4.1. Mass exchange vs. radiative heating/cooling
When the bulk of the energy content and the bulk of the mass content reside in different phases, a relatively small amount of mass or energy transfer between phases can have a large effect on the structure of a multiphase medium. Such a situation is believed to exist in the three-phase model of the ISM (McKee and Ostriker 1977), where the hot phase occupies most of the volume while most of the mass is in cold clouds. Physically, the effect of mass exchange (either by conduction or ablation followed by effective mixing) is to cool the hot phase, since a fixed amount of energy is being distributed among a larger number of particles. Since radiative heating and cooling depend on both density and temperature, mass exchange can affect the radiative evolution of the medium as well. We can illustrate the global consequences of mass and energy exchange between phases by considering a medium with uniform pressure and subsonic motions, in which mass exchange is driven by thermal conduction. The approximate time-dependent equations governing the medium are then
|   | (10) | 
|   | (11) | 
where  represents
the conductive heat flux. Note that these equations are appropriate 
in the single-fluid limit, corresponding to classical or mildly
saturated conduction
(Cowie and McKee 1977):
in the highly saturated suprathermal limit
(Balbus and McKee 1982), 
both the single-fluid approximation and the assumption of pressure
balance break down. 
The evolution of the medium is driven by the terms on the
right-hand-side of eq. (11), and 
may be dominated either by the effects of conduction or by the effects
of radiative heating  and cooling.
represents
the conductive heat flux. Note that these equations are appropriate 
in the single-fluid limit, corresponding to classical or mildly
saturated conduction
(Cowie and McKee 1977):
in the highly saturated suprathermal limit
(Balbus and McKee 1982), 
both the single-fluid approximation and the assumption of pressure
balance break down. 
The evolution of the medium is driven by the terms on the
right-hand-side of eq. (11), and 
may be dominated either by the effects of conduction or by the effects
of radiative heating  and cooling.
There is a crucial distinction between the heat flux term and the
radiative loss term in 
the energy equation: the energy entering or leaving a volume of radius
r due to conduction is proportional to r2
q( r
for classical conduction) whereas that due to heating or cooling 
is proportional to r3. Thus, there is a critical
length scale which enters the problem, which 
turns out to be the Field length,
 r
for classical conduction) whereas that due to heating or cooling 
is proportional to r3. Thus, there is a critical
length scale which enters the problem, which 
turns out to be the Field length,
 F
(eq. [8]), when mass exchange is driven by classical conduction.
F
(eq. [8]), when mass exchange is driven by classical conduction.
The temperature structure of the intercloud medium in a system of clouds
extending 
over a region of size R depends on the ratio of the Field length to 
R.
Balbus (1985)
developed an elegant electrostatic analogy for an ensemble of clouds in
a hot intercloud 
medium under conditions in which radiative heating and cooling are
negligible and the 
temperature is specified on the boundary of the ensemble. This
corresponds to the case R <<
 F. In a
steady state, the  
evaporation rate and the temperature structure in the intercloud 
medium are then determined by a solution of Laplace's equation with
Dirichlet boundary 
conditions. In the complementary case, R >>
F. In a
steady state, the  
evaporation rate and the temperature structure in the intercloud 
medium are then determined by a solution of Laplace's equation with
Dirichlet boundary 
conditions. In the complementary case, R >>
 F, global heat 
flows are insignificant and 
the temperature structure of the intercloud gas is determined by a
competition between 
cloud evaporation on the one hand and heating and cooling on the
other. Numerically, the Field length is
F, global heat 
flows are insignificant and 
the temperature structure of the intercloud gas is determined by a
competition between 
cloud evaporation on the one hand and heating and cooling on the
other. Numerically, the Field length is
|   | (12) | 
where T6
 T/106
K and
 T/106
K and  M-23
M-23
 
 M /
(10-23 erg cm3 s-1) is normalized to a
characteristic value of the radiative cooling rate for astrophysical
plasmas.
M /
(10-23 erg cm3 s-1) is normalized to a
characteristic value of the radiative cooling rate for astrophysical
plasmas.
