[PhD Qualifier] Liquid in a rotating arm

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SUMMARY

The discussion focuses on the physics of a liquid in a rotating "L"-shaped tube, specifically deriving the height to which the liquid rises in the vertical arm when subjected to constant angular speed. The formula derived is y = (P_0 / (gρ))(1 - exp[-(ω²l²M)/(2RT)]), where P_0 is atmospheric pressure, ρ is the liquid density, M is the molecular weight of air, and R is the universal gas constant. The solution involves applying Bernoulli's equation and integrating to find the pressure difference caused by centripetal acceleration, ultimately leading to the height of the liquid column.

PREREQUISITES
  • Understanding of Bernoulli's principle
  • Familiarity with the ideal gas law (pV = nRT)
  • Knowledge of centripetal acceleration concepts
  • Basic calculus for integration
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Homework Statement



An open glass tube of uniform bore (uniform inner diameter) is bent into the shape of an "L". One arm is immersed into a liquid of density \rho and the other arm of length l remains in the air in a horizontal orientation. The tube is rotated with constant angular speed \omega about the axis of the vertical arm. Show that the height y to which the liquid rises in the vertical arm is
y=\frac{P_0}{g\rho}\left(1-exp\left[-\frac{\omega^2 l^2 M}{2RT}\right]\right)​
where P_0 is the atmospheric pressure and M is the molecular weight of air and R is the universal gas constant. Assume that the air pressure inside open end of the tube is atmospheric pressure, as shown (see attached).

Homework Equations



pV=nRT
\rho_{air}=\frac{m}{V}=\frac{MP_0}{RT} (from ideal gas law)

The Attempt at a Solution



I thought about trying to kludge something together with the centripetal acceleration causing a difference in pressure, but that didn't work out for me. Then I looked up Bernoulli's principle, and I don't see how I'm going to get an exponential out of that. What's the appropriate law here?
 

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I think that I've figured it out. You do need Bernoulli's equation. The pressure will be decreasing as you come in from the farthest out point of the arm. The rise in the water level will counteract this decrease in pressure. Now we just need to figure out the change in pressure going from the outside of the arm and working our way in.

An infinitesimal change in pressure from the dynamical pressure term (velocity pressure) will be:
dP= \rho_{air} v dv.

However, v=r\omega and \rho_{air}=\frac{MP}{RT}
So we get:
dP=\frac{MPr\omega^2}{RT} dr
Rearrange and integrate:
\int_{P_0}^P \frac{dP'}{P'}=\int_l^0 \frac{M\omega^2 r}{RT} dr
which yields
P=P_0 exp(-\frac{M\omega^2 l^2}{2R T})
What I have found is the pressure in the air above the water inside the tube. Take the difference between this and P_0 and set it equal to \rho g h (which is making up for the decrease in pressure) and you have the answer. Let me know if you see things wrong with my reasoning.
 

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