Weak solutions 313
if and only if u
±
satisfy (10.2.25) in Ω
±
, the Rankine–Hugoniot (10.2.24) holds
true across Σ and, moreover,
N
0
[η(u)] +
d
j=1
N
j
[q
j
(u)] ≤ 0, (10.2.26)
where N
0
, N
1
, ..., N
d
denote the components in the directions t, x
1
,..., x
d
,
respectively, of a vector N orthogonal to Σ pointing to Ω
+
.
Remark 10.2 This characterization of course does not depend on the choice
of Ω
−
and Ω
+
: if these parts of the space R
d
× R
+
are exchanged, N is changed
to −N and the jumps are also changed into their opposite.
Many solutions of the type described in Proposition 10.2 have been observed
experimentally (in gas dynamics, for instance) and numerically. But there is no
global-in-time existence result for arbitrary jump front Σ.
The special case of a planar Σ reduces the problem to one space dimen-
sion. Solutions consisting of a planar front propagating with constant speed in
constant, homogeneous states are easily found by examining the one-dimensional
Rankine–Hugoniot condition. These solutions are called planar shock waves when
(10.2.26) is a strict inequality. There are also planar contact discontinuities, for
which (10.2.26) is in fact an equality. Planar fronts in gas dynamics are discussed
in detail in Chapter 13.
Spherical shocks are already much more complicated, as they involve a non-
constant speed and non-homogeneous states in general. As regards gas dynamics,
for instance, spherical shocks have received attention for decades: this goes
back to World War II and the atomic bomb research [73, 75, 106, 180, 204], in
which basic solutions were obtained by means of similarity/dimensional analysis
[181]; more recently the interest in the field has been renewed by (hopefully)
more peaceful and nonetheless fascinating phenomena (e.g. sonoluminescence,
cavitation) and various (potential) applications of shock focusing (extracorporeal
therapies, nuclear fusion, etc.); current research concerns complex fluids (van
der Waals or dusty gases, superfluids, etc.) and has incorporated group-analysis
techniques. The interested reader may refer, for instance, to the collected papers
in [198].
Regarding ‘arbitrarily’ curved fronts, as far as gas dynamics is concerned
there is a wide literature on transonic (stationary) shocks (see, for instance,
[30, 34, 220]) or other patterns, in particular those related to the reflexion of
shocks (see, for instance, [182,225,226]). In more general, abstract settings, there
are far fewer results on curved shocks. The main existence results are due to
Majda [124–126], M´etivier [133,136], Blokhin [17,18] and are based on a stability
analysis of reference fronts (known to exist, such as planar ones, or assumed) and
thus are local in time. The description of those results will be the main purpose
of Chapter 12.