A NNALES DE L ’I. H. P., SECTION C
A. B OURGEADE
P H . L E F LOCH
P. A. R AVIART
An asymptotic expansion for the solution of the generalized Riemann problem. Part 2 : application to the equations of gas dynamics
Annales de l’I. H. P., section C, tome 6, n
o6 (1989), p. 437-480
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An asymptotic expansion for the solution of the generalized Riemann problem.
Part 2 : application to the equations of gas dynamics
A. BOURGEAD
E, Ph. LE FLOCH and P. A. RAVIART
Mathématiques Appliquées, École Polytechnique, 91128 Palaiseau Cedex, France Vol. 6, n° 6, 1989, p. 437-480. Analyse non linearie
w e apply Lo me gas uynamics equations me general method of
approximation
for thegeneralized
Riemannproblem proposed by
Le Floch-Raviart[6].
We both consider theequations
of gasdynamics
in
Lagrangian
coordinates in slabsymmetry
with a source term and theequations
in Eulerian coordinates inplane, cylindrical
orspherical
symme-try. Explicit
formulae are derived for the first orderapproximation
of thesolution of the
generalized
Riemannproblem.
Such anapproximate
sol-ution may be
easily
used to construct a second order version of the numerical Godunov method.Key words : Shock, nonlinear hyperbolic systems, asymptotic expansion, gas dynamics.
RESUME. - Nous
appliquons
ausysteme
de ladynamique
des gaz la methodegenerale proposee
par Le Floch-Raviart[6]
pourl’approximation
du
probleme
de Riemanngeneralise.
Nous considerons a la fois lesequa-
tions de la
dynamique
des gaz en coordonnéeslagrangiennes
ensymetrie plane
avec terme de source et lesequations
en coordonnees eulériennes ensymetrie plane, cylindrique
ouspherique.
Des formulesexplicites
sontobtenues pour
l’approximation
dupremier
ordre de la solution du pro- bleme de Riemanngeneralise.
Ces resultatspeuvent
etre facilement utilises pour construire une version d’ordre 2 de la methode de Godunov.Classification A.M.S. : 35 L 65, 35 D 05, 35 C 05, 76 N 15, 35 L 67.
Annales de l’Institut Henri Poincaré - Analyse non linéaire - 0294-1449 Vol. 6,’89/06!437~44.~;6.40’ cQ Gauthier-Villars
438 A. BOURGEADE, PH. LE FLOCH AND P. A. RAVIART
1. INTRODUCTION
_ __ ~,_ _ - __ _ _ _ ~ ~-_~ _r _ . _____,_ ~____~_~ L- LL- ---
of the solution of
the generalized
Riemannproblem.
Westudy here the
of the solution of the
generalized
Riemannproblem.
Westudy
here thegas
dynamics
system in bothLagrangian
and Eulerian coordinates andwe
apply
thegeneral
method ofapproximation proposed
in Le Floch- Raviart[6].
In the first
part [6],
we have consideredsystems
of conservation laws of the form:J v V V
problem
for( 1. 1)
consists insolving
the associatedCauchy problem
withthe initial condition:
ITIx_ 0)= IT.. (xl if TT~ if x~(1_ ll _ 21
system ( 1. 1)
isstrictly hyperbolic;
each characteristic field issupposed
tobe either
genuinely
nonlinear orlinearly degenerate. First,
we consider thefollowing
classical Riemannproblem:
a __~ a _ ___~_ - __~ _ _ - .. - - . -.
f (U°l
= f (0, 0.U°),
there exists a
unique entropy
solution of(1.3)-(1.4), depending only
onthe
self-similarity variable 03BE = x,
which consists ofp + 1
constant statest
separated by
pelementary
waves(shock
wave, contactdiscontibuity
orrarefaction
wave).
Then,
let us recall that theproblem (1. 1)-(1.2)
admits anentropy
weak solutionU = U (x, t), locally
defined in theneighbourhood
of theorigin (x, t) _ (o, 0),
which has the same structure as that ofU°.
Fordetails,
werefer to Li Tatsien-Yu
Wenci[8]
andHarabetian [5].
In
[6],
we looked for anasymptotic expansion
for the function U in the form:_ _ .. r, _ _t_ .~ , b ., x , _ .... _
439
say x = (p
(t),
has also aTaylor expansion
of the form:( 1. 6)
cient
(1k.
w
Furthermore,
we havegiven
error bounds for theapproximate
solutions constructed from
( 1. 5)-( 1. 6).
In this paper, we consider first the
equations
of gasdynamics
inLagran- gian
coordinates and in slabsymmetry
with a source term and ageneral equation
of state. Westudy
next thesystem
of gasdynamics
in Eulerian coordinates and inplane, cylindrical
orspherical symmetry
with an equa- tion of state which is ageneralization
of that of apolytropic perfect
gas.In both cases, we determine the first order
approximation
of the solution of( 1. 1)-( 1. 2),
i. e. we deriveexplicit expressions
for the function( ~)
of theexpansion (1.5).
These results are in fact identical with those of Ben Artzi-Falcovitz([1], [2])
who have used afairly
differentmethod.
Finally,
let us recall that theapproximate
solution of(1. 1)-{ 1. 2)
may beeasily
used to construct a second order version of the Godunov scheme.Such a numerical scheme appear to be very efficient in the numerical
computation
of verystrong
shocks([1],
Van Leer[10]).
An outline of the paper is as follows.
Section
2 is devoted to thetechniques
ofasymptotic expansion
of Le Floch-Raviart[6]
for a nonlinearhyperbolic system
under ageneral
nonconservative form.Then,
in Section3,
we consider thesystem
of gasdynamics
inLagrangian
coordina-tes. In Section
4,
the Euleriansystem
is treated.2. OUTLINES OF THE GENERAL THEORY
Let us
begin by recalling
thetechniques
ofasymptotic expansion
ofLe Floch-Raviart
[6].
For the sake ofsimplicity,
we shall restrict ourselvesto
systems
of the formx ~
aai i.r .. iii VV lriiV wVV iiViiVViiVVl
variables V such
that
T T - rh l Vl ,") ")B
~*j U. tj~~ ~ 2014 u, ~i
states Rl c RP. We first need to
express
the results of[6]
in terms of theVol. 6, n° 6-1989.
440
U of the
generalized
Riemannproblem (2 . 1)-( 1. 2),
thesystem (2 . 1)
isequivalent
to the nonconservative system:av .
.,~ n av ~ , ~ n
," ~B’
~
strictly hyperbolic,
so that theeigenvalues
of thematrix
B(V)
are real anddistinct:
~,, (~ (~ ... (V’), d v E ~.
eigenvectors
andby {l i(V)T}
1 ~i~pa
basis of left(row) eigenvectors,
i. e.r; ~V) _ ~~ (V) r~ (~~ li ~~~ B ~V) _ ~i ~v)
genuinely
nonlinearD~,I ( V) r; ( V) ~ 0,
VV E ’~441
«
~/ ~~
T~
of the form
- - ~-. , ./xB
~i Ol w OA B~’ ~/ B~ * 2014~7* ~
eroth order term
V0=V0(03BE)
in(2.6)
isgiven by
~ 7~
where
U° (x, t)
= IJ°(~) ~ _ ~-
is theentropy
weak solution of the classicalt Riemann
problem
~T To ,
rarefaction waves, shock waves or contact discontinuities. We denote
by Q?
and?~
the lower and upper bounds of thespeeds
of the i-waveVoL 6, n° 6-1989. -
442 H. rn. LC r. ~~.
t -*- ! ! - ~ ~~~L~~~ ~’~7 -*" t B 2014 ____ ~ --~ ~ ~~~~ ~ t-~ j ~ F ~~~~ ~~~~~ ~~~~~~ t~ ~~~ ~~~t~ m. m ~J~JL~~ ~ . TT ~~ V ~~ ~~~
a shock wave or a contact
discontinuity,
weget
rr9 = fr9 - fT9to
[9].
Next,
we note[8]
that the function V has the same structure than the solutionV°
in aneighbourhood
of theorigin.
The(p + 1 )
smoothnessdomains of V are
separated
eitherby
a smooth curve denotedby
x = cpi(t)
such that
, -, - d .__ no
_
~
__ _____. ____ _ __ ____ ______
~ (x, t)E
(F~ xI~ +;
such that
_
_ _ _ _ _ __
__ _~ 1 _ _ _ _
_
1
__ _ _ __- _ _ _. _ . __ _ _ -
Ti B-_-_
_-
cpi, in the form
cn: (t~ _ ~’
( 2 . 91jr -- - jt. --- - B2014 ~
~-... /~
in a more
complicated
way..Replacing
Vby
theexpansion ( 2 . 6)
in( 2 . 3),
we derive as in[6]
theordinary differential equations
satisfiedby
the functionV’~, k >_ 1.
