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A closed, 0.4-m-diameter cylindrical tank is completely filled with oil (SG 0.9)and rotates about its vertical longitudinal axis with an angular velocity of 40 rad/s. Determine the difference in pressure just under the vessel cover between a point on the circumference and a point on the axis

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Answer:
p_(B) - p_(A) = 28800 Pa or 28.8 kPa

Step-by-step explanation: To determine the pressure of a liquid in a rotating tank,it is used:

p =
(p_(fluid).w^(2).r^(2) )/(2) - γfluid . z + c

where:


p_(fluid) is the liquid's density

w is the angular velocity

r is the radius

γfluid.z is the pressure variation due to centrifugal force.

For this question, the difference between a point on the circumference and a point on the axis will be:


p_(B) - p_(A) =
(p_(fluid).w^(2).r_(B) ^(2) )/(2) - γfluid.
z_(B) - (
(p_(fluid).w^(2).r_(A) ^(2) )/(2) - γfluid.
z_(A))


p_(B) - p_(A) =
(p_(fluid).w^(2))/(2) (r_B^(2) - r_A^(2) ) - γfluid(
z_(B) -
z_(A))

Since there is no variation in the z-axis, z = 0 and that the density of oil is 0.9.10³kg/m³:


p_(B) - p_(A) =
(p_(fluid).w^(2))/(2) (r_B^(2) - r_A^(2) )


p_(B) - p_(A) = (0.9.10^3.40^2)/(2)(0.2^2 - 0)


p_(B) - p_(A) = 28800

The difference in pressure between two points, one on the circumference and the other on the axis is
p_(B) - p_(A) = 28800 Pa or 28.8 kPa

User Jhanifen
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