Accession Number : AD0772483

Title :   Measurements of Upstream History Effects in Compressible Turbulent Boundary Layers,

Corporate Author : NAVAL ORDNANCE LAB WHITE OAK MD

Personal Author(s) : Gates,David F.

Report Date : 26 JUL 1973

Pagination or Media Count : 101

Abstract : The report describes an experimental study of compressible turbulent boundary layers for which the upstream history was systematically varied. A series of experiments was conducted using both a supersonic half nozzle and a conventional flat plate for which the nozzle throat and flat plate leading edge can be temperature controlled. The supersonic nozzle provided a favorable upstream pressure gradient together with a controlled thermal history at the throat. The flat plate provided upstream temperature control with no pressure history. Velocity and temperature profile and heat-transfer measurements were made in a downstream region of zero-pressure-gradient and constant wall temperature. (Modified author abstract)

Descriptors :   *Supersonic nozzles, Compressible flow, Turbulent boundary layer, Nozzle throats, Heat transfer, Supersonic flow, Data processing

Subject Categories : Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE