Fluid Mechanics problem - cylinder over a orifice

AI Thread Summary
The discussion revolves around solving a fluid mechanics problem involving a closed cylinder over an orifice in a vessel filled with an ideal fluid. Participants emphasize the application of Bernoulli's equation, highlighting the need to identify appropriate points along a streamline to derive the pressure as a function of the distance from the orifice's axis. The solution involves using the continuity equation to relate velocities at different points and applying Bernoulli's equation to find the pressure under the cylinder. The derived pressure function is valid for distances greater than the orifice radius but raises questions about its validity near the cylinder's edge due to potential edge effects. Overall, the conversation focuses on understanding fluid dynamics principles to arrive at the correct pressure function.
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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:
 
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  • #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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