Experimental Investigation of Air and Methane Injection from In-Stream Fueling Pylons (POSTPRINT)

Abstract

This paper covers experimental results for in-stream fuel injectors in a Mach number 1.95 airflow. Three fuel injection pylon configurations studied include a basic pylon, a ramp pylon, and an alternating wedge pylon. The first pylon is a baseline configuration. The latter two introduce streamwise vorticity into the flow to increase mixing action via their trailing edge geometries. A cold flow study with fuel injection is accomplished to compare the three pylons mixing capabilities and pressure losses. Three experimental techniques are used: aerothermal probing, Raman spectroscopy, and nitric-oxide planar laser induced fluorescence (NO-PLIF). Aerothermal probing and NO-PLIF are accomplished with air injection from the pylons, while Raman spectroscopy is accomplished with methane injection. The ramp and alternating wedge pylons show decisive increases in mixing capability compared with the basic pylon. They also exhibit a slight increase in total pressure loss compared with the basic pylon.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 2008
Accession Number
ADA532865

Entities

People

  • Campbell D. Carter
  • Jason C. Doster
  • Kuang-yu Hsu
  • Mark R. Gruber
  • Michael D. Ryan
  • Paul I. King

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Air Platforms
  • Space

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Air Force Research Laboratories
  • Combustion
  • Fluorescence
  • Fuel Injection
  • Fuel Injectors
  • Geometry
  • Injectors
  • Laser Beams
  • Laser Induced Fluorescence
  • Lasers
  • Light Sources
  • Mach Number
  • Raman Spectroscopy
  • Spectroscopy
  • Wind Tunnels

Fields of Study

  • Physics

Readers

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Technology Areas

  • Directed Energy