To quantify the competition between mass exchange and radiative
heating/cooling, 
consider the spatially averaged effect of cloud evaporation on the hot
phase. This is  
meaningful only when the characteristic temperature of the hot phase
changes over a length 
scale which exceeds the mean intercloud separation
r0. This condition is guaranteed to be 
satisfied when r0 is smaller than
 F. When
r0 exceeds
F. When
r0 exceeds 
 F, then
mass exchange cannot compete with radiative heating and cooling anyway,
so the point is moot. If there are 
ncl(
F, then
mass exchange cannot compete with radiative heating and cooling anyway,
so the point is moot. If there are 
ncl( 3/4
3/4 r30) clouds per unit volume 
evaporating at a mean rate
r30) clouds per unit volume 
evaporating at a mean rate
 ev per
cloud, then the density of the intercloud medium changes at a rate
ev per
cloud, then the density of the intercloud medium changes at a rate
|   | (13) | 
where  ev is
negative for condensation. We may then use
ev is
negative for condensation. We may then use  
 ev to define an
effective evaporative cooling rate,
ev to define an
effective evaporative cooling rate, 
|   | (14) | 
(Begelman and McKee 1990).
The evaporative cooling coefficient
 ev is
analogous to the  radiative cooling coefficient
ev is
analogous to the  radiative cooling coefficient
 in that both
reduce the specific entropy s, but there are  
crucial differences between the two:
 in that both
reduce the specific entropy s, but there are  
crucial differences between the two:
 reduces the total
entropy  of a given volume of intercloud gas, whereas
 reduces the total
entropy  of a given volume of intercloud gas, whereas 
 ev
increases it;
ev
increases it;  reduces the energy density of the intercloud gas, whereas
 
reduces the energy density of the intercloud gas, whereas 
 ev
leaves it unchanged. Because of these distinctions,
ev
leaves it unchanged. Because of these distinctions, 
 ev
should not be included in the net radiative cooling function
ev
should not be included in the net radiative cooling function
 . However, the relative 
impact of mass exchange and 
radiative heating/cooling on the thermal state of the intercloud medium
can be expressed by the radiation/evaporation ratio
(Begelman and McKee 1990),
. However, the relative 
impact of mass exchange and 
radiative heating/cooling on the thermal state of the intercloud medium
can be expressed by the radiation/evaporation ratio
(Begelman and McKee 1990),
|   | (15) | 
When  M
M
 
 M /
M /
 ev is 
>> 1( << 1), then radiative heating and cooling (mass exchange) 
determines the thermal state of the intercloud medium.
ev is 
>> 1( << 1), then radiative heating and cooling (mass exchange) 
determines the thermal state of the intercloud medium.
One can express  in
terms of quantities which characterize the structure of the 
two-phase medium. Writing the evaporation rate in the form
 in
terms of quantities which characterize the structure of the 
two-phase medium. Writing the evaporation rate in the form 
 ev =
4
ev =
4 r2c
 r2c
 h
csf, where cs
is the isothermal sound speed in the hot phase, we have
h
csf, where cs
is the isothermal sound speed in the hot phase, we have
|   | (16) | 
r0 may be eliminated in favor of the cloud filling
factor f (assumed to be << 1) by substituting 
rc/f for 
r03 / rc2. In
the limit of saturated evaporation F ~ a few
(Cowie and McKee 1977),
while 
F ~  / 4 in the
Nulsen (1982)
model of ablation. In the classical conduction 
limit, F is twice the "saturation parameter"
 / 4 in the
Nulsen (1982)
model of ablation. In the classical conduction 
limit, F is twice the "saturation parameter"
 '0 derived by
Cowie and McKee (1977),
with the result that
'0 derived by
Cowie and McKee (1977),
with the result that
|   | (17) | 
Cloud evaporation thus determines the intercloud temperature for
rc > r30 /
 F2.
The corresponding condition on the filling factor is
F2.
