Initial Results with a Plasma Injection Wake Simulator,

Abstract

Research extending plasma injection techniques for ground simulation of the ionized wakes of re-entry vehicles is reported. In the technique reported a blunt cone model is mounted in a conventional continuous M=4 wind tunnel with a support pylon. Plasma injected from an arc jet located in the model nose flows over the model and forms an ionized wake in the wind tunnel flow. Operating over the altitude range from 100,000 to 140,000 feet, impact pressure and electron density profiles of the ionized wake were obtained. (Modified author abstract)

Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1974
Accession Number
AD0783907

Entities

People

  • Charles W. Haldeman
  • James B. Coffin
  • John I. Cofer

Organizations

  • Massachusetts Institute of Technology

Tags

DTIC Thesaurus Topics

  • Abstracts
  • Altitude
  • Charged Particles
  • Electron Density
  • Electrons
  • Elementary Fermions
  • Elementary Particles
  • Fermions
  • Leptons
  • Simulations
  • Simulators
  • Subatomic Particles
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Fluid Mechanics and Fluid Dynamics.
  • Plasma Physics / Magnetohydrodynamics

Technology Areas

  • Microelectronics