Publication | Closed Access
Mixing of a Sonic Transverse Jet Injected into a Supersonic Flow
175
Citations
25
References
2000
Year
Unsteady FlowEngineeringAerospace EngineeringStandard Deviation ImagesFluid MechanicsFlow PhysicTurbulenceTurbulence ModelingRocket EngineAerodynamicsPropulsionMultiphase FlowSupersonic FlowInstantaneous ImagesCrosse Ow
The mixing characteristics of an underexpanded sonic jet injected into a Mach 1.6 crosse ow are studied experimentally. Shadowgraph photography and planar laser-induced e uorescence from acetone are used to obtain temporally resolved e owe eld visualizations of a side viewof the barrel shock region, a side view of the downstream plume, and an end view cross section of the plume. Instantaneous images, mean and standard deviation images, and image-intensity probability density functions (PDFs) are used to study the mixing produced by large-scale turbulent structures. PDFs show that time-averaged mixture fraction measurements greatly overestimate the actual level of instantaneous mixing in the e owe eld. Comparisons of the instantaneous images and PDFs show the role of large-scale rolling structures and jetlike plumes in transporting coherent packets of e uid across the threedimensional shear layer formed between the jet and crosse ow. Signie cant instantaneous mixing in this e owe eld occursin the wakeregiondownstream ofthebarrel shock region and below thejetcenterline.Thecounter-rotating streamwisevortex pairin thejetplumeplaysan importantrole in the scalarmixing processes becauseit transports jet e uid down toward the wake and entrains crosse ow e uid from below up into the jet.
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