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

Respuesta :

Answer: [tex]p_{B} - p_{A}[/tex] = 28800 Pa or 28.8 kPa

Explanation: To determine the pressure of a liquid in a rotating tank,it is used:

p = [tex]\frac{p_{fluid}.w^{2}.r^{2} }{2}[/tex] - γfluid . z + c

where:

[tex]p_{fluid}[/tex] 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:

[tex]p_{B} - p_{A}[/tex] = [tex]\frac{p_{fluid}.w^{2}.r_{B} ^{2} }{2}[/tex] - γfluid.[tex]z_{B}[/tex] - ([tex]\frac{p_{fluid}.w^{2}.r_{A} ^{2} }{2}[/tex] - γfluid.[tex]z_{A}[/tex])

[tex]p_{B} - p_{A}[/tex] = [tex]\frac{p_{fluid}.w^{2}}{2} (r_B^{2} - r_A^{2} )[/tex] - γfluid([tex]z_{B}[/tex] -[tex]z_{A}[/tex])

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

[tex]p_{B} - p_{A}[/tex] = [tex]\frac{p_{fluid}.w^{2}}{2} (r_B^{2} - r_A^{2} )[/tex]

[tex]p_{B} - p_{A} = \frac{0.9.10^3.40^2}{2}(0.2^2 - 0)[/tex]

[tex]p_{B} - p_{A}[/tex] = 28800

The difference in pressure between two points, one on the circumference and the other on the axis is [tex]p_{B} - p_{A}[/tex] = 28800 Pa or 28.8 kPa

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