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Hybrid Code Development for the Numerical Simulation of Instationary Magnetoplasmadynamic Thrusters

In: High Performance Computing in Science and Engineering '08

Author

Listed:
  • M. Fertig

    (Universität Stuttgart, Institut für Raumfahrtsysteme, Abt. Raumtransporttechnologie)

  • D. Petkow

    (Universität Stuttgart, Institut für Raumfahrtsysteme, Abt. Raumtransporttechnologie)

  • T. Stindl

    (Universität Stuttgart, Institut für Raumfahrtsysteme, Abt. Raumtransporttechnologie)

  • M. Auweter-Kurtz

    (Universität Hamburg)

  • M. Quandt

    (Universität Stuttgart, Institut für Aerodynamik und Gasdynamik)

  • C.-D. Munz

    (Universität Stuttgart, Institut für Aerodynamik und Gasdynamik)

  • J. Neudorfer

    (Höchstleistungsrechenzentrum Stuttgart)

  • S. Roller

    (Höchstleistungsrechenzentrum Stuttgart)

  • D. D’Andrea

    (Institut für Hochleistungsimpuls- und Mikrowellentechnik, Forschungszentrum)

  • R. Schneider

    (Institut für Hochleistungsimpuls- und Mikrowellentechnik, Forschungszentrum)

Abstract

Summary This paper describes the numerical modeling of rarefied plasma flows under conditions where continuum assumptions fail. We numerically solve the Boltzmann equation for rarefied, non-continuum plasma flows, making use of well known approaches as PIC (Particle in Cell) and as DSMC (Direct Simulation Monte Carlo). The mathematical and numerical modeling is explained in some detail and the required computational resources are investigated.

Suggested Citation

  • M. Fertig & D. Petkow & T. Stindl & M. Auweter-Kurtz & M. Quandt & C.-D. Munz & J. Neudorfer & S. Roller & D. D’Andrea & R. Schneider, 2009. "Hybrid Code Development for the Numerical Simulation of Instationary Magnetoplasmadynamic Thrusters," Springer Books, in: Wolfgang E. Nagel & Dietmar B. Kröner & Michael M. Resch (ed.), High Performance Computing in Science and Engineering '08, pages 585-597, Springer.
    • Handle: RePEc:spr:sprchp:978-3-540-88303-6_40
    DOI: 10.1007/978-3-540-88303-6_40
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