How do I calculate the new pressure of liquid water using its isothermal compressibility kappaκ and expansion coefficient alphaα?

I'm given that the isothermal compressibility kappa = 4.7xx10^(-5) "atm"^(-1)κ=4.7×105atm1 and expansion coefficient alpha = 1.7xx10^(-4) "K"^(-1)α=1.7×104K1 at 17^@ "C"17C. The rest of the question states:

  • closed rigid container filled with liquid water at an initial temperature of 14^@ "C"14C and initial pressure of "1 atm"1 atm.
  • The temperature is changed to 20^@ "C"20C, and the new pressure is to be found.
  • Assume that alphaα and kappaκ are negligibly different whether it's 17^@ "C"17C or 14^@ "C"14C or 20^@ "C"20C.

What is this new pressure? I know it is "23 atm"23 atm, but I don't know how to do the problem.

Here are the definitions you need to know, and the calculus you may need to know:

alpha = 1/V ((delV)/(delT))_P => alphadT_P = 1/VdV_Pα=1V(VT)PαdTP=1VdVP
kappa = -1/V ((delV)/(delP))_T => kappadP_T = -1/VdV_Tκ=1V(VP)TκdPT=1VdVT

  • ((delV)/(delP))_T(VP)T is the partial derivative of the volume with respect to the pressure at a constant temperature.
  • ((delV)/(delT))_P(VT)P is the partial derivative of the volume with respect to the temperature at a constant pressure.

Note that 1/VdV_P1VdVP and -1/VdV_T1VdVT are under different conditions so they are not equivalent. "_"""_P_P is constant pressure, and "_"""_T_T is constant temperature.

Also, you cannot use the ideal gas law, because it fails on liquids.

1 Answer
Aug 24, 2016

AHA! Actually, right after I wrote this question out, I figured it out.


The logic behind this is to express the change in pressure with respect to temperature at a constant volume in terms of alphaα and kappaκ, since:

  • The container is rigid and full of liquid water. i.e. constant volume.
  • The water changes pressure due to the change in temperature. i.e. (dP)/(dT) = ???dPdT=???

Starting from the total derivative of the differential volume

dV = ((delV)/(delT))_P dT + ((delV)/(delP))_T dPdV=(VT)PdT+(VP)TdP,

we can divide by the partial differential temperature at a constant volume, delT_VTV, to find ((delP)/(delT))_V(PT)V.

cancel(((delV)/(delT))_V)^(0) = ((delV)/(delT))_Pcancel(((delT)/(delT))_V)^(1) + ((delV)/(delP))_T stackrel("goal")overbrace(((delP)/(delT))_V)

The term that cancels to 0 is because the change in volume must be 0 at a constant volume, and the term that cancels to 1 cancels because (dT)/(dT) = 1, and 1 at a constant volume is still 1.

Thus, our big equation becomes:

((delP)/(delT))_V = (-((delV)/(delT))_P)/((delV)/(delP))_T

If we note that the definitions of alpha and kappa say alpha = 1/V((delV)/(delT))_P and kappa = -1/V((delV)/(delP))_T, then:

((delP)/(delT))_V = (cancel(-V)alpha)/(cancel(-V)kappa) = alpha/kappa

Now, we can do this trick where we multiply out a partial differential temperature at a constant volume to turn it into an exact differential, dT_V, and then integrate.

dP_V = alpha/kappa dT_V

int_(P_1)^(P_2) dP_V = alpha/kappa int_(T_1)^(T_2) dT_V

P_2 - P_1 = alpha/kappa (T_2 - T_1)

So the final expression is:

bb(P_2 = P_1 + alpha/kappa (T_2 - T_1))

And if we use this to evaluate the final pressure:

color(blue)(P_2) = "1 atm" + (1.7xx10^(-4) "K"^(-1))/(4.7xx10^(-5) "atm"^(-1))("6 K")

= 22.7 ~~ color(blue)("23 atm")