Nonstationary Oblique-Shock-Wave Reflection in Nitrogen and Argon: Experimental Results,

Abstract

The interferograms of a detailed study on the reflection of non-stationary oblique shock-waves using a 23 cm dia field of view Mach-Zehnder interferometer and the UTIAS 10 cm by 18 cm Hypervelocity Shock Tube are presented in this separate report.

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1978
Accession Number
ADA068759

Entities

People

  • G. Ben-dor

Organizations

  • University of Toronto

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Accuracy
  • Boundaries
  • Deflection
  • Diffraction
  • Errors
  • Fluid Mechanics
  • Interferograms
  • Mach Number
  • Mach Zehnder Interferometers
  • Mechanics
  • Nitrogen
  • Reflection
  • Shock
  • Shock Tubes
  • Shock Waves
  • Tubes
  • Waves

Fields of Study

  • Physics

Readers

  • Combustion Dynamics and Shock Wave Physics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flow