Calculating Shearing Stress in a Newtonian Fluid

AI Thread Summary
The discussion focuses on calculating shearing stress in a Newtonian fluid between two parallel plates, using the velocity distribution equation provided. The viscosity is given as 1.915 Ns/m², with a mean velocity of 0.61 m/s and a plate separation of 5 mm. The shearing stress formula ζ = μ du/dy is emphasized, where the velocity gradient must be determined to find the shear stress at various points. There is confusion regarding the calculation for part B and the origin of the y-coordinate, which is clarified to be at the centerline. The key takeaway is that to find the shear stress, one must derive the velocity function and evaluate it at the appropriate points.
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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.
 
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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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