How do I calculate the new pressure of liquid water using its isothermal compressibility #kappa# and expansion coefficient #alpha#?

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

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

What is this new pressure? I know it is #"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_P#
#kappa = -1/V ((delV)/(delP))_T => kappadP_T = -1/VdV_T#

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

Note that #1/VdV_P# and #-1/VdV_T# are under different conditions so they are not equivalent. #"_"""_P# is constant pressure, and #"_"""_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 #alpha# and #kappa#, 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) = ???#

Starting from the total derivative of the differential volume

#dV = ((delV)/(delT))_P dT + ((delV)/(delP))_T dP#,

we can divide by the partial differential temperature at a constant volume, #delT_V#, to find #((delP)/(delT))_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")#