Accession Number : ADA324327
Title : Final Technical Report on Research on Supersonic Reacting Flows.
Descriptive Note : Final technical rept. 15 Feb 94-14 Feb 97,
Corporate Author : STANFORD UNIV CA DEPT OF MECHANICAL ENGINEERING
Personal Author(s) : Bowman, C. T. ; Hanson, R. K. ; Mungal, M. G. ; Reynolds, W. C.
PDF Url : ADA324327
Report Date : 14 FEB 1997
Pagination or Media Count : 49
Abstract : An experimental and computational investigation of supersonic combustion flows was carried out. The principal objective of the research was to gain a more fundamental understanding of mixing and chemical reaction in supersonic flows. The research effort comprised three interrelated elements: (1) stability analyses and numerical simulations of compressible reacting flows; (2) development of laser induced fluorescence techniques for time resolved multidimensional imaging of species concentration, temperature, velocity and pressure; and (3) an experimental study of mixing and combustion in a supersonic plane mixing layer with the additional development of simple mixing enhancements. The specific objectives and results of the research of each of these program elements have been summarized in this report. New results include: (1) a detailed stability map for reacting, compressible shear layers; (2) new PLIF techniques for transient facilities; (3) new measurements of mixing efficiency in compressible flows; and (4) demonstration of simple mixing enhancement techniques with low pressure drop.
Descriptors : *AIR BREATHING ENGINES, *SUPERSONIC COMBUSTION, *SUPERSONIC FLOW, AIRCRAFT ENGINES, LASER INDUCED FLUORESCENCE, TURBULENT FLOW, COMPUTATIONAL FLUID DYNAMICS, COMBUSTORS, COMPRESSIBLE FLOW, FLOW FIELDS, COMBUSTION STABILITY, HYPERSONIC FLIGHT, SUPERSONIC INLETS, SHEAR FLOW, JET MIXING FLOW, SHOCK TUNNELS.
Subject Categories : Fluid Mechanics
Combustion and Ignition
Distribution Statement : APPROVED FOR PUBLIC RELEASE