EngineeringEngineering (R0)

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