THE EFFECT OF VISCOSITY AND HEAT CONDUCTION ON THE FLOW OF A GAS BEHIND A SEVERELY CURVED SHOCK WAVE

Abstract

Formulas are derived for the relation of stagnation temperatures and pressures behind and in front of a shock wave of any shape, taking into account the viscosity and thermal conductivity of a gas. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jan 25, 1962
Accession Number
AD0270763

Entities

People

  • G.a. Lyubimov

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Conductivity
  • Physical Properties
  • Shock
  • Shock Waves
  • Stagnation Temperature
  • Thermal Conductivity
  • Viscosity
  • Waves

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Explosive Engineering.
  • Thermal Physics or Thermal Science.