How Does the Bernoulli Equation Determine Axial Pressure in Jet Flows?

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SUMMARY

The discussion centers on the application of the Bernoulli equation to determine axial pressure in jet flows of incompressible fluids. It is established that the Bernoulli equation cannot be applied to viscous flows, as the jet core is influenced by viscous forces, particularly at non-dimensional distances of order Re_j^{-1}. The external boundary layer pressure remains constant (P_a) in stagnant environments, and typical calculations for incompressible jets assume negligible pressure gradients due to the thin boundary layer at high Reynolds numbers.

PREREQUISITES
  • Understanding of the Bernoulli equation in fluid dynamics
  • Knowledge of viscous flow and boundary layer theory
  • Familiarity with Reynolds number (Re) and its implications
  • Concept of incompressible fluid dynamics
NEXT STEPS
  • Study the application of the Bernoulli equation in inviscid versus viscous flows
  • Explore boundary layer theory and its impact on pressure gradients
  • Investigate the significance of Reynolds number in fluid dynamics
  • Learn about pressure distribution in incompressible jet flows
USEFUL FOR

Fluid dynamics engineers, researchers in hydraulic systems, and students studying advanced fluid mechanics will benefit from this discussion.

Lucus
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Okay, here's the question:

A jet of incompressible fluid emerges from a horizontal channel into an environment of the same fluid. The momentum of the jet at the exit of the channel is measured to be M. The exit momentum is the source of a downstream flow which spreads gradually with distance.

The fluid outside the jet flow is at rest. Use the Bernoulli equation to determine the axial (x) pressure beyond the boundary of the jet flow. How can that result, and the properties of the boundary layer equations be used to determine the axial pressure gradient inside the jet?

So there's the question. I'm not really sure where to start. Any help would be much appreciated. Thanks!
 
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Lucus said:
Okay, here's the question:
A jet of incompressible fluid emerges from a horizontal channel into an environment of the same fluid. The momentum of the jet at the exit of the channel is measured to be M. The exit momentum is the source of a downstream flow which spreads gradually with distance.
The fluid outside the jet flow is at rest. Use the Bernoulli equation to determine the axial (x) pressure beyond the boundary of the jet flow. How can that result, and the properties of the boundary layer equations be used to determine the axial pressure gradient inside the jet?
So there's the question. I'm not really sure where to start. Any help would be much appreciated. Thanks!

Nice problem, although the statement makes no sense. You can't use Bernoulli equation to determine the axial pressure assuming viscous flow as you are doing. The jet core developed in a non dimensional distance of order [tex]Re_j^{-1}[/tex] is dominated by viscous forces. You only can apply Bernouilli to calculate external boundary layer pressure, but as it is an stagnant atmosphere, this pressure is trivially constant [tex]P_a[/tex].
Usual calculations of incompressible jets assume negligible pressure gradients, in part because the boundary layer is so thin at large [tex]Re[/tex] that transversal pressure gradients are very small, and also because by this argument the external pressure impose an uniform pressure across the symmetry axis.
 

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