An Experimental and Theoretical Investigation of Multiple Ducted Streams with a Periodic or a Steady Supersonic Driver Flow.

Abstract

An experimental and theoretical investigation of a supersonic-subsonic, two-dimensional planar, constant area ejector with a periodically pulsed or a steady driver flow is discussed. A large scale fluidic oscillator was developed to partially pulse the driver flow at frequencies up to 250 Hz. A wide range of ejector flow conditions were experimentally investigated with three values of ejector mixing duct length-to-width ratios. Driver flow frequencies of 142 Hz and 250 Hz were used in the ejector experiments and a complete set of steady driver flow experiments was conducted. A one-dimensional, quasi-steady control volume analysis was successfully employed to model these ejector flows. Unsteady ejector flows were found to be modeled well by the quasi-steady analysis. Both steady and unsteady ejector flow performance parameters were accurately predicted by the one-dimensional analysis with the exception of the pressure recovery characteristics observed. Experimentally determined compression ratios were about 25% lower than predicted by the analysis. The pulsation of the driver flow was found to have little effect on ejector operation.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1980
Accession Number
ADA084786

Entities

People

  • A. L. Addy
  • H. L. Petrie

Organizations

  • University of Illinois Urbana–Champaign

Tags

Communities of Interest

  • Air Platforms
  • Cyber
  • Ground and Sea Platforms

DTIC Thesaurus Topics

  • Back Pressure
  • Boundary Layer
  • Computational Fluid Dynamics
  • Energy Transfer
  • Fluid Dynamics
  • Fluidic Oscillators
  • Measurement
  • Mechanical Engineering
  • Pressure Distribution
  • Pressure Gages
  • Pressure Measurement
  • Pressure Transducers
  • Static Pressure
  • Steady Flow
  • Turbulent Mixing
  • Two Dimensional
  • Waveforms

Fields of Study

  • Physics

Readers

  • Combustion Dynamics and Shock Wave Physics.
  • Combustion and Flow Dynamics.
  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow