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Basics of Fluid Mechanics, 2014a

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4.5. FLUID FORCES ON SURFACES 103<br />

x c A<br />

{ }} {<br />

∫ ξ1<br />

I x<br />

′ x<br />

′<br />

{ }} {<br />

M y = P atmos ξdA+gρ sin β ξ 2 dA (4.112)<br />

ξ 0<br />

ξ 0<br />

The moment <strong>of</strong> inertia, I x ′ ′<br />

x<br />

, is about the axis through point “O” into the page.<br />

Equation (4.112) can be written in more compact form as<br />

∫ ξ1<br />

Total Moment in Inclined Surface<br />

M y = P atmos x c A + gρ sin βI x ′ x ′<br />

(4.113)<br />

Example 4.14 can be generalized to solve any two forces needed to balance the area/gate.<br />

Consider the general symmetrical body shown in figure 4.22 which has two forces that<br />

balance the body. Equations (4.109) and (4.113) can be combined the moment and<br />

force acting on the general area. If the “atmospheric pressure” can be zero or include<br />

additional layer <strong>of</strong> liquid. The forces balance reads<br />

and moments balance reads<br />

F 1 + F 2 = A [P atmos + ρg sin β (l 0 + x c )] (4.114)<br />

F 1 a + F 2 b = P atmos x c A + gρ sin βI x ′ x ′ (4.115)<br />

The solution <strong>of</strong> these equations is<br />

[(<br />

)<br />

]<br />

ρ sin β − P atmos<br />

gb<br />

x c + l 0 ρ sin β + P atmos<br />

g<br />

bA−,I x ′ x ′ ρ sin β<br />

F 1=<br />

(4.116)<br />

g (b − a)<br />

and<br />

)<br />

]<br />

I x ′ x<br />

[(ρ ′ ρ sin β − sin β − P atmos<br />

ga<br />

x c + l 0 ρ sin β + P atmos<br />

g<br />

aA<br />

F 2=<br />

(4.117)<br />

g (b − a)<br />

In the solution, the forces can be negative or positive, and the distance a or b can<br />

be positive or negative. Additionally, the atmospheric pressure can contain either an<br />

additional liquid layer above the “touching” area or even atmospheric pressure simply<br />

can be set up to zero. In symmetrical area only two forces are required since the<br />

moment is one dimensional. However, in non–symmetrical area there are two different<br />

moments and therefor three forces are required. Thus, additional equation is required.<br />

This equation is for the additional moment around the x axis (see for explanation in<br />

Figure 4.23). The moment around the y axis is given by equation (4.113) and the total<br />

force is given by (4.109). The moment around the x axis (which was arbitrary chosen)<br />

should be<br />

∫<br />

M x = yPdA (4.118)<br />

A

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