Accession Number : AD0739864
Title : Similar Solutions of the Three Dimensional Boundary Layer with Constant Cross Flow,
Corporate Author : AEROSPACE RESEARCH LABS WRIGHT-PATTERSON AFB OHIO
Personal Author(s) : Christian,James W.
Report Date : NOV 1971
Pagination or Media Count : 103
Abstract : Governing equations are formulated for laminar compressible similar boundary layers with heat transfer, adverse pressure gradient, and constant cross flow. These equations are expressed in finite difference form and solved numerically. Solutions are found for attached and separated flows in adverse pressure gradients for nine combinations of cross flow and heat transfer. The purpose of these solutions is to provide understanding of how cross flow alters the two-dimensional similar results. Solutions are presented in the form of temperature profiles, main flow and cross flow velocity profiles, and global quantities; wall velocity and temperature gradients, displacement thickness, momentum thicknesses, and form factor.
Descriptors : (*LAMINAR BOUNDARY LAYER, MATHEMATICAL ANALYSIS), EQUATIONS OF MOTION, COMPRESSIBLE FLOW, HEAT TRANSFER, FLOW SEPARATION, THREE DIMENSIONAL FLOW, KINETIC ENERGY, PRESSURE, STAGNATION POINT
Subject Categories : Fluid Mechanics
Distribution Statement : APPROVED FOR PUBLIC RELEASE