Basic Instability Mechanisms in Chemically Reacting Subsonic and Supersonic Flows.

Abstract

The nature of turbulence-combustion interactions was examined by the use of simultaneous dual-thermocouple velocity and LDV-thermocouple measurements, which showed that the presence of the high-frequency velocity (in a direction normal to the flame brush) and temperature fluctuations within slowly drifting turbulent premixed V-flames was associated with changes in the flame shapes, thicknesses, and propagation speeds. Unlike the RMS normal-velocity fluctuations which assumed maximum values within the reaction zone, the RMS tangential-velocity fluctuations remained almost constant, implying that the flame-generated turbulence was in the normal direction. Furthermore, cross-correlation coefficients of simultaneous velocity and temperature fluctuations remained positive within the flame, with values involving normal velocities higher than those involving tangential components. Keywords: Turbulence, Combustion interactions, Instability mechanisms, Dist turbulent flames.

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Document Details

Document Type
Technical Report
Publication Date
Oct 23, 1987
Accession Number
ADA190101

Entities

People

  • Tau-yi Toong

Organizations

  • Massachusetts Institute of Technology

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Availability
  • Classification
  • Coefficients
  • Combustion
  • Cross Correlation
  • Flames
  • Flow
  • Frequency
  • Instability
  • Intervals
  • Measurement
  • Regions
  • Security
  • Standards
  • Supersonic Flow
  • Temperature Gradients
  • Time Intervals

Fields of Study

  • Physics

Readers

  • Atmospheric Science / Meteorology, specifically Wind Wave Turbulence.
  • Combustion science or combustion engineering.

Technology Areas

  • Hypersonics