Parameters of Electrode Ignition Discharges in Supersonic Propane-Air Flows

Abstract

Effective solution of such aerodynamic problem as fuel ignition in ramjets at supersonic velocities is evidently impossible without an application of plasma technologies. In presented work we expose results of experimental and theoretical investigations of ignition process of supersonic propane-air flows with a help of transversal and longitudinal discharges.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Oct 20, 2003
Accession Number
ADA433246

Entities

People

  • A. P. Ershov
  • I. B. Timofeev
  • N. V. Ardelyan
  • O. S. Surkont
  • S. N. Chuvashev
  • V. A. Chernikov
  • V. A. Levin
  • V. G. Gromov
  • V. L. Bychkov
  • V. M. Shibkov

Organizations

  • Moscow State University

Tags

Communities of Interest

  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Air Flow
  • Charged Particles
  • Combustion
  • Computer Simulations
  • Electric Discharges
  • Electric Power
  • Electrodes
  • Equations
  • Flow
  • Gas Discharges
  • Gas Flow
  • Glow Discharges
  • Ignition
  • Mach Number
  • Measurement
  • Simulations
  • Supersonic Flow

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Rocket Propulsion.
  • Theoretical Analysis.

Technology Areas

  • Hypersonics