Self-Excited Superturbulence: The Whistler Nozzle

Abstract

The 'whistler nozzle,' consists of a convergent nozzle section, a constant area section, and a step change to an exit section with a larger constant area. The exit section excites a standing acoustic wave in the constant area section, in a way similar to the action of an organ pipe. The result of this resonance is a loud pure tone and a greatly increased rate of jet mixing. The report contains detailed experimental results for the configurations tested. It includes a discussion of several possible applications and suggestions for future experiments aimed at increasing our understanding and improving the performance of the whistler nozzle. Also included is a discussion of the relationship between the vortex nature of subsonic turbulent mixing layers and the differences in turbulent mixing rates for subsonic and supersonic flows.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1974
Accession Number
ADA001021

Entities

People

  • Peter R. Greene
  • William G. Hill Jr.

Organizations

  • Grumman

Tags

Communities of Interest

  • Air Platforms
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Acoustic Waves
  • Aircrafts
  • Boundary Layer
  • Computational Fluid Dynamics
  • Fluid Dynamics
  • Fluid Flow
  • Fluids
  • Frequency
  • Geometry
  • Physics Laboratories
  • Short Takeoff Aircraft
  • Standing Waves
  • Strouhal Number
  • Supersonic Flow
  • Turbulence
  • Turbulent Mixing
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Plasma Physics / Magnetohydrodynamics

Technology Areas

  • Hypersonics