Paper 2, Section II, C

Waves
Part II, 2018

A perfect gas occupies the region x>0x>0 of a tube that lies parallel to the xx-axis. The gas is initially at rest, with density ρ1\rho_{1}, pressure p1p_{1}, speed of sound c1c_{1} and specific heat ratio γ\gamma. For times t>0t>0 a piston, initially at x=0x=0, is pushed into the gas at a constant speed VV. A shock wave propagates at constant speed UU into the undisturbed gas ahead of the piston. Show that the excess pressure in the gas next to the piston, p2p1βp1p_{2}-p_{1} \equiv \beta p_{1}, is given implicitly by the expression

V2=2β22γ+(γ+1)βp1ρ1V^{2}=\frac{2 \beta^{2}}{2 \gamma+(\gamma+1) \beta} \frac{p_{1}}{\rho_{1}}

Show also that

U2c12=1+γ+12γβ\frac{U^{2}}{c_{1}^{2}}=1+\frac{\gamma+1}{2 \gamma} \beta

and interpret this result.

[Hint: You may assume for a perfect gas that the speed of sound is given by

c2=γpρc^{2}=\frac{\gamma p}{\rho}

and that the internal energy per unit mass is given by

e=1γ1pρe=\frac{1}{\gamma-1} \frac{p}{\rho}