Basic Research in Plasma-Enhanced Combustion

Abstract

PLASMA DYNAMICS FOR AEROSPACE APPLICATIONS * RUSSIAN AJAX HYPERSONIC FLIGHT VEHICLE (1994) * THEME OBJECTIVE: Understand, Predict, and Control Weakly Ionized Flows to Revolutionize the Performance of Aerospace Vehicles. RESEARCH * Aerodynamic Drag Reduction * MHD Flow Control * Glow Discharge Flow Control * Plasma Generation * Ignition Combustion Enhancement.

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Document Details

Document Type
Technical Report
Publication Date
Nov 04, 2009
Accession Number
ADA532916

Entities

People

  • Julian Tishkoff

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Energy and Power Technologies
  • Space

DTIC Thesaurus Topics

  • Aerodynamic Drag
  • Aerospace Craft
  • Air Force
  • Air Force Research Laboratories
  • Boltzmann Equation
  • Combustion
  • Combustion Chambers
  • Demographic Cohorts
  • Drag
  • Drag Reduction
  • Dynamics
  • Flow
  • Glow Discharges
  • Hypersonic Flight
  • Hypervelocity Flow
  • Ignition
  • Ignition Lag

Fields of Study

  • Physics

Readers

  • Defense Technology Research and Development.
  • Fluid Dynamics.
  • Pulsed Power and Plasma Physics.

Technology Areas

  • Hypersonics
  • Space
  • Space - Hall-Effect Thruster
  • Space - Spacecraft Maneuvers