Fluid-flow of a row of jets in crossflow - A numerical studyA detailed computer-visualized flow field of a row of jets in a confined crossflow is presented. The Reynolds averaged Navier-Stokes equations are solved using a finite volume method that incorporates a partial differential equation for incremental pressure to obtain a divergence-free flow field. The turbulence is described by a multiple-time-scale turbulence model. The computational domain includes the upstream region of the circular jet so that the interaction between the jet and the crossflow is simulated accurately. It is shown that the row of jets in the crossflow is characterized by a highly complex flow field that includes a horse-shoe vortex and two helical vortices whose secondary velocity components are co-rotating in space. It is also shown that the horse-shoe vortex is a ring of reversed flows located along the circumference of the jet exit.
Document ID
19920045574
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kim, S.-W. (NASA Lewis Research Center Cleveland, OH, United States)
Benson, T. J. (NASA Lewis Research Center Cleveland, OH, United States)