Accession Number : ADA290859
Title : An Experimental Study Of Planar Heterogeneous Supersonic Confined Jets.
Descriptive Note : Doctoral thesis,
Corporate Author : AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OH
Personal Author(s) : Tanis, Frederick J., Jr
PDF Url : ADA290859
Report Date : DEC 1994
Pagination or Media Count : 184
Abstract : The effects of varying the exit pressure of a supersonic helium jet exhausting coaxially with two parallel supersonic air streams into a constant area duct were investigated. The method used to evaluate the mass entrainment rate was to measure helium molar concentration profiles and mass flux across the duct using a binary gas probe then calculate the mass entrainment into the helium jet. In order to conduct this study a novel binary gas probe was developed which allowed helium concentration and mass flux data to be obtained during continuous traverses across the supersonic flowfield. High exit pressure ratio (EPR) led to improved overall mixing compared to the baseline case with an EPR near unity. The high EPR caused low mass entrainment along the jet shear layers due to high convective Mach numbers and velocity ratios, but the high EPR caused oblique shocks to form which reflected off the duct walls and intersected with the helium jet several times causing significant mass entrainment due to numerous shock-shear layer interactions (SSLIs). A correlation between the vorticity generated during a SSLI and the mass entrainment into the jet was developed. (AN)
Descriptors : *SUPERSONIC FLOW, *SUPERSONIC COMBUSTION RAMJET ENGINES, *JET MIXING FLOW, VELOCITY, PRESSURE GRADIENTS, EXPERIMENTAL DATA, SHOCK WAVES, AIR FLOW, THESES, BOUNDARY LAYER, VORTICES, GAS DYNAMICS, MASS FLOW, FLOW FIELDS, SHEAR STRESSES, WIND TUNNEL TESTS, HELIUM, MACH NUMBER, CONVECTION(HEAT TRANSFER), STATIC PRESSURE, GAS SURFACE INTERACTIONS, NOZZLE GAS FLOW, SCHLIEREN PHOTOGRAPHY, FUEL INJECTION, AIR ENTRAINMENT.
Subject Categories : Fluid Mechanics
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE