Accession Number : AD0719535
Title : The Incompressible Laminar Boundary Layer over a Slender Body of Revolution at Small Incidence.
Descriptive Note : Aeronautical rept.,
Corporate Author : NATIONAL AERONAUTICAL ESTABLISHMENT OTTAWA (ONTARIO)
Personal Author(s) : Nonweiler,T. R. F.
Report Date : APR 1970
Pagination or Media Count : 40
Abstract : The work investigated the incompressible flow within the boundary layer of a body of revolution at incidence, using slender body theory to describe the inviscid flow field. The calculations were made by digital computer, using adaptive procedures to keep close control of truncation errors. The results obtained confirm previously published expectations of the state of the flow. (Author)
Descriptors : (*SLENDER BODIES, INCOMPRESSIBLE FLOW), (*LAMINAR BOUNDARY LAYER, BODIES OF REVOLUTION), ANGLE OF ATTACK, FLOW FIELDS, NUMERICAL METHODS AND PROCEDURES, DIGITAL COMPUTERS, PERTURBATION THEORY, EQUATIONS OF MOTION, APPROXIMATION(MATHEMATICS), THEORY
Subject Categories : Fluid Mechanics
Distribution Statement : APPROVED FOR PUBLIC RELEASE