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Numerical Simulation of Combustion Dynamics at ISTA/JAXA

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High-Performance Computing (ISHPC 2005, ALPS 2006)

Part of the book series: Lecture Notes in Computer Science ((LNTCS,volume 4759))

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Abstract

This paper briefly reviews recent numerical combustion simulation results at ISTA/JAXA obtained by DNS and LES approaches, and shows some topics towards future combustion research. We have successfully simulated detailed structures of a hydrogen jet lifted flame by DNS and an unsteady combustor flow field in a gas turbine combustor by LES. In these simulations, numerical simulation has been proved very effective, but its applicability is still limited due to long computational time. It is expected that future progress in computer performance will make this kind of simulation more realistic and useful in combustion research and development.

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Authors and Affiliations

  1. Institute of Space Technology and Aeronautics (ISTA), Japan Aerospace Exploration Agency (JAXA), 7-44-1 Jindaiji-higashimachi, Chofu, Tokyo, 182-8522, Japan

    Junji Shinjo, Shingo Matsuyama, Yasuhiro Mizobuchi & Satoru Ogawa

Authors
  1. Junji Shinjo
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  2. Shingo Matsuyama
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  3. Yasuhiro Mizobuchi
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  4. Satoru Ogawa
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Editor information

Jesús Labarta Kazuki Joe Toshinori Sato

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© 2008 Springer-Verlag Berlin Heidelberg

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Shinjo, J., Matsuyama, S., Mizobuchi, Y., Ogawa, S. (2008). Numerical Simulation of Combustion Dynamics at ISTA/JAXA. In: Labarta, J., Joe, K., Sato, T. (eds) High-Performance Computing. ISHPC ALPS 2005 2006. Lecture Notes in Computer Science, vol 4759. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-77704-5_39

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  • DOI: https://doi.org/10.1007/978-3-540-77704-5_39

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-540-77703-8

  • Online ISBN: 978-3-540-77704-5

  • eBook Packages: Computer ScienceComputer Science (R0)

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