Unsteady Flows Applicable to Ejector Mechanics,

Abstract

As a result of the size and weight constraints on the application of ejectors to aerospace vehicles, there is a continuing search for improvements to meet those constraints within performance limits. The objective of the present research program is to examine the effect of forced unsteady motions on the mean flow. The specific geometries include fluidically and mechanically driven unsteady jets, airfoils, rearward facing ramps and steps, driven diffusers and the detailed identification of large scale structures in unsteady flows.

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1982
Accession Number
ADP000521

Entities

People

  • David Bougine
  • Hermann Viets
  • Michael Piatt
  • Mont Ball
  • Richard Bethke

Organizations

  • Wright State University

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerospace Craft
  • Airframes
  • Diffusers
  • Flow
  • Fluid Dynamics
  • Fluid Mechanics
  • Geometry
  • Identification
  • Mechanical Structure
  • Mechanics
  • Physics
  • Unsteady Flow
  • Vehicles
  • Workshops

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Combustion and Flow Dynamics.
  • Systems Analysis and Design

Technology Areas

  • Space
  • Space - Hall-Effect Thruster