Section 10

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Zur gasdynamischen Auslegung eines Stosswellenkanals

  1. Katrin Schemperg*,
  2. Christian Mundt*

Article first published online: 13 DEC 2004

DOI: 10.1002/pamm.200410194

Issue

PAMM

PAMM

Volume 4, Issue 1, pages 426–427, December 2004

Additional Information

How to Cite

Schemperg, K. and Mundt, C. (2004), Zur gasdynamischen Auslegung eines Stosswellenkanals. Proc. Appl. Math. Mech., 4: 426–427. doi: 10.1002/pamm.200410194

Author Information

  1. Institut für Thermodynamik, Universität der Bundeswehr München, 85577 Neubiberg, Deutschland

*Phone: +49 89 6004 2102, Fax: +49 89 6004 2116

Publication History

  1. Issue published online: 13 DEC 2004
  2. Article first published online: 13 DEC 2004

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Literatur

  • [1]
    Hornung, H.: High Enthalpy Facilities,The third joint Europe/US short course in hypersonics at RWTH Aachen, Oktober 1990.
  • [2]
    Hornung, H.: Performance data of the new free-piston shock tunnel at GALCIT, Graduate Aeronautical Laboratories, California Institute of Technology, AIAA 92-3943, 1992.
  • [3]
    Itoh, K., Ueda, S., Komuro, T., Sato, K., Takahashi, M., Miyajima, H., Tanno, H., Muramato, H.: Improvement of a free piston driver for a high-enthalpy shock tunnel, National Aerospace Laboratory, Kakuda Research Center, Japan, AIAA 0215-0233, 1997.
  • [4]
    Jacobs, P. A.: Shock Tube Modelling with L1d, Research Report 13/98, Department of Mechanical Engineering, The University of Queensland, November 1998.
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