Accession Number : ADP007715
Title : Numerical Analysis of Converging-Diverging Nozzle Flows in Chemical Non-Equilibrium,
Corporate Author : MOTOREN- UND TURBINEN-UNION G M B H MUNICH (GERMANY F R)
Personal Author(s) : Walther, R.
Report Date : FEB 1992
Pagination or Media Count : 7
Abstract : The converging-diverging nozzle geometries, which are presently proposed for hypersonic propulsion systems, are characterized by large expansion area ratios, and by a geometrically variable nozzle throat to control the engine mass flow. Within the expanding nozzle flow, chemical recombination reactions of the combustor exhaust gas products will occur; the limited chemical reaction rates generally leading to a relaxation of the chemical species composition.
Descriptors : *HYPERSONIC NOZZLES, *NUMERICAL ANALYSIS, CHEMICAL REACTIONS, CHEMICALS, COMBUSTORS, CONTROL, ENGINES, EXPANSION, FLOW, MASS, MASS FLOW, NOZZLE THROATS, NOZZLES, PROPULSION SYSTEMS, RATES, RATIOS, REACTION KINETICS, RECOMBINATION REACTIONS, RELAXATION, THROAT, VARIABLES.
Subject Categories : Fluid Mechanics
Distribution Statement : APPROVED FOR PUBLIC RELEASE