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Transverse Injection from Circular and Elliptic Nozzles into a Supersonic Crossflow
128
Citations
27
References
2000
Year
AeroacousticsEngineeringFluid MechanicsMechanical EngineeringUnsteady FlowVortex DynamicTransverse InjectionStandard DeviationPropulsionMultiphase FlowSonictransverse InjectionSupersonic CombustionCavitating FlowAerospace EngineeringTurbulence ModelingElliptic NozzlesAerodynamicsVortex Induced VibrationSupersonic Crossflow
An investigation of sonictransverse injection from circular and elliptic nozzles into a supersoniccrosse ow using planar Rayleigh/Mie scattering is reported. Instantaneous images allow examination of the structural details, whereas ensemble-averaged images provide transverse penetration and lateral spread data for each jet. Standard deviation images produce information regarding the large-scale mixing/entrainment and reveal the mixing zones. Results show a highly three-dimensional near-e eld interaction dominated by shear-layer eddies and a counterrotating vortex pair. Ensemble-averaged results show that the elliptic jet spreads more rapidly in the lateral direction than the circular jet, cone rming that an axis-switching phenomenon is present. Near-e eld transverse penetration data collapse well with low-speed scaling conventions; however, the jet produced by the elliptic nozzle suffersa20%reductioninpenetrationcomparedto thecircularjet.Compressibilityleveldoesnotplaya signie cant roleintheaveragepenetrationorspreadofthesejets,althoughitstronglyaffectsthemixing/entrainmentandlargescale structure. Analysis of mixing potential from the standard deviation images indicates that the low and high convective Mach number Mc injection cases are signie cantly different; low Mc injection yields better large-scale mixing potential than high Mc injection regardless of the injector geometry.
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