Fluid Mechanics problem - cylinder over a orifice

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SUMMARY

The discussion focuses on applying Bernoulli's equation to determine the static pressure of an ideal fluid in the clearance between a closed cylinder and a round orifice. The derived formula for pressure as a function of the radial distance r is given by P(r) = P_o + \rho gh(1 - \frac{R_1^2}{r^2}), where P_o is atmospheric pressure, \rho is fluid density, h is fluid height, and R_1 is the radius of the orifice. The discussion emphasizes the importance of using a streamline for applying Bernoulli's equation and clarifies the relationship between velocities at different points.

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Homework Statement


The horizontal bottom of a wide vessel with an ideal fluid has a round orifice of radius ##R_1## over which a round closed cylinder is mounted, whose radius ##R_2>R_1##. The clearance between the cylinder and the bottom of vessel is very small, the fluid density is ##\rho##. Find the static pressure of fluid in the clearance as a function of the distance r from the axis of the orifice (and the cylinder), if the height of the fluid is equal to ##h##.


Homework Equations





The Attempt at a Solution


I think I have to apply the Bernoulli's equation but I need two points to apply the Bernoulli equation. How do I find those points? :confused:

I understand I should show some more attempt but I really can't get the intuition behind these fluid mechanics problem so I am unable to make any attempt.

Any help is appreciated. Thanks!
 

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Pranav-Arora said:
I think I have to apply the Bernoulli's equation but I need two points to apply the Bernoulli equation. How do I find those points? :confused:

You might start with two points where you know some information. For example, what can you learn by picking points 1 and 2 as shown?
 

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Hi Pranav-Arora! :smile:
Pranav-Arora said:
I think I have to apply the Bernoulli's equation but I need two points to apply the Bernoulli equation.

No, you need a streamline

Bernoulli's equation is always and only valid along a streamline.​

Once you've drawn a streamline, it should be obvious what to do next. :wink:
 
Hi TSny and tiny-tim! :smile:

tiny-tim said:
No, you need a streamline

Bernoulli's equation is always and only valid along a streamline.​

Once you've drawn a streamline, it should be obvious what to do next. :wink:

I use the streamline shown by TSny and the reference line is a line passing through 2.

From Bernoulli's equation,
$$P_1+\rho gh+\frac{1}{2}\rho v_1^2=P_2+\frac{1}{2}\rho v_2^2$$

I am not sure but is ##P_1=P_2## as both points are open to atmosphere or medium outside? Also, how do I relate ##v_1## and ##v_2##? :confused:
 
Hi Pranav-Arora! :smile:
Pranav-Arora said:
… how do I relate ##v_1## and ##v_2##? :confused:

Draw circles round the hole …

since the density is constant, isn't it obvious from the geometry how the speed must increase as the circles get smaller? :wink:
 
tiny-tim said:
Draw circles round the hole …

since the density is constant, isn't it obvious from the geometry how the speed must increase as the circles get smaller? :wink:

Yes, I do understand that speed increases as the hole size decreases. Okay, so let the area of hole in clearance be s and that of wide vessel be S. From equation of continuity, ##Sv_1=sv_2## but what now? Do I approximate ##v_1## equal to zero? :confused:
 
the pressure (under the cylinder) is a function of r

the pressure in the outlet should be the same as if the cylinder wasn't there :wink:
 
tiny-tim said:
the pressure (under the cylinder) is a function of r

the pressure in the outlet should be the same as if the cylinder wasn't there :wink:

I don't think I get this, can you please elaborate a bit more? :redface:
 
the gauge pressure for an outlet (to the atmosphere) is zero, so that gives you v in the outlet :wink:
 
Last edited:
  • #10
tiny-tim said:
the static pressure for an outlet (to the atmosphere) is zero, so that gives you v in the outlet :wink:

So that means ##v_2=\sqrt{2gh}##? But the question asks something else...
 
  • #11
yes, it asks for P as a function of r, as r moves away from the rim of the hole
 
  • #12
tiny-tim said:
yes, it asks for P as a function of r, as r moves away from the rim of the hole

Hehe tiny-tim. :P

But I don't get why you asked me to find the speed, I am honestly not sure what to do with it. How do I find the pressure as a function of r? :confused:
 
  • #13
Bernoulli's equation gives you the pressure if you know the speed. :wink:
 
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  • #14
The fluid is going to be entering the hole horizontally (i.e., radially), so the volumetric throughput rate entering the hole is going to be 2\pi R_1t\sqrt{2gh}, where t is the clearance. Once you know the volumetric throughput rate, you can get the fluid velocity at any radial location r.
 
  • #15
Chestermiller said:
The fluid is going to be entering the hole horizontally (i.e., radially), so the volumetric throughput rate entering the hole is going to be 2\pi R_1t\sqrt{2gh}, where t is the clearance. Once you know the volumetric throughput rate, you can get the fluid velocity at any radial location r.

Hi Chestermiller!

Okay, I see that you find the rate of flow of liquid but I still don't get how to find the pressure as a function of r.

Do I have to apply Bernoulli at 2 and at some distance r from the axis?
 
  • #16
Pranav-Arora said:
Hi Chestermiller!

Okay, I see that you find the rate of flow of liquid but I still don't get how to find the pressure as a function of r.

Do I have to apply Bernoulli at 2 and at some distance r from the axis?

Yes. You have the pressure and velocity at r = R1, and you have the velocity at arbitrary r, so you use the Bernoulli equation between these two locations to get the pressure at r.
 
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  • #17
Chestermiller said:
Yes. You have the pressure and velocity at r = R1, and you have the velocity at arbitrary r, so you use the Bernoulli equation between these two locations to get the pressure at r.

Thanks Chestermiller and tiny-tim! :smile:

Applying Bernoulli at 2 and at a distance r,
$$P_o+\frac{1}{2}\rho(\sqrt{2gh})^2=P(r)+\frac{1}{2}\rho v^2$$
From equation of continuity, I have
$$A(r)v=2\pi R_1t\sqrt{2gh} \Rightarrow 2\pi rtv=2\pi R_1t\sqrt{2gh} \Rightarrow v=\frac{R_1\sqrt{2gh}}{r}$$

Substituting in Bernoulli and solving for P(r),
$$\boxed{P(r)=P_o+\rho gh\left(1-\frac{R_1^2}{r^2}\right)}$$
(##P_o## is the atmospheric pressure)
 
  • #18
yes, that looks right :smile:
 
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  • #19
tiny-tim said:
yes, that looks right :smile:

Thanks tiny-tim! :)

I compared my answer with the answer given in book. The book shows the condition that ##R_1<r<R_2##. I don't get this. Why not ##R_1 \leq r \leq R_2##? The P(r) I have found is valid for ##R_1##, I am not sure about ##R_2## though.
 
  • #20
Pranav-Arora said:
The P(r) I have found is valid for ##R_1##, I am not sure about ##R_2## though.

i agree with you …

it seems obviously valid for R1, but "at" (or even near) R2 there's likely to be some "edge effect" (related to the movement not being entirely horizontal)

all this is academic … for an "ideal" fluid and "ideal" cylinder, your limits are just as good as the book's! :smile:
 
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  • #21
tiny-tim said:
i agree with you …

it seems obviously valid for R1, but "at" (or even near) R2 there's likely to be some "edge effect" (related to the movement not being entirely horizontal)

all this is academic … for an "ideal" fluid and "ideal" cylinder, your limits are just as good as the book's! :smile:

Thank you once again tiny-tim! :smile:
 

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