The Effect of Hole Geometry on the Near Field Character of Crossflow Jets

Abstract

Water tunnel experiments were conducted to understand the effect of hole exit geometry on the lift-off characteristics of crossflow jets. Six basic hole shapes were investigated, all having the same cross-sectional area: round, elliptical, square, and rectangular. Laser Induced Fluorescence (LIF) and Particle Image Velocimetry (PIV) were used to visualize the jet structures near the hole, and acquire velocity and vorticity field information, respectively. The flow visualization pictures, and PIV data images, graphs, and vector plots' complement each other to provide a deeper understanding of the basic make-up of the kidney-vortices that are present in a crossflow jet. The vorticity around the circumference of the jet was tracked using LIF and PIV to understand the relative contributions to the kidney-vortices. The jet side-wall boundary layer is responsible for the primary kidney vortex structures. These vortices result from the roll-up of the side-wall boundary layer as the jet exits the hole. Here, hole geometry alone was found to have a distinct influence on the lift-off behavior by affecting the lateral separation of these side-wall vortices.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1996
Accession Number
ADA311883

Entities

People

  • Brenda A. Haven

Organizations

  • Air Force Institute of Technology

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Argon Lasers
  • Boundary Layer
  • Cameras
  • Flow Visualization
  • Fluid Dynamics
  • Fluid Flow
  • Fluid Mechanics
  • Gas Turbines
  • Geometry
  • Heat Transfer
  • Near Field
  • Pressure Distribution
  • Secondary Flow
  • Stagnation Point
  • Turbines
  • Turbulent Mixing
  • Two Dimensional

Fields of Study

  • Physics

Readers

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

Technology Areas

  • Directed Energy