Performance of Multiple Nozzle Eductor Systems with Several Geometric Configurations.

Abstract

Cold flow tests of a four nozzle eductor system were conducted to evaluate the system's performance with the following geometric modifications: changing the area ratio of the mixing stack to primary flow nozzles from 3.0 to 2.5; adding a solid diffusor to the exit of the mixing stack; adding two- and three-ring diffusors to the exit of the mixing stack; adding film cooling ports along the length of the mixing stack; and combining the effects of film cooling ports, a two-ring diffusor and a shroud. Non-dimensional parameters governing the flow phenomena are developed from a one-dimensional analysis of a simple eductor system based on the conservation of momentum for an incompressible gas. The eductor performance is evaluated in terms of these non-dimensional parameters. Within the range of modifications considered, the configuration with the film cooling ports, shroud and two diffusor rings provided the best overall eductor system performance. (Author)

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1978
Accession Number
ADA061278

Entities

People

  • Christopher Paul Staehli
  • Robert James Lemke

Organizations

  • Naval Postgraduate School

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Ground and Sea Platforms

DTIC Thesaurus Topics

  • Air Flow
  • Back Pressure
  • Computational Fluid Dynamics
  • Creep
  • Engineering
  • Fluid Dynamics
  • Geometry
  • Instrumentation
  • Lepidoptera
  • Mach Number
  • Measurement
  • Mechanical Engineering
  • Mechanics
  • Pressure Distribution
  • Schools
  • United States
  • United States Naval Academy

Readers

  • Combustion and Flow Dynamics.