The interaction of a microwave-generated plasma with a hemisphere cylinder at Mach 2.1 is simulated. The theoretical model is the unsteady threedimensional Euler equations for a multi- species reacting gas. The thermochemistry model for air incorporates 23 species and 238 reactions. The initial condition for the simulation is the steady flow past the hemisphere cylinder.A 9 GHz microwave pulse of 1.2 μs duration is focused upstream of the blunt body shock on the hemisphere cylinder centerline. The high temperature plasma region generated by the microwave pulse is convected to the hemisphere cylinder and interacts with the blunt body shock resulting in the momentary formation of a recirculation region and reduction in surface pressure on the hemisphere cylinder centerline. The computed surface pressure shows good agreement with experiment.

Original languageEnglish
Title of host publicationProceedings of the 6th European Symposium on Aerothermodynamics for Space Vehicles
StatePublished - 17 Jun 2009
Event6th European Symposium Aerothermodynamics for Space Vehicles - Versailles, France
Duration: 3 Nov 20086 Nov 2008

Publication series

NameEuropean Space Agency, (Special Publication) ESA SP
Volume659 SP
ISSN (Print)0379-6566

Conference

Conference6th European Symposium Aerothermodynamics for Space Vehicles
Country/TerritoryFrance
CityVersailles
Period3/11/086/11/08

    Scopus subject areas

  • Aerospace Engineering
  • Space and Planetary Science

    Research areas

  • CFD., Energy deposition, Microwave

ID: 47780436