2. Evaporation 7 pts

Thermodynamics · Phase transitions, Diffusion, Heat transfer

Piston–cylinder equilibrium with saturated vapour, and derivation of the wet-bulb temperature of sweating skin in a sauna.

Solution by Jaan Kalda, grading schemes by Mattias Bjerklöv, Marko Tsengov, Eppu Leinonen.

Part i (2 points)

Water is in a good approximation incompressible; hence, when the piston starts moving, the growing volume must be filled by gas which can only be the water vapours. Thus, the water starts boiling: these vapours must be in equilibrium with water, hence the vapour pressure must be equal to the pressure inside the piston. We can read from the graph that at T0T_0, the vapour density is ρ=420gm3\rho = 420\,\text{g\,m}^{-3}; this corresponds to the pressure p1=ρRT/μ=70kPap_1 = \rho RT/\mu = 70\,\text{kPa}. With atmospheric pressure p0=100kPap_0 = 100\,\text{kPa}, the force needed to pull the piston is S(p0p1)=300NS(p_0 - p_1) = 300\,\text{N}.

Grading

  • Realize that the pressure inside the cylinder equals the saturated vapour pressure of water at temperature T0T_0: 0.8 pts
  • Read the density ρ\rho from the graph, in the range [400,440]gm3[400,\,440]\,\text{g\,m}^{-3}: 0.2 pts
  • Use the ideal gas law to find an expression for the pressure p1p_1 at temperature T0T_0: 0.4 pts
  • Correct expression for the force: S(p0p1)S(p_0 - p_1): 0.4 pts
  • Correct numerical answer: 0.2 pts

Part ii (2 points)

When the piston is pulled by displacement aa, creating new volume Vnew=S×aV_\text{new} = S \times a, the water partially evaporates to fill this volume with vapour and the remaining liquid water cools from temperature T0T_0 to T1T_1. The mass of vapour mvm_v needed to fill the new volume can be calculated using the vapour density ρ1=405gm3\rho_1 = 405\,\text{g\,m}^{-3} as mv=Saρ1m_v = Sa\rho_1. For the heat balance, the energy needed for evaporation must come from the cooling of the remaining liquid water:

mvL=(mmv)c(T0T1).(1)m_v L = (m - m_v) \cdot c \cdot (T_0 - T_1). \tag{1}

Here we have neglected the dependence of LL on temperature and the heat capacity of water vapours, because μL4R(T1T0)\mu L \gg 4R(T_1 - T_0) (but we have not neglected the work done by the piston, because LL is the enthalpy of evaporation and already includes pΔVp\Delta V). Similarly, since Lc(T1T0)L \gg c(T_1 - T_0), we can neglect mvm_v in the right-hand-side and express

m=mvLc(T0T1)=ρ1SaLc(T0T1)=650g.(2)m = \frac{m_v L}{c(T_0 - T_1)} = \frac{\rho_1 SaL}{c(T_0 - T_1)} = 650\,\text{g}. \tag{2}

Grading

  • Read the vapour density ρ1\rho_1 from the graph (ρ1[390,420]gm3\rho_1 \in [390,\,420]\,\text{g\,m}^{-3}): 0.2 pts
  • Correct expression for mass of water vapour: 0.3 pts
  • Correct expression for the latent heat (mvLm_v L): 0.3 pts
  • Correct expression for heat lost by water ((mmv)c(T0T1)(m - m_v)\cdot c\cdot(T_0 - T_1)): 0.3 pts
  • Expression for energy conservation: 0.4 pts
  • Correct expression for mass of water mm: 0.3 pts
  • Correct numerical answer m[630,680]gm \in [630,\,680]\,\text{g} (with correct dimension): 0.2 pts

Part iii (3 points)

At thermal equilibrium, there is as much heat flux to the skin as there is heat loss due to evaporation. The former (per area) equals κdTdx\kappa\frac{dT}{dx} and the latter (per area) equals LJm-LJm where mm is the mass of one molecule, which we find to be m=μ/NAm = \mu/N_A to get JμL/NAJ\mu L/N_A. Note that the minus sign comes from the fact that the particles diffuse from higher density areas to lower density areas. Now from the ideal gas law n=P/(TkB)=PNA/(TR)n = P/(Tk_B) = PN_A/(TR) to get

J=DddxrpTkB=DddxPNART.J = -D\frac{d}{dx}\frac{rp}{Tk_B} = -D\frac{d}{dx}\frac{PN_A}{RT}.

