Skip to content

The Force That Outraces Its Own Piston

Irodov 1.322DifficultyDifficulty 3 of 5UniquenessUniqueness 4 of 5

Problem Irodov 1.322

A horizontal cylinder full of water is closed by a piston at one end and has a small orifice of cross-sectional area ss at the other, with ss much smaller than the piston’s own cross-sectional area. A constant force pushes the piston until the entire volume VV of water has been squeezed out through the orifice, taking a time tt to do so. Neglecting friction and viscosity, find the work done by the force.

The horizontal cylinder: a constant force F drives the piston, squeezing the water of volume V out through the small orifice of area s.

The horizontal cylinder: a constant force FF drives the piston, squeezing the water of volume VV out through the small orifice of area ss.

Given
  • VV
  • ss
  • tt
  • s≪Ss \ll S (piston area)
Find
Find the work AA done by the force during the time tt

Solution

Step 1Why the flow is steady throughout

The force FF and the piston area SS are both constant, so the gauge pressure driving the water is constant for the whole process:

p=FS.p = \frac{F}{S}.

Since s≪Ss \ll S, the piston itself advances far slower than the water leaves the orifice, so at every instant the flow is effectively the same steady jet driven by this fixed pressure: the exit speed vv it sets does not change with time.

Step 2Work done equals the kinetic energy carried out by the jet

The cylinder is horizontal, so no water changes height, and friction and viscosity are negligible by hypothesis. The piston’s own speed is smaller than the jet’s by the same factor s/S≪1s/S \ll 1, so its kinetic energy is negligible next to the jet’s. By energy conservation, all the work AA done by the force converts into the kinetic energy of the ejected water:

A=12(ρV)v2,A = \frac{1}{2}(\rho V) v^2,

where ρ\rho is the density of water and ρV\rho V the mass of the whole volume expelled.

A=12ρVv2A = \dfrac{1}{2}\rho V v^2
(1)
Step 3The exit speed from continuity

The orifice passes the whole volume VV over the time tt at the rate svsv, constant because the exit speed vv is, so

V=svt⟹v=Vst.(2) V = s v t \quad\Longrightarrow\quad v = \frac{V}{st}. \tag{2}
Step 4Combining

Substituting the exit speed (2) into (1) and squaring first,

A=12ρV(Vst)2=12ρV⋅V2s2t2.A = \frac{1}{2}\rho V\left(\frac{V}{st}\right)^2 = \frac{1}{2}\rho V\cdot\frac{V^2}{s^2t^2}.
A=ρV32s2t2A = \dfrac{\rho V^3}{2 s^2 t^2}
(3)
Check

Dimensions: [ρ][V]3/([s]2[t]2)=(kg/m3)(m9)/(m4 s2)=kg m2/s2=J[\rho][V]^3/([s]^2[t]^2) = (\text{kg/m}^3)(\text{m}^9)/(\text{m}^4\,\text{s}^2) = \text{kg}\,\text{m}^2/\text{s}^2 = \text{J}, correct for work. Also A∝1/t2A\propto 1/t^2: squeezing the same volume out twice as fast needs four times the work, since the exit speed doubles and the kinetic energy goes as v2v^2; and AA does not depend on the piston area SS at all, only on the orifice, which is the whole point of s≪Ss\ll S.

Remark

The piston does work on the water, but essentially none of it stays as the piston’s own kinetic energy: because s≪Ss\ll S the piston creeps while the jet flies, so all the work reappears as the jet’s kinetic energy. That is the same accounting used for a fire hose or a rocket nozzle, where a wide, slow reservoir is driven through a narrow, fast exit, and it is why AA never has to mention the piston’s own speed at all.