• V. Yu Kolosov
  • V. Yu Sepman
  • V. S. Sukhomlinov
  • Yu A. Tohuache
  • A. L. Kuranov
  • V. V. Kuchiusky
  • V. A. Sheverev
  • M. V. Otugen

In this report, a dispersion relation for sound wave in a uniform, low ionization plasma is derived from the plasma hydrodynamic equations. From this relation, the properties of a shock wave travelling in a glow discharge are evaluated and compared with previous experimental results. The present results show that a small acoustic dispersion can cause the broadening of the shock wave and the formation of a complex density structure downstream of the wave. The calculations of the density distribution in front of and behind a shock wave are in good qualitative agreemenwt ith that previously measured across a shock wave travellmg through a glow discharge.

Original languageEnglish
Title of host publication9th International Space Planes and Hypersonic Systems and Technologies Conference
PublisherThe American Institute of Aeronautics and Astronautics
StatePublished - 1999
Event9th International Space Planes and Hypersonic Systems and Technologies Conference, 1999 - Norfolk, United States
Duration: 1 Nov 19994 Nov 1999

Conference

Conference9th International Space Planes and Hypersonic Systems and Technologies Conference, 1999
Country/TerritoryUnited States
CityNorfolk
Period1/11/994/11/99

    Scopus subject areas

  • Space and Planetary Science
  • Control and Systems Engineering
  • Aerospace Engineering

ID: 9653942