THE ARC JET AS A MEANS OF PRODUCING FULL TEMPERATURE SIMULATION IN A HYPERSONIC WIND TUNNEL (APPLICATION OF A CROSSED FIELD ACCELERATOR)

Abstract

The general concept of using crossed electrostatic and magnetic fields to accelerate the flow of an ionized plasma was investigated experimentally and theoretically. The experimental installation consists of the following units: an air-stabilized arc which serves as the plasma generator, an inlet viewing chamber for velocity measurements, the acceleration section, an outlet viewing chamber, the test section with quartz viewing window, and finally the vacuum system. The experimental effort consists in correlating the input and output accelerator velocity and Mach number with the applied electromagnetic fields, mass flow, and gross operating parameters of the installation. The theoretical results of the one-dimensional, steady, compressible flow treatment of the problem are presented. These results are summarized in the form of nondimensional charts which display the role of the relevant nondimensional groups that enter into the interaction. These charts readily establish the performance limits of such an accelerator. (Author)

Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1961
Accession Number
AD0269206

Entities

People

  • P.j. Dickerman
  • R.m. Krupa

Tags

DTIC Thesaurus Topics

  • Compressible Flow
  • Electromagnetic Fields
  • Flow
  • Generators
  • Hypersonic Wind Tunnels
  • Mach Number
  • Magnetic Fields
  • Mass Flow
  • Plasma Generators
  • Simulations
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Plasma Physics.
  • Pulsed Power and Plasma Physics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow