
Accession Number : AD0708735
Title : TURBULENT MIXING OF SUPERSONIC JETS.
Descriptive Note : Final rept.,
Corporate Author : AEROSPACE RESEARCH LABS WRIGHTPATTERSON AFB OHIO
Personal Author(s) : Haugen,Ronald L.
Report Date : MAY 1970
Pagination or Media Count : 104
Abstract : The mixing of compressible turbulent jets is investigated theoretically. Two solution techniques are presented. A FORTRAN IV computer coding is included for each technique. In the first method, the problem is solved by first writing the momentum and energy equations in Crocco variables. The resulting coupled pair of integral equations are solved numerically using a method of successive approximation. In the second method, the problem is solved, assuming selfsimilar solutions, by applying a coordinate transformation. The resulting coupled pair of nonlinear ordinary differential equations are solved numerically. (Author)
Descriptors : (*JET MIXING FLOW, *SUPERSONIC COMBUSTION), SUPERSONIC COMBUSTION RAMJET ENGINES, TURBULENCE, COMPRESSIBLE FLOW, COMPUTER PROGRAMS, INTEGRAL EQUATIONS, TRANSFORMATIONS(MATHEMATICS)
Subject Categories : Aerodynamics
Fluid Mechanics
Combustion and Ignition
Distribution Statement : APPROVED FOR PUBLIC RELEASE