Weobtain:
_ ~ _ _ _ .~ _ _ _
matter to check as in
[6,
LemmaI],
thefollowing property:
if V1 is apolynomial
ofdegree
less than 1 forOlk-l,
then thefunction §
t2014~a"‘ (~)
Annales de l’Institut Henri Poincaré - Analyse non linéaire
443 is a
polynomial
ofdegree
less than k - 1. For k =1,
we have1~ W tL... 1 1l 111 ~11V
Since for
W2
in the function:i~ a a vau u v asar.v
y ~ , !~ ~ . r
C=C(W1, W2) such
thata Lt
‘Li ~ 7
- _ _ _ _______ _ _-_ _
_j __ __ __ _ ‘ . - _ / . __ _.._ _ _ . _ _ __
the function
V°.
For
integrating
the differentialsystem (2. 13),
we have todistinguish
between the two
types
of intervals:]~°, a° 1[
and]~°, ~°[.
Let us firstconsider the case of an interval
] a°, ~° 1 [
where the functionv°
takesthe constant value
V?,
with the convention thatao
= - ~, 03C30p+ 1= + oo . We have theanalogous
of[6,
Lemma2] :
LEMMA 2 1. - Assume
that ~ belongs
to the interval]a°, 1[,
0 _ i_ p.
Then, for
all k >_1,
thegeneral
solutionof
thedifferential
system(2. 13)
isgiven by
t1k /~1 - /~ ~ !t1°llk Dk /~1 l’! 1 A1
..rrvr v ~ ’ YV WrV WI J vJ wa I "l ai. ilrfLilWiVaa
of
degree
_ k -1 with values in !~p whichdepends only
onV °,
... ,Vk -1.
Moreover, for
k=1,
we haveP~
= h(o, V°). ( 2 . 1 S)
to an i-rarefaction wave for
V°.
It is easy toverify
that:h . iV° I § 1 1 = E
_ ..___a .,__...,...»... v~ ’I’ ’I’ ~ J 1 ~ I ~ ~ ’1"’1" v vv v
p p
. va. vj u
444 A. BOURGEADE, PH. LE FLOCH AND Y. A. KAVlAKl
i
,. d .
1 m- .w , ___~_~.~~~~ ~~~ --la t - i . lv . Ja " ..- ~_ - -
1 iVlIVV’ y V V V 4H.i11
’.,, t
- --~-7 _-_- ---- _ . _ . _____ _ ~ . ‘ ~ r i n
{ ~I p 1
..__-_ _ _
_i B . t 7l/ "-;17 _ J ~ ~
P
that in
(2. 19) 03B2ii
isequal
to 1.By differentiating
the relation B ri(~~) _ ~
ri/ - dVOB
. -.--- -- - -.--- __ _ _
~~__T _ _-~J__ __- --_- _ _
Since
~yo
20142014
isproportional
tor~(V~),
we have/
Thus we find
auu
LEMMA 2. 2. - Assume
that ~ belongs
to the interval6i L.
then, thedifferential
system(2. 13)
isequivalent
to thealgebraic equation (2. 21 )
andthe
(p -1 ) coupled differential equations (2. 18) for j ~
i.In order to obtain the function
Vk,
we need to determine the vectorsintroduced in Lemma 2 . 1. Let us then consider the
jump
relations satisfied
by
a functionVk
at adiscontinuity
ofV°. First,
at ashock or a contact
discontinuity,
we may write theRankine-Hugoniot jump
relationcorresponding
to thehyperbolic system (2. 1):
__ / /~1 fT n r Y* !T TBl /~1 ~1~1B
diffeomorphism O,
we obtain,., +i rm «rii - r r m « n ii 1
[6,
Lemma4] :
LEMMA 2. 3. - Assume that
V°
contains an i-shock wave or a i-contactdiscontinuity.
Thenfor
all k>__ l,
there exists a vectorqi‘
E whichdepends only
onV °,
..., and ...,~ -1
such thatl - 6°~k+ i Vk ,
Vol. 6, n 6-1989.
446
r k =1, we haveq~
=(V°) C~’~V°) - a°)
hC~~
Recall that and are the smooth characteristic curves
which bound
the corresponding
rarefaction zone of V. We set~i(t)- ~ ~k. i-+1~ § i (t) ~ £ 8f . P ~ ~ .
Lemma
5] :
LEMMA 2.4. - Assume that
V°
contains ani-rarefaction
wave.Then, for
qk =
the initial data
VL, VR
definedby
VL(X)=
LEMMA 2. 5. - For all
integer
k ?0,
we havevo - vL, vR.
result:
THEOREM 2.1
(Le
Floch-Raviart[6]).
- Let k>__
1 be aninteger
andsuppose thet the
function V1= Vj (~)
and the numbersai
or thepairs
(a~, 6i),
1 _ i _ p, have beenalready
determinedfor t =1,
..., k -1. Then,if ‘
is smallenough,
there exists aunique function
Vk =V~‘ (~)
andAnnales de l’Institut Henri Poincaré - Analyse non linéaire
. t tr . ~ Ir ~ bw ~ i . i 1 _ .
equations (2.13), (2.14), (2.23), (2.25)
and(2.26).
3. THE GAS DYNAMICS
EQUATIONS
IN LAGRANGIANCOORDINATES
We
begin by considering
the gasdynamics equations
inLagrangian
coordinates and in slab
symetry
with a source term[4]
’
aT a~. I
the internal energy per unit mass, the total energy per unit mass, and the constant h
represents
a source term. Wesupplement
thesystem (3.1)
with anequation
of state of the form_ ~ ,_ _.
~ i,
u,S}
where thespecific entropy
S is definedby
(3.1)
becomes:, ,
and q = q
(T, S) by
an ari I an
Vol. 6, n" 6-1989.
448 1 1 LVt.I 1 . !’1.
? "~~C3
~ ~* ~
-- ________-______ ___-__ __ ____
_J___~ ~__-)
~1 n m Y’
-
-- - - -_--- . -- --- - - ----
--- -- - , . , -- -
- --- ---- --- ----
--w--- --w--- . --- -- - ’ . J
/ I ’ ,’ 1 ’
G114
nonlinear and the second one is
linearly degenerate.
As an
example,
we consider thefollowing
usefulgeneralization
of theequation
of state for apolytropic perfect
gas- -2 i _ v
we have
equivalently
_ _ _ _ __ _ __ ~
C72014’7 ’ .. _ a_ _
~r
t
Now,
for each stateV°=t / u° ,
thecomponents (ai) 1 ~ t ~ 3
of a stateB So
/’B
V = (u S) on the are
given by
or
equivalently
. i7V .... V 1161. y..., 1.11V
h - -
.. .., ... _,.,_.
450 A. BOURGEADE, PH. LE FLOCH AND P. A. RAVIART t
- 2014~ ~~~~
~~~~~M~ ~A~~~~~j ~~~*At~~~ ~i± ~.
the first order
approximation
Here
p = 3
and we denoteby To, u°, p°, co, gO,... (respectively i 1, u 1, pB cB gi, ... )
thequantities
associated with the stateV ° (resp.
Let usrecall that the zones of smoothness of
V°
are numbered from i = 0 to i = 3.(See Figs.
3.1 and3.2.)
Since
V°
is theentropy
weak solution of the classical Riemannproblem
for
(3.1),
it consists of four constant statesseparated by i-waves, 1 __ i __ 3.
Recall that the 1- and 3-waves are rarefaction waves or shock waves, while the 2-wave is a
stationnary
contactdiscontinuity x = 0 .
Moreoverthe
velocity u°
and the pressurep°
are continuous at the contact disconti-nuity.
Let us denoteby u*
andp*
theirrespective
values In thesequel,
we will assume that the functionsV°
has been determinedexplici- tely :
see for instance[4], [9].
Let us now compute the function of the
expansion (2.6)
associated with the system
(3.1).
As in Section2,
we setV i l ~ ~ - ~’ rv l ~ 1 r T ° l ~ 11 ~ ~.- ILD
h 0!’1 T /~1 !1 ’t 17 N /1T1 1~ 1~1 !1 IV ~ N l y . 1 ‘ 1 ‘ 1 11 !11 in1 /r
Lemma
2.1,
we deduce thegeneral
form of the functionsa~
in an interval whereV°
is constant.LEMMA 3.1. - In each interval
] a°, a° 1 [,
i =0, 1, 2, 3,
there exists threereal
2, 3,
such that_.__ _~ ". h
rarefaction
zone63 [ = ] gi,
Thenusing (2.18)
and Lemma2.2,
weobtain the
following expressions
for thea~’s.
LEMMA 3. 2. - Assume that
V °
contains ani-rarefaction
wave(i =1
or3). Then,
there exist two constantsbl, 2
andfor
i =l,
andb3,1
andb3, 2 for
1=3,
suchthat for
i =1and ~ E ] - g° [
VoL 6, n° 6-1989.
452 c~. a aa ~ ar a . s ~. a~ ~ . a~
~r~~ ~~ /~~
_ . ~~,. ~._.__.._ua s_~_~ ~~.." ___~_~_~_~ ______~___-_ _-_ __ _-___
--
~___ _ ____-__J _~ _-__
_-
t / ~ (1
we know that
d _
( ~)
becomes here:/ a~ B o a ,~o / L
-
(3.15).
Infact, (3.15 b)
is an ODE for the function a2, whosegeneral
solution is obvious.
Next, knowing (3.15 c) gives
an ODE for a3 which isagain easily
solved.Finally,
thealgebraic equation (3.15 a) gives ai ..
In the
particular
case of theequation
of state(3.6),
we can obtain moreexplicit
formulae.LEMMA 3.3. - Assume that
(3.6)
holds.Then,
thefunctions of
Lemma 3.2 are
given for ~ E ] -gL, g°[ by
.. , , ,
-~ ---
454
~~o -Or L,.
know that
C‘~ r~l _ ~.~o __ o r~~ _ ~
~ 2 Y/~Y ’~ 1 ) /.
and
~ - __ ____ 2014 2014201420142014
_____~ ___r________ 2014~ 2014 ____ _______.. _ ~B~
wi B’O ~ ~0B
so rnar
rr c
1
auu
on /
Let us now derive the
boundary
relations satisfiedby
the functionV~
at the discontinuities ofV°.
Consider first rarefaction waves. From Lemmas 2.4 and3.2,
we have:LEMMA
3.4. -If yO
contains aI-rarefaction
wave, the constantsand
bl, 3 of
Lemma 3.2satisfy
~ 2014 ~. 1 o~
.
_...._. ~ .._ ._~.._ ____
______._____~ r. ~r__ ____ ~_ ~ o
.... /’ .,.0 n~ - _. i .~0 ~ n~ , - ~ z
Jtt T ~H~ ~~ ~ t~~ ~ ~~
Lemma 3.2
satisfy
~ ~ - n ~~o~
~ ~.~o ~ ~,~o - n1 ; - 1 ?
Define the function
p 1= p 1 (~) by p 1= op ~ ,r 1
+( B -~- ) as S 1.
Then at thecontact
discontinuity,
weget
LEMMA 3. 5. - 7he
functions u 1= u 1 (~)
andp 1= p 1 (~)
are continuous at~=o.
Proof -
At the contactdiscontinuity,
theRankine-Hugoniot jump
relations for the
system ( 3.1 )
becomer i r i m
f~.~ ~ t~..i ~ 1.
and
VoL 6, n° 6-1989.
456 ___rr_~:_~~_ _ _~ ~ _ i ~ _ ~ ~ 1..
~ r - n r
3 3
~rt 1 ~ ~Tt 1 ~T~
Lemma 3.1 f or i = 0 and i = 3.
LEMMA 3.6. - We have for 1 i 3
shock
discontinuity
of V". Let us assume that a state{i,
u,p)
is connected to a state(ia,
ua,pa) by
a shockdiscontinuity. Introducing
theHugoniot
function
H~ (T, p)
H _ fi_ (3.251
L J
1:=
By writting
...
=G~~Q + ..., P° +tPa - .., ... )~
UO + t u
~ _t_ _ _t_ ~’--~~~’2014--’~-- --- L ____ __..
_1 -1/ -O , r~B _1 _1 i-O n~ -~-
~1 2014~1/~0 n~
Vl 611V Vl ...-
LEMMA 3.7. - When the pressure p is
given by (3.6),
the relations(3.28)
and
(3.29)
may be written :/ r. B
ana
and
___.__~..__
_ .r_ ~.~_ _.~__~.._~a ~___.~___~~, .._ ..~_ ~__ _~___ __ _ ____
(see [4], again)
for a I-shock waveVol. 6, n" 6-1989.
458 A. BOURGEADE, PH. LE FLOCH AND P. A. RAVIART
we obtain
Now,
we have~
.
J~- ~ - ~ ~ ~ ~ . ~ ~ 2014
~
/
1B
1 1nm
Annales de l’lnstitut Henri Poincaré - Analyse non linéaire
459
function G
x T
logether witn this gives ,o I Tv - 11
cum -
We are now able to determine
explicitely
the functionV1. By
Lemmas 3.1 and
3.2,
we haveonly
tocompute
theconstants ai, j,
1i, j 3,
of Lemma 3.1.
We
havealready
noticed in Lemma 3.6 that and a3, ~,1 j 3,
are known.Using
Lemma3. 5,
we may set’
~,i - ~.1 /~YB ~,1 - ~i /o ~oB
and
p*. Next,
we will show how tocompute
the coefficients fromu*
and
p*.
