Droplet Combustion and Non-Reactive Shear-Coaxial Jets with Transverse Acoustic Excitation

Abstract

This experimental study focused on the coupling of transverse acoustic flow perturbations with two different fundamental phenomena that take place in combustion chambers: droplet combustion, and injection of non-reactive shear-coaxial jets.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 2012
Accession Number
ADA590360

Entities

People

  • Sophonias Teshome

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Energy and Power Technologies
  • Materials and Manufacturing Processes
  • Sensors
  • Weapons Technologies

DTIC Thesaurus Topics

  • Acoustic Waves
  • Acoustics
  • Alcohol Fuels
  • Buoyancy
  • Burning Rate
  • Change Detection
  • Combustion
  • Combustion Chambers
  • Computational Fluid Dynamics
  • Convection
  • Fluid Dynamics
  • Heat Transfer
  • Materials Laboratories
  • Measurement
  • Pressure Measurement
  • Standing Waves
  • Turbulent Mixing

Fields of Study

  • Physics

Readers

  • Combustion science or combustion engineering.
  • Fluid Mechanics and Fluid Dynamics.