EQUILIBRIUM SURFACE TEMPERATURE RESULTING FROM AERODYNAMIC HEATING AND RADIANT COOLING FOR TURBULENT-BOUNDARY-LAYER FLOW OVER A FLAT PLATE,

Abstract

The approximate equilibrium surface temperature resulting from aerodynamic heating and radiant cooling is calculated for turbulent-boundary-layer flow over a flat plate at zero angle of attack and moving at a constant Mach number. (Author)

Document Details

Document Type
Technical Report
Publication Date
Feb 28, 1958
Accession Number
AD0675134

Entities

People

  • H. W. Woolard
  • R. H. Cramer

Organizations

  • Johns Hopkins University Applied Physics Laboratory

Tags

DTIC Thesaurus Topics

  • Aerodynamic Heating
  • Boundaries
  • Boundary Layer
  • Boundary Layer Flow
  • Cooling
  • Flow
  • Heating
  • Layers
  • Mach Number
  • Radiant Cooling
  • Surface Temperature
  • Turbulent Boundary Layer

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Combustion and Flow Dynamics.
  • Image Processing and Computer Vision.