Accession Number : ADA183952
Title : High-Speed Reacting Flows: Research to Understand Processes in Supersonic Combustors.
Descriptive Note : Annual letter rept. 1 Jun 86-31 May 87,
Corporate Author : ILLINOIS UNIV AT URBANA DEPT OF MECHANICAL AND INDUSTRIAL ENGINEERING
Personal Author(s) : Krier, H ; Dutton, J C ; Renie, J P
PDF Url : ADA183952
Report Date : 31 May 1987
Pagination or Media Count : 4
Abstract : The objective of this program is to determine the fundamental fluid dynamic mechanisms occurring in the mixing and entrainment processes in the free shear layer formed between two high-speed (supersonic/sonic) streams. How the fluid mixing and subsequent combustion depends upon compressibility, as well as other parameters of the free shear layer process, is currently being investigated in an experimental study of the two-dimensional, compressible, turbulent reactive free shear layer. Use of non-intrusive, laser-based diagnostics including laser Schlieren for flow visualization, Laser Doppler Velocimetry (LDV) for velocity and turbulence measurement, and Planar Laser-Induced Fluorescence (PLIF) for temperature and concentration measurements are being employed.
Descriptors : *COMBUSTORS, *SUPERSONIC CHARACTERISTICS, *SUPERSONIC COMBUSTION RAMJET ENGINES, COMBUSTION, COMBUSTORS, DIAGNOSIS(GENERAL), DOPPLER SYSTEMS, ENTRAINMENT, FLOW VISUALIZATION, FLUID DYNAMICS, FLUIDS, LASER APPLICATIONS, LASER INDUCED FLUORESCENCE, LASER VELOCIMETERS, LASERS, LAYERS, MEASUREMENT, MIXING, SHEAR PROPERTIES, SUPERSONIC CHARACTERISTICS, TURBULENCE, REACTIVE GASES, COMPRESSIBLE FLOW, TURBULENT FLOW
Subject Categories : Combustion and Ignition
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE