96 Prublema €4 Solutions on Thermodynamics €4 Statistical Mechanics
Solution:
(a) The molecular number density at height h is denoted by n(h). From
the condition of mechanical equilibrium dp = -nmgdh and the equation of
state p = nkT, we find
1 mg
-dp = --dh.
P kT
Thus n(h) = no exp(-mgh/kT). Let Jf n(h)dh/JT n(h)dh = -, then
1
2
The average molecular weight of the atmosphere is 30. We have
8.31 x lo7 x 273
30 x 980
H= x In2 M 8 x lo5 cm = 8 km.
1 mg
P kT
(b) -dp = --dh is still correct and the adiabatic process follows
p('-7)/7T = const
where 7 = 5 w 7/2 (for diatomic molecules). Therefore -~ dT^7 - -
CU T 7-1
-_ mg dh. Integrating we get
kT
T - To = -(7 - l)mg(h - ho)/7k.
Furthermore,
_- dT -
- mg NN -0.1 K/m.
dh 7k
1099
The atmosphere is often in a convective steady state at constant en-
tropy, not constant temperature. In such equilibrium pV7 is independent
of altitude, where 7 = Cp/Cu. Use the condition of hydrostatic equilibrium
in a uniform gravitational field to find an expression for dT/dz, where z is
the altitude.
(UC, Berkeley)