Abstract
The present study reports on a new type of entrainment enhancement method. In this case, delta wings, like vortex generators, have been mounted in the periphery of an axisymmetric nozzle, near the exit plane. Thus, streamwise vortices are being generated in the periphery of the jet, The paper reports on an experimental investigation of the effect of this embedded streamwise vorticity on the near field entrainment characteristics of a round jet, for several angles of attack and ReD between 5.8 × 104.
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© 1994 Springer Science+Business Media Dordrecht
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Saini, K.N., Georgiou, D.P., Tsahalis, D.T. (1994). Embedded Streamwise Vorticity in an Axisymmetric Jet. In: Davies, P.A., Neves, M.J.V. (eds) Recent Research Advances in the Fluid Mechanics of Turbulent Jets and Plumes. NATO ASI Series, vol 255. Springer, Dordrecht. https://doi.org/10.1007/978-94-011-0918-5_18
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DOI: https://doi.org/10.1007/978-94-011-0918-5_18
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