Variable-Area Ejector Development

Abstract

An experimental investigation was conducted to determine the performance of a variable-area ejector. Test equipment consisted of various fixed-geometry primary driving nozzles and either a constant-area or a conical- converging mixing duct attached to a conical-diverging exit section, which was equipped with a conical centerbody. Axial movement of the conical centerbody varied the minimum area of the ejector. Five primary driving nozzle geometries were used. Both steady-state and transient performance characteristics of the ejector configurations are presented. A constant-area (no centerbody) ejector having a diameter equivalent to that of the variable-area ejector mixing duct was also evaluated. In general, the performance of the variable-area ejector configuration exceeded that of the constant-area ejector.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1976
Accession Number
ADA028977

Entities

People

  • David Duesterhaus
  • Delbert Taylor
  • Frank Lee
  • Marvin Simmons

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Energy and Power Technologies
  • Space

DTIC Thesaurus Topics

  • Air Force
  • Air Supplies
  • Engineering
  • Exhaust Gases
  • Exhaust Nozzles
  • Exhaust Systems
  • Gas Turbines
  • Jet Engines
  • Mach Number
  • Propulsion Systems
  • Recording Systems
  • Stagnation Pressure
  • Test Facilities
  • Turbines
  • Turbofan Engines
  • Turbojet Engines
  • United States

Readers

  • Combustion and Flow Dynamics.