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Question: For the \(L - \) shaped vessel shown in the figure, determine the value of acceleration \(a\) so tha...

For the LL - shaped vessel shown in the figure, determine the value of acceleration aa so that the pressure at point AA becomes equal to p02\dfrac{{{p_0}}}{2}? (p0{p_0} is atmospheric pressure)

A) gg
B) g2+p02ρH\dfrac{g}{2} + \dfrac{{{p_0}}}{{2\rho H}}
C) p02ρH+g\dfrac{{{p_0}}}{{2\rho H}} + g
D) 3p02ρH+g\dfrac{{3{p_0}}}{{2\rho H}} + g

Explanation

Solution

The pressure at which the atmosphere is in directly in contact with the surface is known as atmospheric pressure. Bernoulli’s theorem is based upon the conservation of total energy in a system.

Complete step by step answer:
Bernoulli’s theorem states that the total energy (pressure energy, potential energy and kinetic energy) per unit volume or mass of an incompressible and non-viscous fluid in steady flow through a pipe remains constant throughout the flow, provided there is no source or sink of the fluid along the length of the pipe.
P+ρgh+12ρv2=P + \rho gh + \dfrac{1}{2}\rho {v^2} = constant
Where, P=P = Pressure energy per unit volume
ρgh=\rho gh = Potential energy per unit volume
12ρv2=\dfrac{1}{2}\rho {v^2} = Kinetic Energy per unit volume
In the above case the total energy at AAis equal to total energy at BB. So,
PA+ρaH+ρgH=PB{P_A} + \rho aH + \rho gH = {P_B}
Where, PA={P_A} = Pressure energy per unit volume at AA
ρaH=\rho aH = Kinetic Energy per unit volume at AA
ρgH=\rho gH = Potential energy per unit volume at AA
PB={P_B} = Total energy per unit volume at BB
Now, given in the question that,
PA=p02\Rightarrow {P_A} = \dfrac{{{p_0}}}{2}
PB=p0\Rightarrow {P_B} = {p_0}
So, p02+ρaHρgH=p0\dfrac{{{p_0}}}{2} + \rho aH - \rho gH = {p_0}
ρH(ag)=p02\Rightarrow \rho H\left( {a - g} \right) = \dfrac{{{p_0}}}{2}
ag=p02ρH\Rightarrow a - g = \dfrac{{{p_0}}}{{2\rho H}}
Therefore, a=p02ρH+ga = \dfrac{{{p_0}}}{{2\rho H}} + g

Hence, option C is the correct answer.

Note: The atmosphere exerts the same pressure all over the earth’s surface. That pressure is known as atmospheric pressure. Its value is 1atm1atm. Bernoulli’s theorem is another form of proof for the Law of conservation of energy.