Accession Number : AD0753046
Title : Study of Heat Exchange and Drag during a Turbulent Flow of Compressible Gas,
Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Personal Author(s) : Zysina-Molozhen,L. M. ; Soskova,I. N.
Report Date : 27 NOV 1972
Pagination or Media Count : 23
Abstract : A study was made of a two layered model of a compressed turbulent boundary layer with heat exchange. A temperature profile was determined from the Crocco integral; for the velocity profile in the turbulent part of the layer a Van-Drist profile was used. The distinguishing feature of the solution is dependence of the dimensionless width of the laminar sub-layer on the temperature factor and the Mach number. Results of the calculations are compared with experiments on friction and heat exchange.
Descriptors : (*TURBULENT BOUNDARY LAYER, *HEAT TRANSFER), COMPRESSIBLE FLOW, PRANDTL NUMBER, MATHEMATICAL MODELS, LAMINAR FLOW, VELOCITY, EQUATIONS OF MOTION, EXPERIMENTAL DATA, FLAT PLATE MODELS, DRAG, USSR
Subject Categories : Fluid Mechanics
Distribution Statement : APPROVED FOR PUBLIC RELEASE