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Center of Pressure Experiment in Mechanical Engineering Laboratories, Summaries of Acting

Information about an experiment conducted in mechanical engineering laboratories to determine the resultant force and center of pressure acting on a partially and fully submerged plane surface. the objectives, description of apparatus, theoretical analysis, and procedures for the experiment.

Typology: Summaries

2021/2022

Uploaded on 09/12/2022

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Mechanical Engineering Laboratories
1
Center of Pressure
Objectives:-
1- To determine experimentally the resultant force acting on a partially and fully submerged plane
surface.
2- To determine experimentally the moments due to the resultant force ,and compare the results with
theoretical analysis.
3- To determine experimental and the theoretical center of pressure.
Description of Apparatus:-
Water is contained in a quadrant of a semi-
circular perspex tank assembly which is
allowed to roll on a smooth surface. The
cylindrical sides of the quadrant have their
axes coincident with the centre of rotation of
the tank assembly, and therefore the total
fluid pressure acting on these surfaces exerts
no moment about that centre. The only
moment present is that due to the fluid
pressure acting on the plane surface. This
moment is measured experimentally by
applying weights to a weight hanger
mounted on the semi-circular assembly on
the opposite side to the quadrant tank.
A second tank, Situated on the same side of
the assembly as the weight hanger, provides
a trimming facility and enables different
angles of balance to. The angular position of
the plane and the height of water above it are
measured on a protractor scale mounted on
the tank and a linear scale on the back panel. Fig. 1 center of pressure apparatus
The apparatus is completed by base leveling feet and
spirit level together with a water reservoir and filling jug.
Specifications:
Inner radius R1 = 100 mm
Outer radius R2 = 200 mm
Breadth(width) B = 75 mm
Moment arm R3 = 203 mm
Weight hanger 50 g
Theory:-
Centre of Pressure may be defined as the point in a plane at which the fluid thrust can be said to be
acting normal to that plane.
Referring to (fig 2), consider an element at start depth y, width dy.
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Center of Pressure

Objectives:-

1- To determine experimentally the resultant force acting on a partially and fully submerged plane surface.

2- To determine experimentally the moments due to the resultant force ,and compare the results with theoretical analysis.

3- To determine experimental and the theoretical center of pressure.

Description of Apparatus:-

Water is contained in a quadrant of a semi- circular perspex tank assembly which is allowed to roll on a smooth surface. The cylindrical sides of the quadrant have their axes coincident with the centre of rotation of the tank assembly, and therefore the total fluid pressure acting on these surfaces exerts no moment about that centre. The only moment present is that due to the fluid pressure acting on the plane surface. This moment is measured experimentally by applying weights to a weight hanger mounted on the semi-circular assembly on the opposite side to the quadrant tank.

A second tank, Situated on the same side of the assembly as the weight hanger, provides a trimming facility and enables different angles of balance to. The angular position of the plane and the height of water above it are measured on a protractor scale mounted on the tank and a linear scale on the back panel. Fig. 1 center of pressure apparatus

The apparatus is completed by base leveling feet and spirit level together with a water reservoir and filling jug.

Specifications:

Inner radius R 1 = 100 mm Outer radius R 2 = 200 mm Breadth(width) B = 75 mm Moment arm R 3 = 203 mm Weight hanger 50 g

Theory:-

Centre of Pressure may be defined as the point in a plane at which the fluid thrust can be said to be acting normal to that plane.

Referring to (fig 2), consider an element at start depth y , width d y.

The basic equation of the resultant hydrostatic force is as follows:

   A

F P dA … (1)

Where,

dA B dy

P ycos h

Therefore, result force on element :

F  (^)    ycoshBdy …(2)

Equation (2) provides an expression for the resultant force F as a function of the pressure acting over the differential area element dA = B dy.

Assume the localized acceleration of gravity is a constant 9.81 m/s

2 and that the water is

incompressible with constant density 1000 kg/m

3 so:  g  1000  9. 81  9810 N/ m^3 … (3)

The moment of force on element about O is:

Mo F y

Mo  (^)   ycosh Bdy y

M (^) o  (^)    y^2 coshyBdy … (4)

The value of moment experimentally is:

M (^) exp  gmR 3 … (5)

Fexp  m g … (6)

Case 1:- plane partially submerged

Recall Equ.(2) and integrate from (h secθ ) to R 2 :-

 ^  

R 2

hsec

Fth B ycos h dy

R 2

hsec

2 th 2 cos hy

y F B 

h sec cos hR 2

R
F B

2 2

2 2 th …(7)

Now, recall Equ.(4) and integrate from (h secθ ) to R 2 :-

 ^  

R 2

hsec

2 Mth B y cos hy dy

trim tank until the desired position is achieved. The protractor on the tank assembly should be read against the zero line on the back scale.

2- First add a 20g weight to the weight hanger, Pour water into the quadrant tank until a 0^0 balance is restored. Note the weight and the height reading of the water (h). Repeat the procedure for the fuIl range of weights in steps of 50 g.

3-Empty both tanks of water and repeat the procedure for 10^0 , 20^0.

4-Readings should be tabulated in table (1) and(2).

Discussion:

1-The point of action of the result force is below the centroid, why?

2-If we change the water to some other fluid ,such as oil , does the magnitude of the result force and its location change? why?

3-What is the applications of this experiment?

4-Explane why the tank take the shape of quadrant?

5-Discuss the sources of error?

6-Plot ,find the slope, and discuss the results for both cases :

-partially submerged

[

BR h M

2 2 th

 against h 3 ] and [ 2

BR h M

2 2 exp

 against h 3 ]

-fully submerged

[ M (^) thagainst h ] and [ Mexp against h ]

Fig. 2 schema of center of pressure apparatus

B

θ

R 1

h

R 3 R 2

W

dF

dy

y

dy