Accession Number : AD0778306
Title : Measurements of a Supersonic Favorable-Pressure-Gradient Turbulent Boundary Layer with Heat Transfer. Part 1. Data Compilation.
Descriptive Note : Technical rept.,
Corporate Author : NAVAL ORDNANCE LAB WHITE OAK MD
Personal Author(s) : Voisinet,Robert L. P. ; Lee,Roland E.
Report Date : 12 DEC 1973
Pagination or Media Count : 124
Abstract : The results of a detailed experimental investigation of the compressible turbulent boundary layer in a favorable-pressure-gradient flow are presented for zero, moderate and severe heat-transfer conditions. The studies were conducted on a flat nozzle wall at momentum thickness Reynolds numbers from 6,700 to 56,000 and at three wall-to-adiabatic-wall temperature ratios. An attempt was made to hold values of Clauser's pressure-gradient parameter constant. Complete profile measurements were taken with Pitot pressure probes and conical-equilibrium and fine-wire temperature probes. (Modified author abstract)
Descriptors : *Turbulent boundary layer, *Supersonic characteristics, *Pressure gradients, Heat transfer, Compressible flow, Nozzles, Walls, Test methods, Wind tunnel tests, Data processing
Subject Categories : Fluid Mechanics
Distribution Statement : APPROVED FOR PUBLIC RELEASE