Accession Number : AD0774726
Title : An Investigation of Hypersonic Viscous Merged Flow.
Descriptive Note : Final rept. 1 Oct 66-30 Sep 73,
Corporate Author : OHIO STATE UNIV COLUMBUS DEPT OF AERONAUTICAL AND ASTRONAUTICAL ENGINEERING
Personal Author(s) : Li,Ting Y.
Report Date : NOV 1973
Pagination or Media Count : 55
Abstract : The report deals with the hypersonic Rayleigh problem. The exact Navier-Stokes equations are used in the formulation. The perfect gas model with gamma and sigma constant ratio of specific heats and Prandtl number, respectively is assumed. The case of an insulated plate under impulsive motion at a limiting hypersonic Mach number is considered. Numerical solutions based on an explicit scheme and a Crank-Nicolson scheme have been obtained within the hypersonic viscous merged layer over the plate surface. These numerical results are compared with existing analytical and empirical results. Difficulties encountered in the numerical calculations and their remedies are briefly outlined. (Modified author abstract)
Descriptors : *Viscous flow, *Hypersonic characteristics, *Flat plate models, Numerical methods and procedures, Mathematical models, Boundary layer, Equations of motion, Mixing, Computer programming, Dynamic pressure
Subject Categories : Fluid Mechanics
Distribution Statement : APPROVED FOR PUBLIC RELEASE