Accession Number : AD0756242
Title : A Study of Implicit Finite Difference Techniques for Compressible Viscous Flow.
Descriptive Note : Final rept.,
Corporate Author : ULTRASYSTEMS INC IRVINE CALIF
Personal Author(s) : Masson,Bruce S.
Report Date : JAN 1973
Pagination or Media Count : 33
Abstract : The purpose of this contract has been to develop numerical procedures for solving the Navier Stokes equations to study separated flows over wings at transonic speeds and in the near wake of missiles at hypersonic speeds. As a result of this effort a finite difference technique has been developed for the time dependent motion of a viscous compressible gas. The method is intended to permit efficient solution of the equations in both the viscous dominated and inviscid limits.
Descriptors : (*AERODYNAMIC CONTROL SURFACES, *FLOW SEPARATION), WAKE, FLOW FIELDS, COMPRESSIBLE FLOW, VISCOSITY, NUMERICAL METHODS AND PROCEDURES, TRANSONIC CHARACTERISTICS, NAVIER STOKES EQUATIONS, EQUATIONS OF MOTION, SHOCK WAVES, BOUNDARY LAYER
Subject Categories : Aerodynamics
Distribution Statement : APPROVED FOR PUBLIC RELEASE