Submerged jet's profile-specific heat transfer: Stagnation zone and beyond

• Analysis of a new free-surface jet regime, in which centerline velocity remains constant over long distances, is explained and generalized for all issuing profiles. • The deceleration during wall-approach is successfully captured over a wide range of conditions, as an interpolation between far- and near-wall analytical solutions. • Flow aspects, such as the boundary layer thickness are quite well predicted in the stagnation zone and a foundation is laid for more detailed radial distributions. • An explicit heat transfer prediction within the stagnation zone is provided, which is shown to be dependent only on arrival jet profile for a multitude of conditions: horizontal jets, vertical jets with gravity, high surface tension, highly viscous flows, etc. A general analytical description for the heat transfer distribution (HTD) under an impinging submerged jet is derived, from the jet velocity profile arriving at the wall. First, the cause-and-effect chain is broken down: i) the streamline-bending projection of the arriving profile's dynamic pressure gives the wall pressure distribution; ii) the pressure gradient drives the radial acceleration; iii) the acceleration unlocks the entire flow field: boundary layer, wall-shear and vorticity distributions; iv) ultimately also the HTD is recovered from similarity; iv) this extends up to deceleration, approaching the known wall-jet solution. This new theory is validated against simulations and experiments over a wide range of conditions: from uniform to fully developed issuing profiles, over a range of flights. Thus, confirming that the arriving profile contains everything needed for the subsequent wall-flow description, and demonstrating that the HTD diversity corresponds to that of the arrival profiles. This permits the prediction of the HTD in a universal way, from stagnation point to wall-jet. Specifically, relating the well-known off-center peak (boundary layer thinning) to an incoming profile shape with strong velocity gradients, as encountered in profiles with a potential core. Two different pathways for the generation of this off-center peak are studied and compared.

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Publication Details

Journal
International Journal of Heat and Mass Transfer
Published
2025-03-28
DOI
https://doi.org/10.1016/j.ijheatmasstransfer.2025.126924
Primary Topic
Heat Transfer Mechanisms
Type
article
Field-Weighted Citation Impact
0.00

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article

Submerged jet's profile-specific heat transfer: Stagnation zone and beyond

Herman D. Haustein, Barak Kashi
International Journal of Heat and Mass Transfer
Heat Transfer Mechanisms
article

Submerged jet's profile-specific heat transfer: Stagnation zone and beyond

Herman D. Haustein, Barak Kashi
article en

Abstract

• Analysis of a new free-surface jet regime, in which centerline velocity remains constant over long distances, is explained and generalized for all issuing profiles. • The deceleration during wall-approach is successfully captured over a wide range of conditions, as an interpolation between far- and near-wall analytical solutions. • Flow aspects, such as the boundary layer thickness are quite well predicted in the stagnation zone and a foundation is laid for more detailed radial distributions. • An explicit heat transfer prediction within the stagnation zone is provided, which is shown to be dependent only on arrival jet profile for a multitude of conditions: horizontal jets, vertical jets with gravity, high surface tension, highly viscous flows, etc. A general analytical description for the heat transfer distribution (HTD) under an impinging submerged jet is derived, from the jet velocity profile arriving at the wall. First, the cause-and-effect chain is broken down: i) the streamline-bending projection of the arriving profile's dynamic pressure gives the wall pressure distribution; ii) the pressure gradient drives the radial acceleration; iii) the acceleration unlocks the entire flow field: boundary layer, wall-shear and vorticity distributions; iv) ultimately also the HTD is recovered from similarity; iv) this extends up to deceleration, approaching the known wall-jet solution. This new theory is validated against simulations and experiments over a wide range of conditions: from uniform to fully developed issuing profiles, over a range of flights. Thus, confirming that the arriving profile contains everything needed for the subsequent wall-flow description, and demonstrating that the HTD diversity corresponds to that of the arrival profiles. This permits the prediction of the HTD in a universal way, from stagnation point to wall-jet. Specifically, relating the well-known off-center peak (boundary layer thinning) to an incoming profile shape with strong velocity gradients, as encountered in profiles with a potential core. Two different pathways for the generation of this off-center peak are studied and compared.

International Journal of Heat and Mass TransferVol. 245
Tel Aviv University (IL)
PAZY Foundation
Affordable and clean energy
Openalex Percentile: Top 94%
Heat Transfer Mechanisms
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