It is worthwile to notice that in the construction of the second order accurate version of Godunov method ofapproximation
of(3.1),
asdeveloped
in[1],
we needonly
tocompute
thepair u~, p*
without cons-tructing
the whole functionV 1.
THEOREM 3.1. - l .
If
thefunction V °
contains aI-rarefaction
wave, wehave
where
~-. AJ v 1+ rvc
~ 1 /0 t
___ _, _ _ _____
460
(’ / a B01 f / a B~ 1
I
f / a B01 f -~~ / ~ B01
/
~"
B-~* ’*/ ~-~.~~-~~ f~~ tH~~~ ~~~ .7*" "20142014*~-~ ~’ A~ mFMA t 201420142014
i~.~2014 / ~ B 0
~ ’ ~~~* ~-~~~~t~~~~~~jL ~~~~~
B*’* ’/
and Lemma
3.1,
we have on one handL
ana, oy
/ _ 1
auu
and 3.4 we have
,
n i n ~ , .., of _f)
we nave
, i > i v
(3.39).
The case of a 3-rarefaction wave is similar.’
Consider next, the case of a 3-shock wave
(say !).
We may write from(3.28):
Vol. 6, n° 6-1989.
462
. i.~ ~.m ~.~ t i^ ~ i~ " ---- 1_ ____
amu
hand,
we have in a similar way_ - ~
-
-, - -, - - -
, , - ’ , « , ’Irr.
f.1.11Bi L/
(,/,~. ~ ~ V’; ~~ V(~.11 ~~~
from their values
at ~=0: 1 .J:
/n v ~.. ~ iB t~
ana
yields ( 3.42 a) ..
We
emphasize
that the 2 x 2system given by
Theorem 3. 1 isalways numerically
solvable. Afterhaving
determinedu*
andp*,
we nowcompute
the constants ai, J.
THEOREM 3. 2. - For i =
1, 2,
we havei f ~,1 1
no
ana
~j ’ v~.~..w~.~... w
r.wvvi mv Jrrrw
~~ _ _ - ~ r’~C’’T ~ ~ ~ .
Vol. 6, n" 6-1989.
464 !~. r i l. i r . !i. 1
I
For a1, 2
or a2, 2, we first consider the case where for instance the functionV°
contains a 1-rarefaction wave.By
Lemma3. 4,
we havea, (-~°+Ol=a, (-~°-0~.
and
J B / ~ x /
contains a 3-shock wave, we use Lemma 3. 7 and we write
. , " ..
~ aG ~° , . " __ ~ aG ~° , . " __ ~ aG ~° , . " __
~1 (~°+0) _~’°. ,~~
,~1 ‘~0-O~
Finally, as
atrivial
consequence ofTheorems
3. 1 and 3.2,
we obtain COROLLARY. - The valueso.f
thefunction
i 1at 03BE
= 0 aregiven by
..1 ln ~ - 1 f..l L 1 « cc~
AN ASYMPTOTIC EXPANSION FOR THE GAS DYNAMICS 465
~l~
Let us close this section by computmg tne constants ansmg m 1 neorem 3 .1 in the case of the
equation
of state( 3 . 6) .
As a direct consequence of Lemmae 3.3 and3.7,
Theorem 3.1 and(3.36), (3.37)
and(3.38),
weobtain:
THEOREM 3 . 3. - 1.
If
thefunction V °
contains aI-rarefaction
wave,the constant
CL
in(3 . 39)
isgiven by
, , " 1 ,
If V contains a
3-rarefaction
wave, the constant CR in (J . 40) IS givenby
- , , , ,
3.
If
V" contains a 1-shock wave, thecoef f icients o~
theequataon
41 )are
explicitely given by
.... ,., "
and
4.
If -
V" contains a 3-shock wave, the coefficients oJ the equation 42)are
explicitely given by
, _ . " ~ - n n
VoL 6, n° 6-1989.
466
zs i a.aas va awmr i 1 ..._. ~ . ~. v ~.~a~ v v v s~ ~ ,-- ---
Let us now consider the gas
dynamics system
in Eulerian coordinates and inplane (v
=0), cylindrical (v =1)
orspherical (v
=2) symetry [4]:
~ -
i~ i - , .’ 1
~...-n
l~ 1~1v
variables have the
meaning
defined in Section 3. For the sake ofsimplicity,
we assume the
equation
of state(3 . 6).
Using
the nonconservative variables( p,
u,S),
thesystem (4 . I)
becomesI I , , v , , - ,
/ rB
v c~t ~ -
U
. _. ~ n . /~t~
~ ,
n _ n _ n ~ _
~ ~-~ ~ ’ ~~ - /
A state
V°=
t / M° B t being fixed,
the characteristic coordinates(K,)i§.~3
of any
arbitrary
state V=t M !,
L e.3
Vol. 6, n 6-1989.
