A Study on the Hydrogen-Oxygen Diffusion Flame in High Speed Flow

Abstract

A new type of apparatus was adapted to the study on the diffusion flame in high speed flow with the use of a shock tube/detonation tube combination. The flows behind the incident shock wave propagating into O2-Ar mixture and the burned gas behind the detonation wave traveling into a fuel-rich H2-O2-Ar mixture were used to produce a fuel flow and an oxidizer flow respectively. The burned gas was issued through a nozzle in parallel to the oxidizer flow and two-dimensional flow field was established at the test section of the shock tube. The process from the starting of the flows to the formation of a diffusion flame was investigated by the pressure measurements in both tubes and by schlieren and interferometric photography. Also the ignition distances of the diffusion flames in quasi-steady state were measured from direct photography. As a result, a detonation tube was shown to be a useful device for producing a high speed and high temperature flow and it was confirmed that the ignition distance is greatly influenced by both velocity difference and hydrogen concentration.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1981
Accession Number
ADP000311

Entities

People

  • H. Kawada
  • S. Takahashi
  • T. Minegishi
  • Y. Yoshizawa

Organizations

  • Tokyo Institute of Technology

Tags

Communities of Interest

  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Combustion
  • Compression Waves
  • Detonation Waves
  • Flow Fields
  • Gas Flow
  • High Temperature
  • Ignition
  • Mechanical Engineering
  • Photographs
  • Photography
  • Pressure Measurement
  • Shock Tubes
  • Shock Waves
  • Steady Flow
  • Steady State
  • Supersonic Combustion
  • Supersonic Combustion Ramjet Engines

Readers

  • Combustion and Flow Dynamics.
  • Plasma Physics / Magnetohydrodynamics
  • Rocket Propulsion.