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