Calculating Shearing Stress in a Newtonian Fluid

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SUMMARY

The discussion focuses on calculating shearing stress in a Newtonian fluid flowing between two parallel plates, using the velocity distribution equation u=3V/2[1-(y/h)^2]. The viscosity of the fluid is specified as 1.915 Ns/m², with a mean velocity (V) of 0.61 m/s and a plate separation (h) of 5 mm. The shearing stress is determined using the formula ζ=μ du/dy, where the velocity gradient du/dy is derived from the velocity profile. Key insights include that the shearing stress at the bottom wall is zero, and the maximum velocity occurs at the centerline (y=0).

PREREQUISITES
  • Understanding of Newtonian fluid dynamics
  • Familiarity with viscosity and its units (Ns/m²)
  • Knowledge of calculus, specifically differentiation
  • Ability to interpret velocity profiles in fluid mechanics
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  • Study the derivation of velocity profiles for Newtonian fluids
  • Learn about the implications of shear stress in fluid flow
  • Explore the concept of parabolic velocity profiles in laminar flow
  • Investigate the application of the Navier-Stokes equations in fluid dynamics
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Homework Statement


The velocity distribution for the floe of a Newtonian fluid between 2 wide parallel plates is given by the equation u=3V/2[1-(y/h)^2] where V is the mean velocity. The fluid has a viscosity of 1.915Ns/m^2. When V=0.61m/s and h=5mm, determine:
A) the shearing stress acting on the bottom wall.
B) the shearing stress acting on a plane parallel to the wall.
C) the shearing stress at the centerline.

Homework Equations


ζ=μ du/dy

The Attempt at a Solution


For C) I worked out u=0.915[1-y^2/2.5X10^-3]
From that I worked out ζ=1.915 X 0.915[1-y^2/2.5X10^-3] X 1/dy.

I have no idea how to work out B).

I think A) =0 as there is no velocity there? I could be very wrong saying that though.
 
Last edited:
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Where is the origin of h? Bottom plate, top plate, center?
 
Either bottom or top plate, doesn't make a diff in this question. It's like a radius if you will. It says the flow is symetrical.
 
I hit the h key instead of the y key. Typo. Where is the origin of y?
 
"For C) I worked out u=0.915[1-y^2/2.5X10^-3]
From that I worked out ζ=1.915 X 0.915[1-y^2/2.5X10^-3] X 1/dy."

How can this be when ζ=μ du/dy?
 
Origin of y is the centerline.

LawrenceC said:
"For C) I worked out u=0.915[1-y^2/2.5X10^-3]
From that I worked out ζ=1.915 X 0.915[1-y^2/2.5X10^-3] X 1/dy."

How can this be when ζ=μ du/dy?

I dunno, I'm really confused. :/
 
Here is some more help. The profile is parabolic with the velocity function given by u=V/2[1-(y/h)^2] where V is the average velocity.

The shear stress is given by:
S = mu*du/dy which is the viscosity multiplied by the velocity gradient in the direction perpendicular to the flow. If you plot the velocity profile you will note that when y is zero (centerline), the velocity is maximum. Furthermore the fluid velocity is zero at the walls where y= +h or -h. To determine shear, you take the derivative with respect to y. V, the average velocity, is constant.

So all you need to do for part C is take the derivative and plug in the value of y=h.
 

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