Near-Wall Velocity Field Measurements of a Very Low Momentum Flux Transverse Jet (Briefing Charts)

Abstract

Transverse jets have been the subject of study for several decades due to their relevance in a number of flows in nature and engineering applications. The momentum flux ratio between the jet and crossflow is generally considered to be the leading independent parameter, and has been explored extensively over a nominal range from unity to several hundred. The current study considers the flow field of a transverse jet at momentum flux ratios much smaller than unity. A modulated absorption/emission thermometry technique under development at AFRL requires a narrow film barrier to maintain a clean optical access window, while limiting the transverse penetration of the jet into the crossflow to avoid corruption of the optical measurement. The current effort examined the near field behavior of very low momentum flux ratio transverse jets to elucidate the jet and crossflow interactions. Under low momentum flux ratio conditions, the crossflow has sufficient local momentum near the injection location, exceeding that of the jet, which leads to crossflow ingestion. It was expected that reduced area and consequent increase in mean jet velocity would increase the effective momentum flux ratio which would lead to increased momentum flux and penetration into the crossflow. However, the complex 3-dimensional interaction between the jet and crossflow suggests penetration is far reduced for these very low momentum flux ratio cases. Particle image velocimetry was used to investigate the jet and cross flow interactions near the jet exit over a range of low momentum flux ratios, 0.0013 < or = J < or = 0.075. A fully developed laminar jet was injected into a fully developed turbulent channel crossflow. The two lowest momentum flux ratio cases were found to penetrate the least into the crossflow with regard to mean behavior of the jet.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 2014
Accession Number
ADA618196

Entities

People

  • David J. Forliti
  • David V. Salazar
  • Edward Coy
  • Kalya Kuzmich

Organizations

  • Air Force Research Laboratory

Tags

DTIC Thesaurus Topics

  • Abstracts
  • Air Force
  • Air Force Research Laboratories
  • Cross Flow
  • Department Of Defense
  • Film Cooling
  • Flow
  • Frequency Domain
  • Light Sources
  • Military Research
  • Momentum
  • Particle Image Velocimetry
  • Shear Stresses
  • Stratified Fluids
  • Stresses
  • Three Dimensional
  • Transverse

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Fluid Mechanics and Fluid Dynamics.