468 A. BOURGEADE, PH. LE FLOCH AND P. A. RAVIART
»
V J
1 t_. ~T1 _. --. - /__ 1~T~11
approximation
,__ _,
~T~ lxl .. ~r,
(4. 1).
The notations are as shown inFigure
4. 1 and 4.2. In order toAnnales de l’Institut Henri Poincaré - Analyse non linéaire
determine the function Vl
(~),
we introduce as before itsdecomposi-
tion on the basis of
eigenvectors
~’ ", t~1 ~ c - -
w e begin oy deriving ine general form or tne functions 03B1j=03B1j(03BE) in an
interval where the function
V°
remains constant:LEMMA 4. 1. - In each interval
1 [,
i =0, 1, 2, 3,
there exist three real constants ai,=1, 2, 3,
such thatcorresponding
to aI-rarefaction
wave ofV°.
LEMMA 4.2. - Assume that
V°
contains aI-rarefaction
wave. Thenthere exist two real constants
b 1, 2
andb 1, 3
such thatfor all ~ cr°[ :
/YB
where c" = c" (~) is the sound
speed
in a1-raref action
zone. Thefunctions M°
=M° (c°)
andNL
=NL (c°)
aredefined by
" .,& i 1
and
,It
- - , ,..
/
U~ P~
° ’and
u° 1 ~
c(p, S) dp
areconstant
andu° - c° = E.
d
/
1C° r, = r, l V°1
+ 3
un tne oiner nana, we aeauce me uenvauves oi irum ~~ anu
4.13)
t’lnally,
usmg(4 . 14) . (4 . 15),
theordinary
dmerentialequations (2. 1 ~)
becomesThe integration of (4. 16 d) is stralightforward and gives (4 . tu b). t nen,
replacing
a2by
itsexpression (4.10 b)
in(4. 16 c),
we obtain an O.D.E.for the function whose solution is
given by (4 . 10 c). Finally (4.10 a)
follows from the
algebraic equation (4. 16 a)..
Then,
we treatsimilarly
the case of an interval63[ _ ]u2
+c2, uR
+cR[ corresponding
to a3-rarefaction
wave ofV°.
LEMMA 4. 2 bis. - Assume that
V °
contains a3-rarefaction
wave.Then,
there exist two real constants
b3,
I andb3, 2
such thatfor all ~
E]a3,
wehave
~
Vol. 6, n° 6-1989.
472 ..0lW __ m__ ______~ ____~ ___ _ ~ ____r__~____ _____ ~- .
M°
=M° (c°)
isdefined by (4 . 11), and the function NR = NR (c°)
isgiven by
discontinuities of
V°.
We consider firstrarefaction
waves. As a directconsequence of Lemmas 2. 4 and
4. 2,
we obtain:LEMMA 4 . 3. - Assume that
V °
contains a1-rarefaction
wave, Then theconstants
b 1, 2
andb 1, 3 of Lemma
4 . 2satisfy
b, ~ _ - a~ ~ . (c°) - Zo’‘ - l ~(4 . 19)
+
N ~"o - ~o - n~ - r" ~,.o - ,~o _
and
b3, 2 of
Lemma 4. 2 bissatisfy
b ~ ~
= a ~ ~(e~°) -
2~cY -1~, (4 . 22)
.
already
studied in theprevious
Section 3(see
Lemma3. 7).
It remains toconsider the contact
discontinuity corresponding to §
=u* (u°
= As inAnnales de l’Institut Henri Poincaré - Analyse non linéaire
ASYMPTOTIC EXPANSION
Section
3,
we define the functionpl by
/ a~.Bo /
auu ~c ~
LEMMA 4. 4. - The
function ul
andpl
are continuous at thepoint
~=u°.
Again,
define the coefficients and aR, J, 1_ j _ 3, by
r’ _ __ lzT01 ~"’ .. _.
Lemma 4 .1 f or i = 0 and i = 3:
: I ~ ~ ~ i . ~ Y
1BGlll.~,(I l4. - V ‘T . V J GillB.1. ‘’T , 1.11V 1 VliV ’11’’11’
llis VAY11V11-
formulae for the constants
ao, i
11 / i __ ~ v
dnu
For
obtaining
the function it remains to determine the constants of Lemma 4 . 1 for i =1 and i = 2. Thanks to Lemma4. 4,
we can seti i __~ ~__n~ i 1 _1 ~__ov /~ ~~B
and
p;.