Now the pressure of the water vapour is related to rr through P=rpP = rp, where pp denotes the saturation pressure of vapour. So,

κdTdx=DLμRddxrpT,\kappa\frac{dT}{dx} = -\frac{DL\mu}{R}\frac{d}{dx}\frac{rp}{T},

where p=p(T)p = p(T) denotes the water vapour saturation pressure at the local air temperature; hence by integrating over xx we obtain

κ(TTs)=DLμR[p(Ts)Tsrp(T)T],\kappa(T - T_s) = \frac{DL\mu}{R}\left[\frac{p(T_s)}{T_s} - \frac{rp(T)}{T}\right],

where the index ss denotes quantities evaluated at the skin surface. Also, we have used the fact that rs=1r_s = 1, because at the skin surface, the air is in direct contact with water (due to sweating, skin is wet), so that prs=p(Ts)pr_s = p(T_s). Substituting ρ=pμRT\rho = \frac{p\mu}{RT} we obtain

ρ(Ts)=rρ(T)+κDL(TTs).\rho(T_s) = r\rho(T) + \frac{\kappa}{DL}(T - T_s).

Here we evaluate from the graph rρ(T)=24.3gm3r\rho(T) = 24.3\,\text{g\,m}^{-3} and κDL=0.51gm3K1\frac{\kappa}{DL} = 0.51\,\text{g\,m}^{-3}\text{K}^{-1}. Now we can draw this straight line onto the provided graph to find the intersection point at Ts=41.5°CT_s = 41.5\,°\text{C}.

Figure: Saturation water-vapour density \rho as a function of temperature (black curve, in g/m³ vs °C). The straight red line \rho(T_s) = r\rho(T) + (\kappa/DL)(T - T_s) is overlaid; its intersection with the saturation curve gives the skin temperature T_s \approx 41.5\,°\text{C}.

Solution 2 by Eppu Leinonen: One can also work directly with ρ\rho through the fact that n=N/V=MNA/(μV)=ρNA/μn = N/V = MN_A/(\mu V) = \rho N_A/\mu. Then the heat flux magnitude will directly become

LJm=LmDdndx=LmDNAμdρdx=LDdρvdx,LJm = LmD\frac{dn}{dx} = LmD\frac{N_A}{\mu}\frac{d\rho}{dx} = LD\frac{d\rho_v}{dx},

where ρv\rho_v is the density of the water vapour. Then with correct signs we get

κdTdx=LDdρvdx\kappa\frac{dT}{dx} = -LD\frac{d\rho_v}{dx}

from which by integrating and using ρv=rρ\rho_v = r\rho we get

ρ(Ts)=rρ(T)+κDL(TTs)\rho(T_s) = r\rho(T) + \frac{\kappa}{DL}(T - T_s)

and the solution proceeds the same way as in Solution 1.

Grading

NB! The ρ=pμ/RT\rho = p\mu/RT substitution can be done earlier so the schemes below represent only the relevant observations which can be done with ρ\rho already. Equivalent forms will give points (i.e. if using kk and NAN_A instead of RR in the middle steps).

  • Heat going away from skin (up) = heat going to skin (down) at equilibrium: 0.4 pts
  • Heat flux down κdTdx\kappa\frac{dT}{dx}: 0.2 pts
  • Heat flux up magnitude DLμRddxPT\frac{DL\mu}{R}\frac{d}{dx}\frac{P}{T}: 0.5 pts
    • Magnitude of heat flux up is LJmLJm: 0.3 pts
    • m=μ/NAm = \mu/N_A: 0.1 pts
    • n=P/(TkB)n = P/(Tk_B): 0.1 pts
  • Deducing that the direction of the heat flow is opposite to dndx\frac{dn}{dx} (explicitly mentioned or with the existence of the minus sign in the equations): 0.1 pts
  • P=rpP = rp: 0.1 pts
  • κ(TTs)=DLμR[p(Ts)Tsrp(T)T]\kappa(T - T_s) = \frac{DL\mu}{R}\left[\frac{p(T_s)}{T_s} - \frac{rp(T)}{T}\right] (integrating correctly): 0.4 pts
    • Or doing a change from dΔd \to \Delta in the derivatives, which has to be motivated properly (for Fick’s law one must state that JJ is constant due to conservation of particles).
  • ρ=pμ/RT\rho = p\mu/RT: 0.1 pts
  • Reading ρ\rho correctly (ρ1[800,815]gm3\rho_1 \in [800,\,815]\,\text{g\,m}^{-3}): 0.2 pts
  • Graphical method: 0.8 pts
    • Noticing that ρ(Ts)=rρ(T)+κDL(TTs)\rho(T_s) = r\rho(T) + \frac{\kappa}{DL}(T - T_s) defines a straight line in (T,ρ)(T,\,\rho): 0.8 pts
    • Any other valid numerical method that is explained is accepted.
  • Correct final result T[36,47]°CT \in [36,\,47]\,°\text{C}: 0.2 pts