Accession Number : AD0493180
Title : DEVELOPMENT OF HIGH SPEED AERODYNAMIC HEAT TRANSFER COEFFICIENTS FOR FLAT PLATES AND CONES,
Corporate Author : ARMY MISSILE RESEARCH DEVELOPMENT AND ENGINEERING LAB REDSTONE ARSENAL AL AER OBALLISTICS DIRECTORATE
Personal Author(s) : Johnson, Lloyd H. ; Lowry, W. E.
Report Date : 11 JUL 1963
Pagination or Media Count : 30
Abstract : The boundary layer on a flat plate for laminar and turbulent flow with an analysis of a current method to calculate aerodynamic heat transfer coefficients are presented. Specific heat variations of gas with temperatures up to dissociation are included with the aerodynamic heat transfer coefficient in a transient temperature digital program. The boundary layer and aerodynamic heat transfer coefficients developed for a flat plate may be applied to cone surfaces with the correction factors indicated in this report. (Author)
Descriptors : *FLAT PLATE MODELS), (*AERODYNAMIC HEATING, MATHEMATICAL MODELS, HYPERSONIC CHARACTERISTICS, SKIN FRICTION, DRAG, LAMINAR BOUNDARY LAYER, TWO DIMENSIONAL FLOW, INCOMPRESSIBLE FLOW, TURBULENT BOUNDARY LAYER, SHEAR STRESSES, TURBULENCE, HEAT TRANSFER, COMPUTER PROGRAMMING, CONICAL BODIES, BOUNDARY LAYER.
Subject Categories : Fluid Mechanics
Distribution Statement : APPROVED FOR PUBLIC RELEASE