Investigation of Jet Transition Phenomena

Abstract

The experimental investigation examines jet phenomena, gaseous and liquid, in small submerged and bounded jets. Its general objectives are to acquire experimental data and to develop mathematical expressions for predicting the behavior of fluidic elements and designs. Data are presented for circular nozzles of 0.25 to 4.6 mm and square nozzles of 0.5 to 1.0 mm, observed by Schlieren and Birefringent flow techniques at low Reynolds numbers compatible with miniature fluidic designs. Good correlation between compressible and incompressible flow is obtained. Three principal nondimensional terms are used to evaluate and correlate experimental results. They are Reynolds number, transition number (a relationship of nozzle diameter and length of laminar flow), and momentum number (represented the interaction of two jets). Three sets of tests are described. One measures the transition from laminar flow to turbulence in single submerged jets. The second introduces a secondary jet flow to determine its effect upon transition and deflection of the primary jet. The third involves variations of nozzle geometry commonly used in fluidic elements: sidewall divergence, sidewall setback and reinjection curvature. These geometries provide feedback paths and reflecting surfaces, allowing the jet to produce premature transition. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1968
Accession Number
AD0671977

Entities

People

  • C. P. Mckenzie
  • D. B. Wall

Organizations

  • Martin Marietta

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Space

DTIC Thesaurus Topics

  • Amplifiers
  • Compressible Flow
  • Corporations
  • Curvature
  • Diameters
  • Energy Consumption
  • Experimental Data
  • Flow
  • Fluid Dynamics
  • Fluidic Amplifiers
  • Fluidic Devices
  • Geometry
  • Incompressible Flow
  • Jet Flow
  • Laminar Flow
  • Reynolds Number
  • Secondary Injection

Fields of Study

  • Physics

Readers

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