A Preliminary Review in the Application of Hot-Wire Anemometry to the Study of Repeated Shock Waves

Abstract

The feasibility of using a hot-wire anemometer as a means of examining the complex flow field associated with repeated plane shock waves in a shock tube is investigated. The limitations inherent in this study and the variables that must be accounted for are considered. A criterion is established for the determination of the presence of significant acoustical streaming. A method for measuring peak alternating velocities is postulated. Experimental results show good agreement with theory except for the alternating boundary layer which is apparently not an example of simple shear flow.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1960
Accession Number
AD0845921

Entities

People

  • Charles L. Teevan
  • Philip G. Charest

Organizations

  • Naval Postgraduate School

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Compressors
  • Boundaries
  • Boundary Layer
  • Equations
  • Fibers
  • Flow
  • Frequency
  • Heat Energy
  • Hot Wire
  • Hot Wire Anemometers
  • Layers
  • Measurement
  • Shock Waves
  • Tubes
  • Two Dimensional
  • United States
  • Waves

Fields of Study

  • Physics

Readers

  • Fluid Mechanics and Fluid Dynamics.
  • Systems Analysis and Design