EXPERIMENTAL INVESTIGATION OF THE FORMATION OF A GAS JET BEHIND THE FRONT OF A SHOCK WAVE IN THE OUTFLOW OF DIVERGENT AND SUPERSONIC NOZZLES,

Abstract

A shock tube was used in carrying out the investigations. Dimensions of the nozzles used in the experiment are given together with empirical formulas obtained.

Document Details

Document Type
Technical Report
Publication Date
Jul 14, 1966
Accession Number
AD0644046

Entities

People

  • A. I. Starshinov

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Nozzles
  • Shock
  • Shock Tubes
  • Shock Waves
  • Supersonic Nozzles
  • Tubes
  • Waves

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Plasma Physics / Magnetohydrodynamics

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow