Fluidic Combustion Control of a Ramjet.

Abstract

The patent application relates to a method of fluidic combustion control of a ramjet by injecting a fluid into the base or recirculation region to reduce the critical injection parameter, or to shut down the ramjet without affecting the hot air flow.

Document Details

Document Type
Technical Report
Publication Date
Jul 06, 1976
Accession Number
ADD003152

Entities

People

  • Allen L. Holzman

Organizations

  • United States Department of the Navy

Tags

DTIC Thesaurus Topics

  • Air Flow
  • Chemical Reactions
  • Combustion
  • Exothermic Reactions
  • Flow
  • Fluid Flow
  • Patent Applications
  • Patents

Fields of Study

  • Physics

Readers

  • Electrical Engineering
  • Fluid Mechanics and Fluid Dynamics.
  • Internal Combustion Engine (ICE) Technology.