Mixing Effects of Pylon-Aided Fuel Injection Located Upstream of a Flameholding Cavity in Supersonic Flow

Abstract

The Air Force Research Lab (AFRL), Propulsion Directorate, Wright-Patterson Air Force Base, Ohio is conducting ongoing research into propulsive efficiency in supersonic ramjet (scramjet) technology. One current focus of this research is the usefulness of flameholding cavities implemented in the supersonic hydrocarbon-fueled combustion chamber. Because good mixing and proper cavity-core interaction lead to more efficient combustion, methods of optimizing fuel/air mixing both within and upstream the cavity are investigated. In a cooperative effort with the Air Force Institute of Technology (AFIT), AFRL provided a supersonic wind tunnel outfitted with an existing cavity design. A circular injection port was placed upstream of the cavity, and a series of three pylons (medium, tall, wide geometries) were in turn fitted just upstream of the port to improve mixing and penetration of the fuel into the core airflow. The main goals of this experiment were to characterize the mixing ability of injected fuel with the core flow as it propagated downstream of the pylon and to analyze the effects, if any, of this mixing strategy on cavity flow and overall efficiency compared to a no pylon case. The experiment was a non-reacting mixing study. Measurements were obtained from pressure transducers, Planar Laser-Induced Fluorescence (PLIF), and Mie scattering visualization. Of the three pylon geometries tested, the wide pylon provided the best combination of fuel penetration into the freestream (135% increase) and mixing potential. The taller pylon provided more penetration but incurred a large loss penalty. All pylons lifted the fuel from the injector to prevent flashback, and all pylons demonstrated equivalent or better mixing potential than the flat reference at various tunnel conditions.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 2005
Accession Number
ADA434195

Entities

People

  • Daniel R. Montes

Organizations

  • Air Force Institute of Technology

Tags

Communities of Interest

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

DTIC Thesaurus Topics

  • Air Force
  • Boundary Layer
  • Combustion
  • Combustors
  • Computational Fluid Dynamics
  • Fluid Dynamics
  • Geometry
  • Ignition
  • Laser Induced Fluorescence
  • Pressure Measurement
  • Ramjet Engines
  • Supersonic Combustion
  • Supersonic Combustion Ramjet Engines
  • Test Facilities
  • Three Dimensional
  • Turbulent Mixing
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Combustion science or combustion engineering.
  • Fluid Dynamics.

Technology Areas

  • Directed Energy
  • Hypersonics
  • Hypersonics - Hypersonic Flow