Accession Number : AD0675134

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

Corporate Author : JOHNS HOPKINS UNIV SILVER SPRING MD APPLIED PHYSICS LAB

Personal Author(s) : Woolard,H. W. ; Cramer,R. H.

Report Date : 28 FEB 1958

Pagination or Media Count : 27

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)

Descriptors :   (*REENTRY VEHICLES, AERODYNAMIC HEATING), HEAT TRANSFER, SURFACE TEMPERATURE, COOLING, BODIES OF REVOLUTION, ATMOSPHERE ENTRY, FLAT PLATE MODELS, ANGLE OF ATTACK, HYPERSONIC CHARACTERISTICS, SUPERSONIC CHARACTERISTICS, SUBSONIC CHARACTERISTICS, TURBULENT BOUNDARY LAYER, FLOW FIELDS, PRANDTL NUMBER, MATHEMATICAL PREDICTION, ATMOSPHERE MODELS, ENTHALPY, BAROMETRIC PRESSURE

Subject Categories : Guided Missiles
      Thermodynamics

Distribution Statement : APPROVED FOR PUBLIC RELEASE