Accession Number : AD0615471
Title : THE EFFECTS OF ACTIVE COOLING ON THE AERODYNAMIC AND AEROTHERMODYNAMIC CHARACTERISTICS OF SLENDER BODIES OF REVOLUTION.
Descriptive Note : Final rept.,
Corporate Author : GENERAL DYNAMICS/CONVAIR SAN DIEGO CALIF
Personal Author(s) : Leadon,B. M. ; Rosciszewski,Jan. ; Gallaher,W. H. ; Holst,W. R. ; Carter,W. V.
Report Date : NOV 1964
Pagination or Media Count : 102
Abstract : A new self consistent method has been developed for calculation of boundary layer with mass injection. The system of partial differential equations is reduced to a system of ordinary differential equations by integration over different strips. The velocity and enthalpy profiles are assumed to be expressed by series of error functions. A method of calculating the initial velocity and enthalpy profiles, based on an analysis of singularity, is presented herein. The calculation of the initial profiles is reduced to the solution of a system of transcendential equations. The initial derivatives are calculated from linearlized equations near the singular points and provide a smooth start of integration of the downstream equations. The present method was applied to the cases of a sharp edged body and a blunt body. In addition to the velocity and enthalpy profiles, the pressure distribution and shock layer thickness can be calculated from generalized Newtonian expressions developed as a part of this effort. (Author)
Descriptors : (*AERODYNAMIC CHARACTERISTICS, SLENDER BODIES), (*SLENDER BODIES, AERODYNAMIC CHARACTERISTICS), THERMODYNAMICS, COOLING, BOUNDARY LAYER, BLUNT BODIES, FLUID FLOW, VELOCITY, PARTIAL DIFFERENTIAL EQUATIONS, DIFFERENTIAL EQUATIONS, NUMERICAL INTEGRATION, NUMERICAL ANALYSIS, ENTHALPY, EQUATIONS
Distribution Statement : APPROVED FOR PUBLIC RELEASE