By Antonio Segalini

ISBN-10: 3319306006

ISBN-13: 9783319306001

ISBN-10: 3319306022

ISBN-13: 9783319306025

This quantity collects quite a few contributions from the 5th foreign convention on Jets, Wakes and Separated Flows (ICJWSF2015) that happened in Stockholm in the course of June 2015. Researchers from all over the global provided their most modern effects bearing on basic and utilized features of fluid dynamics. With its basic personality, the convention embraced many elements of fluid dynamics, corresponding to shear flows, multiphase flows and vortex flows, for example. The constitution of the current ebook displays the range of subject matters handled in the convention i.e. Jets, Wakes, Separated flows, motor vehicle aerodynamics, Wall-bounded and restrained flows, Noise, Turbomachinery flows, Multiphase and reacting flows, Vortex dynamics, Energy-related flows and a bit devoted to Numerical analyses.

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Additional info for Proceedings of the 5th International Conference on Jets, Wakes and Separated Flows (ICJWSF2015)

Sample text

1a(1), where one reactant is advected to a planar reaction sheet while the other counter-diffuses against the combustion products. This configuration is desirable for the development of theoretical models because all transport processes are 1D and combustion-mediated phenomena can be investigated uncoupled from hydrodynamic perturbations. The counter-flowing jet array overcomes a longstanding obstacle preventing the experimental realization such flames: ensuring the spatially homogeneous supply of the counter-diffusing reactant and removal of the combustion products on the same side of the reaction sheet.

7, the axial velocity of the annular jet becomes equal to the similar velocity of the round jet, and then along the distance to the stagnation point exceeds this value. In addition, the velocity pulsations at the annular jet axis are significantly higher than velocity pulsations in the round jet; they vary non-monotonically along the region length and increase directly near the obstacles. This follows clearly from data comparison in Fig. 3b. (b) 0,0 x/d0 x/d0 (a) 0,0 0,5 0,5 1,0 1,0 1 2 1,5 1,5 1 2 U, m/s 2,0 -8 -4 0 4 8 12 16 20 u'/U0 2,0 0,00 0,04 0,08 0,12 0,16 0,20 Fig.

Jet arrays (without counterflow) impinging on solid surfaces have been studied in the context of electronic components cooling. The effect of jet spacing [3] was investigated but the issue of penetration depth was not addressed. Instabilities with characteristic length greater than the jet spacing have been observed as a results of the interaction between several jets in closely spaced co-flowing arrays with high ???? [9]. The investigations described above are of limited use here as they were carried out assuming that diffusion is negligible and that the jet confinement is small.

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Proceedings of the 5th International Conference on Jets, Wakes and Separated Flows (ICJWSF2015) by Antonio Segalini


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