Accession Number : ADA186631
Title : Generation of Surface Grids through Elliptic Partial Differential Equations for Aircraft and Missile Configurations.
Descriptive Note : Interim rept. Apr 86-Jun 87,
Corporate Author : MISSISSIPPI STATE UNIV MISSISSIPPI STATE DEPT OF AEROPHYSICS AND AEROSPACE EN GINEERING
Personal Author(s) : Warsi, Z U
PDF Url : ADA186631
Report Date : Jul 1987
Pagination or Media Count : 25
Abstract : Numerical solution of the partial differential equations for the generation of surface grids requires a specification of the forcing function which depends on the geometry of the given surface. The data for the surface is usually in discrete form. Methods have been developed which fit a function over the given data. For complicated shapes, e.g., an airplane, the functional fit and the eventual grid generation for the fuselage and wings are done separately and then integrated later. Keywords: Grid generation; Curvilinear coordinates; Numerical methods; Computational fluid dynamics.
Descriptors : *GRIDS(COORDINATES), *PARTIAL DIFFERENTIAL EQUATIONS, AIRCRAFT, COMPUTATIONS, COORDINATES, CURVES(GEOMETRY), ELLIPSES, FLUID DYNAMICS, FUSELAGES, GUIDED MISSILES, LINEAR SYSTEMS, NUMERICAL ANALYSIS, NUMERICAL METHODS AND PROCEDURES, SOLUTIONS(GENERAL), SURFACES, WINGS, FITTING FUNCTIONS(MATHEMATICS)
Subject Categories : Numerical Mathematics
Distribution Statement : APPROVED FOR PUBLIC RELEASE