The corresponding condition on the filling factor is
|   | (18) | 
or f > (r0 /
 F)6;
for f ~ 0.03, as in the ISM, this will
be true if
F)6;
for f ~ 0.03, as in the ISM, this will
be true if  F
F
 2r0. In terms of the 
sound-crossing time across rc (measured in the hot phase),
ts ~ rc / 2cs, and
the radiative cooling time in the hot phase, 
tc ~ 5kTh / 2nh
2r0. In terms of the 
sound-crossing time across rc (measured in the hot phase),
ts ~ rc / 2cs, and
the radiative cooling time in the hot phase, 
tc ~ 5kTh / 2nh
 (Th)
, we may express the condition for mass 
exchange to dominate globally in the form
(Th)
, we may express the condition for mass 
exchange to dominate globally in the form
|   | (19) | 
Writing (18) in the form 
r0 < r1/3c
 F2/3,
we see that the intercloud spacing in a 
conduction-dominated medium must also be smaller than the Field
length. This has  
important consequences for the thermal stability of the hot phase in a
conduction-dominated system. Since
F2/3,
we see that the intercloud spacing in a 
conduction-dominated medium must also be smaller than the Field
length. This has  
important consequences for the thermal stability of the hot phase in a
conduction-dominated system. Since
 F is
roughly the minimum wavelength which is thermally unstable
(Field 1965),
potentially unstable regions must contain many clouds. The
conduction-modified 
condition for thermal instability is obtained simply by including
F is
roughly the minimum wavelength which is thermally unstable
(Field 1965),
potentially unstable regions must contain many clouds. The
conduction-modified 
condition for thermal instability is obtained simply by including
 ev
in Balbus's (1986a) 
criterion (eq. [4]):
ev
in Balbus's (1986a) 
criterion (eq. [4]):
|   | (20) | 
(Begelman and McKee 1990). 
nh
 ev /
Th is
generally an increasing function of Th: for 
isobaric perturbations nh
ev /
Th is
generally an increasing function of Th: for 
isobaric perturbations nh
 ev /
Th ~ q
ev /
Th ~ q
 Th7/2(Th1/2)
for classical (saturated) conduction.  
Therefore, evaporation has a  stabilizing influence on the hot
phase, and in a  
conduction-dominated medium thermal instability will be inhibited by the
presence of evaporating clouds
(Begelman and McKee 1990).
This will be true even if the radiative processes place 
the hot phase in a thermally unstable regime. However, it should be
noted that the cooling 
time scale in the hot phase of a conduction-dominated medium is shorter
than the radiative 
cooling time scale. Therefore, conduction cannot stabilize a hot phase
over a time scale 
which is longer than the time scale for radiative thermal
instability. However, it can lead 
to the hot phase cooling down somewhat before the onset of thermal
instability. Since 
thermal conduction generally becomes less important at low temperatures,
such a system 
may evolve to a state in which evaporative cooling no longer dominates,
whereupon thermal 
instability may occur. Since the Field length is generally a strongly
increasing function of 
temperature, the operation of thermal instability may lead to the
production of smaller 
and more closely spaced clouds than would have formed in the hotter medium.
Th7/2(Th1/2)
for classical (saturated) conduction.  
Therefore, evaporation has a  stabilizing influence on the hot
phase, and in a  
conduction-dominated medium thermal instability will be inhibited by the
presence of evaporating clouds
(Begelman and McKee 1990).
This will be true even if the radiative processes place 
the hot phase in a thermally unstable regime. However, it should be
noted that the cooling 
time scale in the hot phase of a conduction-dominated medium is shorter
than the radiative 
cooling time scale. Therefore, conduction cannot stabilize a hot phase
over a time scale 
which is longer than the time scale for radiative thermal
instability. However, it can lead 
to the hot phase cooling down somewhat before the onset of thermal
instability. Since 
thermal conduction generally becomes less important at low temperatures,
such a system 
may evolve to a state in which evaporative cooling no longer dominates,
whereupon thermal 
instability may occur. Since the Field length is generally a strongly
increasing function of 
temperature, the operation of thermal instability may lead to the
production of smaller 
and more closely spaced clouds than would have formed in the hotter medium.
It is instructive to apply the ideas discussed above to the three-phase
model of the ISM
(McKee and Ostriker 1977).
