Accession Number : AD0708162

Title :   COMPRESSIBLE TURBULENT PLANE COUETTE FLOW WITH VARIABLE WALL TEMPERATURE.

Descriptive Note : Final rept.,

Corporate Author : AEROSPACE RESEARCH LABS WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Korkegi,Robert H. ; Briggs,Ronald A.

Report Date : MAR 1970

Pagination or Media Count : 27

Abstract : Equations describing compressible turbulent plane Couette flow for the general case of arbitrary wall enthalpy have been developed for a perfect gas based on the von Karman mixing length model. The procedure used was to obtain the velocity distribution near each wall and determine the matching point of the two profiles by the requirement that the velocities and their slopes must be equal at this point. Sample results are given in terms of the influence of heat transfer on velocity, enthalpy, and skin-friction distributions. (Author)

Descriptors :   (*COUETTE FLOW, THERMAL ANALYSIS), COMPRESSIBLE FLOW, TURBULENT BOUNDARY LAYER, TEMPERATURE, HEAT TRANSFER

Subject Categories : Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE