MEASUREMENT OF SHOCK WAVE THICKNESS BY THE ELECTRON BEAM FLUORESCENCE METHOD

Abstract

Shock wave thicknesses and density ratios have been measured in helium, argon and nitrogen by means of the electron beam fluorescence method, over the range 1.5 < M < 17.4, in a low density wind tunnel. The shock thickness in argon and helium agreed well with Mott-Smith theory at the higher Mach numbers, and were between NavierStokes and Mott-Smith theory at the lowest Mach number. In nitrogen, the measured shock thicknesses were considerably greater than the predictions of Navier-Stokes theory. Measured density ratios across the shock wave were in good agreement with theory, in the lower density flows. Poorer agreement was found at higher flow densities, leading to estimates of upper bounds for the range of linear variation of fluorescence intensity with gas density. Measured density ratios for shocks produced in divergent free-jet flows were found to be in better agreement with theory after a viscous curvature correction was applied.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1965
Accession Number
AD0466304

Entities

People

  • F. Robben
  • L. Talbot

Organizations

  • University of California, Berkeley

Tags

Communities of Interest

  • Air Platforms
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Abstracts
  • Boundary Layer
  • Contracts
  • Electron Beams
  • Flow
  • Fluid Dynamics
  • Fluid Flow
  • Free Stream
  • Government Procurement
  • Governments
  • Jet Flow
  • Mach Number
  • Measurement
  • Radiation
  • Shock Tubes
  • Shock Waves
  • Wind Tunnels

Fields of Study

  • Physics

Readers

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

Technology Areas

  • Directed Energy
  • Directed Energy - Lasers
  • Microelectronics