Accession Number : AD0776559
Title : Adiabatic Surface Temperature in a Vortex Boundary Layer,
Corporate Author : ARMY FOREIGN SCIENCE AND TECHNOLOGY CENTER CHARLOTTESVILLE VA
Personal Author(s) : Morozov,M. G.
Report Date : 03 DEC 1974
Pagination or Media Count : 8
Abstract : Calculation of temperature reduction of the adiabatic surface in a supersonic, turbulent boundary layer was carried out. It was shown that the temperature reduction is a consequence of the appearance of a chain of vortices in the boundary flow. Comparison of calculated and experimental data gives qualitative agreement.
Descriptors : *Turbulent boundary layer, *Supersonic characteristics, *Temperature, *Vortices, Surface properties, Reduction, Adiabatic conditions, Notch sensitivity, Flat plate models, Translations, USSR
Subject Categories : Fluid Mechanics
Distribution Statement : APPROVED FOR PUBLIC RELEASE