Measurements in the Turbulent Boundary Layer at Constant Pressure in Subsonic and Supersonic Flow. Part 2. Laser-Doppler Velocity Measurements

Abstract

Experiments have been carried out using laser-Doppler velocimetry in conjunction with Pitot and surface-friction instrumentation for the measurement of the mean flow, the velocity fluctuations, and the Reynolds stresses in turbulent boundary layers at constant pressure in subsonic and supersonic flows. Part I of this work was a detailed analysis of the mean flow as observed using Pitot-tube, Preston-tube, and floating-element balance instrumentation. The present work (Part II) is a description of both the mean and the fluctuating components of the flow, and of the Reynolds stress as observed using a dual forward-scattering laser-Doppler velocimenter. A detailed description of the instrument, and of the data analysis techniques, have been included in order to fully document the data. A detailed comparison is made between the laser-Doppler results and those presented in Part I, and an assessment is made of the ability of the laser-Doppler velocimeter to measure the details of the flows involved.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1979
Accession Number
ADA072016

Entities

People

  • Daniel B. Lang
  • Donald J. Collins
  • Paul E. Dimotakis

Organizations

  • California Institute of Technology

Tags

Communities of Interest

  • Advanced Electronics
  • Air Platforms

DTIC Thesaurus Topics

  • Accuracy
  • Air Force
  • Boundary Layer
  • Data Analysis
  • Data Rate
  • Engineering
  • Equations
  • Free Stream
  • Hydrodynamics
  • Jet Propulsion
  • Mach Number
  • Measurement
  • Particle Flux
  • Particle Size
  • Scattering
  • Turbulent Boundary Layer
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Business Analytics
  • Fluid Dynamics.

Technology Areas

  • Directed Energy
  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flow