The three-phase ISM consists of cold HI clouds 
surrounded by warm HI and HII envelopes, all embedded in a pervasive hot
ionized medium 
(HIM). The physical conditions in the HIM are governed by mass exchange
with the clouds 
and energy injection by supernovae. The model is intrinsically
time-dependent: A given 
element of gas is compressed and heated by SNRs at intervals of about
5 × 105 yr, and
this makes its evolution difficult to analyze using concepts developed
to treat steady-state 
or slowly evolving systems. Nonetheless, it is of interest to evaluate
the Field length and 
the radiation/evaporation ratio. Using the fit to the cooling function
of Raymond, Cox and Smith
(1976)
for cosmic abundances, 
 (T)
(T)
 1.6 ×
10-19T-1/2 erg cm3
s-1 (105 K
< T < 4 × 107 K), multiplied by an
enhancement factor
 1.6 ×
10-19T-1/2 erg cm3
s-1 (105 K
< T < 4 × 107 K), multiplied by an
enhancement factor 
 
 10
10 1
1
 10 to take account of
nonequilibrium ionization and density inhomogeneity near conduction fronts
(McKee and Ostriker 1977),
we have
 10 to take account of
nonequilibrium ionization and density inhomogeneity near conduction fronts
(McKee and Ostriker 1977),
we have 
 F =
44(
F =
44( c1/2
T36 /
c1/2
T36 /
 4
4
 11/2) pc, where
11/2) pc, where
 4
4
 p /
104k and 
T6
 p /
104k and 
T6  Th/106 K. We can write condition (18) in
the form
Th/106 K. We can write condition (18) in
the form
|   | (21) | 
It is evident that the relative importance of conductive and radiative
energy exchange 
is sensitive to conditions in the hot phase, particularly to
Th, as well as to the filling  
factor and typical size of clouds. Under the conditions deduced by McKee
and Ostriker (T6 = 0.45,
 4 = 0.36,
4 = 0.36,
 1
= 1, rc = 2.1
pc, and f = 0.23), condition (21) is marginally 
satisfied. Equivalently, the radiation/evaporation ratio is given by
R = 0.38, which implies
that evaporative cooling dominates radiative cooling and that the HIM is
thermally stable. 
(The argument that evaporation can stabilize the HIM is originally due
to McCray [1986].) 
However, even a small amount of cloud ablation by hydrodynamic processes
(Section 3.2) or a 
slight increase in the HIM temperature would lead to a drastic increase
in the energetic 
importance of evaporation. If the typical clouds were sufficiently small
that conduction 
were saturated, i.e., for
1
= 1, rc = 2.1
pc, and f = 0.23), condition (21) is marginally 
satisfied. Equivalently, the radiation/evaporation ratio is given by
R = 0.38, which implies
that evaporative cooling dominates radiative cooling and that the HIM is
thermally stable. 
(The argument that evaporation can stabilize the HIM is originally due
to McCray [1986].) 
However, even a small amount of cloud ablation by hydrodynamic processes
(Section 3.2) or a 
slight increase in the HIM temperature would lead to a drastic increase
in the energetic 
importance of evaporation. If the typical clouds were sufficiently small
that conduction 
were saturated, i.e., for
|   | (22) | 
(Cowie and McKee 1977; Balbus and McKee 1982), the appropriate version of condition (19) would be
|   | (23) | 
In the McKee-Ostriker picture, each region of HIM is overrun by another
supernova remnant before it has time relax to a stationary state with
 
 1. Stochastic heating
by SNR shocks thus leads to discontinuous trajectories in the p -
V plane, and heating 
is balanced by radiative cooling. In the galactic fountain model
(Shapiro and Field 1976; 
Wang and Cowie 1988),
the heat is advected into the galactic halo. If clouds are effectively 
ablated then the accelerated lowering of Th by
evaporation may allow the large tracts of 
the ISM to cool to a homogeneous state at 
T
 1. Stochastic heating
by SNR shocks thus leads to discontinuous trajectories in the p -
V plane, and heating 
is balanced by radiative cooling. In the galactic fountain model
(Shapiro and Field 1976; 
Wang and Cowie 1988),
the heat is advected into the galactic halo. If clouds are effectively 
ablated then the accelerated lowering of Th by
evaporation may allow the large tracts of 
the ISM to cool to a homogeneous state at 
T  104 K. The intercloud medium remains 
thermally stable until radiative cooling begins to dominate over
evaporative cooling, at Th
104 K. The intercloud medium remains 
thermally stable until radiative cooling begins to dominate over
evaporative cooling, at Th
 105
K. Since the Field length is a strongly increasing 
function of Th, the onset of
instability at a reduced temperature may lead to the formation of
sub-parsec size clouds.
 105
K. Since the Field length is a strongly increasing 
function of Th, the onset of
instability at a reduced temperature may lead to the formation of
sub-parsec size clouds.