CALCULATING THERMAL BOUNDARY LAYER IN A FLOW OF COMPRESSIBLE GAS

Abstract

Discussion of method for calculating laminary, transient and turbulent zones of thermal boundary layer when a flow of compressible gas is directed around a surface: translation of Russian article.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Apr 03, 1963
Accession Number
AD0402588

Entities

People

  • L. M. Zysina-molozhen

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Boundaries
  • Boundary Layer
  • Compressible Flow
  • Department Of Defense
  • Experimental Data
  • Flow
  • Foreign Technology
  • Government Procurement
  • Governments
  • Incompressible Flow
  • Layers
  • Pressure Gradients
  • Temperature Gradients
  • Thermal Boundary Layer
  • Translations

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.