Friction, Heat Exchange, and Removal of Material in the Turbulent Boundary Layer oa a Compressible High-Enthalpy Gas in Conditions of Essential Nonisothermicity, Blowing, and Negative Pressure Gradient,

Abstract

The report develops a numerical method for determining the ablative characteristic of a rocket motor nozzle liner.

Document Details

Document Type
Technical Report
Publication Date
Oct 29, 1973
Accession Number
AD0770006

Entities

People

  • E. G. Zaulichnyi

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Enthalpy
  • Friction
  • Layers
  • Materials
  • Pressure Gradients
  • Rocket Engines
  • Rockets
  • Turbulent Boundary Layer

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Neurotrauma and Rehabilitation Medicine.