A theoretical analysis was carried out studying the formation and propagation of a weak shock wave through a gas with axial temperature gradients. The focus of the study was the shock wave - glow discharge plasma interaction problem. In particular, the thermal gradient effects on the shock structure and speed, caused by the discharge were investigated. First, the equation governing the formation and propagation of a weak shock wave through a non-uniform medium in the absence of energy dissipation has been derived. Next, an approximate analytical solution to the one-dimensional wave propagation equation is established. With this, the effects of axial (longitudinal) temperature gradients on shock wave speed and strength have been investigated. The present results indicate that axial temperature gradients affect both the shock wave speed and its strength. The present analysis was used to reanalyze the experiments of [1] and [2] who studied the effect of glow discharge plasma on shock wave parameters.

Original languageEnglish
Title of host publication9th International Space Planes and Hypersonic Systems and Technologies Conference
PublisherThe American Institute of Aeronautics and Astronautics
Pages1-16
Number of pages16
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: 9654020