How Do You Calculate Static Pressure Drop in a Laminar Flow Channel?

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Discussion Overview

The discussion revolves around calculating the static pressure drop in a laminar flow channel, specifically under conditions of steady state and incompressible flow. Participants explore methods for determining this pressure drop, considering the geometry of the channel and the properties of the fluid involved.

Discussion Character

  • Technical explanation, Conceptual clarification, Debate/contested

Main Points Raised

  • One participant seeks assistance in calculating the static pressure drop across a fully developed laminar flow channel, having already determined the inlet velocity based on the Reynolds number.
  • Another participant suggests solving the Navier-Stokes equations, potentially using numerical methods, and mentions that an analytical solution can be obtained for a simpler case of rectilinear flow between parallel plates.
  • A third participant clarifies the problem's assumptions, including laminar flow, steady state, constant density, and fully developed flow, and hints at using the Darcy Friction Factor and Moody Diagram as part of the solution approach.
  • A later reply requests a more precise statement of the problem to better understand the context and requirements.

Areas of Agreement / Disagreement

Participants express differing views on the methods to calculate the pressure drop, with some suggesting numerical solutions and others proposing analytical approaches. The discussion remains unresolved regarding the best method to apply.

Contextual Notes

Participants have not fully defined the channel geometry, which may affect the calculations. There is also a lack of consensus on the specific assumptions and parameters needed for the pressure drop calculation.

Darcy30
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Hallo. Since I'm new in this field, I hope someone can help me.
I have a laminar, steady state, incompressible flow in a channel (a fully developed).
Geometry of the channel is on the photo.
How should I calculate the drop of static pressure across the channel?
Since I have Re, I did calculate a inlet velocity, but now I'm stuck.
Thanks
 

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To do this, you need to solve the Naiver Stokes equations, probably numerically. To get a lower bound to the pressure drop, you can at least solve analytically for the case where you remove the constriction and have rectilinear flow between parallel plates.
 
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Hi Darcy30,

Was it intentional that your username would hint at the solution?

I understand the problem as follows:
  • Assume laminar, steady state, constant density (incompressible), fully developed flow.
  • Channel Geometry and Fluid Properties are known (I will assume the channel is circular)
  • The inlet velocity is known
Goal:
  • Find the pressure drop across a channel.
Solution Hint:
Darcy Friction Factor, Moody Diagram

Solution:

The pressure drop down a pipe is related to the friction factor.
For Laminar flow,
$$ f_D = \frac{64}{Re} $$
If not, then you will need to assume smooth walls or know the surface roughness.

The pressure drop is related to the following.
$$ dP = f_D * \frac{\rho*V^2*L}{2*D} $$
Break the problem into 3 sections. Inlet straight pipe, the circular restriction, and the outlet straight pipe. The inlet and outlet is straight forward. You will add up the dP for each section to find your answer.

The tricky part of this problem is that you need to integrate the friction factor (hence pressure drop) over the circular restriction. You need a formula for the relationship of Pipe Diameter, D, to length across the channel, x. Something like this:
$$ Dtube = 2 * R - R*sin(acos(R/x)) $$
Additionally, the velocity changes based on cross-sectional area. Use the conservation of mass to find that
$$ mdot = \rho*Area*Velocity $$
There is symmetry, so we only need to consider a 1/4 circle and multiply the friction factor by 2. Integrate from x = 0 to R. Or solve it numerically in a spreadsheet program with small steps of x.

PS: If the channel is indeed non-circular, then use the hydraulic diameter Dh in place of D.
$$ Dh = \frac {4*Area}{Perimeter} $$



References:
[1] Moody Diagram https://en.wikipedia.org/wiki/Moody_chart?msclkid=7b62d23aaee911ec823e165de974644a
[2] Hydraulic Diameter https://en.wikipedia.org/wiki/Hydraulic_diameter?msclkid=0899a52baef711ec890e442c37cca7b6
 
What is the exact statement of the problem?
 

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