THEOREM 4. 1. - 1.
If
thefunction V°
contains aI-rarefaction
wave, wehave
__1 _t 1 L
/oL b, n
474 __.
_r,.,..__~-__~_., _ __. _.a, _ _...__ ~__.y _.._. _~_.~s___
* * / _. . ~ ... In n , ~Tn. ..
7 ~ i ~ J ~ a ~r y~i L ~ V r
( 4 . 1 ~)
and(4 . 20) (resp. (4 . 11 )
and(4 . 12)).
2.
If
thefunction V °
contains a3-rarefaction
wave, we have-
u* ~ p*
- R /-o,3 - y>12 y - 1>(4 . 22) . (4. 23) (resp. (4 . 11 )
and(4 . 18)).
3.
If
thefunction V °
contains a I -shock wave, we have.. n ~ / n n , ~n ~ ~ 1
- a1°-uO
1 ~.-.n
1 ~T~O /20140 . 0B 1
/
~ .2~0 B ) I
/20140 0B ~1 1t
J J /
r -, _o ~_o __o~ ~.o ~ _ 1 .
~ -~~3-u~~
1 . ’t~0_/20140 ..0B..l
/
1...2~0 B ) I
/20140 . 0B ~1 i Btion wave
(the
derivation is similar in the case of a 3-rarefactionwave).
Annales de l’Institut Henri Poincaré - Analyse non tineaire
ana usmg d~ ana we nave aiso
/ 1 m., ~ v .
ihus, we o btain
rience, io n suinces [0 aetermme now me constant al, 3.
Thanks to
(4 . 21),
the function (Xg is continuousat ~ = u~ - c°. Therefore,
using (4. 9)
and(4.10),
we have~
wmcn yieias ai, 3.
Next,
we consider the case of a 3-shock wave(again
the derivation is similar in the case of a 1-shockwave).
Lemma 3. 7gives
thefollowing
relation between
ul
+0), pl
+0)
andpl
+o):
/1’
~~ B~~ p,11r l~Brl 1111.i1.i V ~ ‘J . JG~ . ‘J . J J J .
We
begin by computing
theright
hand side of(4. 35). Using (4. 7)
and(4. 9),
weget
"1 ~~o ~ n~ - ~a / - N ~o ~ ~ ~ ~ ii
Then because 01 ana (4. /), we nave
r .i
voi. o, n
476 .
r
and
Now,
wecompute
the left hand side of(4. 35). Again using (4. 7)
and(4. 9),
we obtain~ ~ __n .,. n f _ ~ _n ~ . _ _ ~ _n B~
... ~~ i ~, J
u*
andp*.
We may writeby
Lemma 4. 1:W _ -1~~1Z ln_ _ ..~n_ _1
Annales de l’Institut Henri Poincare - Analyse non lineare
477
that is
me values 01 u - ana p - are:
rnnally, noting that ~4J
We are now able to determine the whole of constants
THEOREM 4 . 2. - For i =1 and
2,
theconstants ai, 1 and ai, 3
aregiven
~y:
When
V °
contains ak-rarefaction
wave, we have;I
s.l. 6. n‘ ;-19$9.
478 A. BOURGEADE, PH. LE FLOCH AND P. A. RAVIART
-- ~ - --
.______ ___~ ____________~ _J ____ J__________ - - _ , , ,
Proof -
Formulae(4. 38)
and(4. 39)
werepreviously
demonstrated in theproof
of Theorem 4. 1. To prove(4. 40) [it
is similar for(4. 41)],
wehave
by (4. 9)
r,i_ l -~~l- -h~.~»~l n_ _ v, ‘ ~ . i v~
~*~~HL*~~/ B’* ~2014~/ B ~ -~2014201420142014~ 201420142014201420142014 2014- 20142014
constant
~i,
2~. ~ n~- ?/~2014 ~~ f nB- ~/~2014 i~
t PL jPL (
‘’T . ’TV~.
in zne case wnere v ~ nas a snocK wave, say a ..1-wave,
gives
a relation betweenpl
+0)
andpl
+0):
_
pi ± 0)
andget:
B~
and
u sing ~ 4 . i ) . ~ 4 . y), we als o determine l r,i . s. r,r _ ~ r.. 1 l rr ~ - (11
i l 1
Finally,
as a trivial consequence of Theorems 4.1 and4.2,
weget:
COROLLARY. - T7~ value
of the function p~
at~=M~
aregiven by
n i
Vol. 6, n° 6-1989.