c
c
c =====================================================
subroutine rpn3eu(ixyz,maxm,meqn,mwaves,mbc,mx,ql,qr,
& maux,auxl,auxr,wave,s,fl,fr)
c =====================================================
c
c # solve Riemann problems for the 3D ZND-Euler equations using
c # the Flux-Vector-Splitting of Vijayasundaram
c
c # On input, ql contains the state vector at the left edge of each cell
c # qr contains the state vector at the right edge of each cell
c # This data is along a slice in the x-direction if ixyz=1
c # the y-direction if ixyz=2.
c # the z-direction if ixyz=3.
c
c # On output, wave contains the waves, s the speeds,
c # fl and fr the positive and negative flux.
c
c # Note that the i'th Riemann problem has left state qr(i-1,:)
c # and right state ql(i,:)
c # From the routines, this routine is called with ql = qr
c
c # Copyright (C) 2002 Ralf Deiterding
c # Brandenburgische Universitaet Cottbus
c
implicit double precision (a-h,o-z)
dimension wave(1-mbc:maxm+mbc, meqn, mwaves)
dimension s(1-mbc:maxm+mbc, mwaves)
dimension ql(1-mbc:maxm+mbc, meqn)
dimension qr(1-mbc:maxm+mbc, meqn)
dimension fl(1-mbc:maxm+mbc, meqn)
dimension fr(1-mbc:maxm+mbc, meqn)
dimension auxl(1-mbc:maxm+mbc, maux, 3)
dimension auxr(1-mbc:maxm+mbc, maux, 3)
double precision el(3), er(3)
common /param/ gamma,gamma1
c
c # Method returns fluxes
c ------------
common /rpnflx/ mrpnflx
mrpnflx = 1
c
c # set mu to point to the component of the system that corresponds
c # to momentum in the direction of this slice, mv and mw to the
c # orthogonal momentum:
c
if(ixyz .eq. 1)then
mu = 2
mv = 3
mw = 4
else if(ixyz .eq. 2)then
mu = 3
mv = 4
mw = 2
else
mu = 4
mv = 2
mw = 3
endif
c
do 10 i=2-mbc,mx+mbc
rhol = qr(i-1,1)
rhor = ql(i ,1)
rhoul = qr(i-1,mu)
rhour = ql(i ,mu)
rhovl = qr(i-1,mv)
rhovr = ql(i ,mv)
rhowl = qr(i-1,mw)
rhowr = ql(i ,mw)
rhoEl = qr(i-1,5)
rhoEr = ql(i ,5)
c
rho = 0.5d0*(rhol + rhor )
rhou = 0.5d0*(rhoul + rhour)
rhov = 0.5d0*(rhovl + rhovr)
rhow = 0.5d0*(rhowl + rhowr)
rhoE = 0.5d0*(rhoEl + rhoEr)
c
u = rhou/rho
v = rhov/rho
w = rhow/rho
p = gamma1*(rhoE - 0.5d0*rho*(u**2+v**2+w**2))
H = (rhoE+p)/rho
if (p.le.0.d0.or.rho.le.0.d0)
& write (6,*) 'Error in middle state in',i,p,pl,pr,
& rho,rhol,rhor,a,al,ar
a = dsqrt(gamma*p/rho)
f = 0.5d0/a**2
c
el(1) = 0.5d0*(u-a + dabs(u-a))
el(2) = 0.5d0*(u + dabs(u) )
el(3) = 0.5d0*(u+a + dabs(u+a))
er(1) = 0.5d0*(u-a - dabs(u-a))
er(2) = 0.5d0*(u - dabs(u) )
er(3) = 0.5d0*(u+a - dabs(u+a))
c
zl = el(1)-el(3)
zr = er(1)-er(3)
ol = el(1)-2.d0*el(2)+el(3)
or = er(1)-2.d0*er(2)+er(3)
dul = a*(rhol*u-rhoul)
dur = a*(rhor*u-rhour)
dEl = gamma1*(rhoEl+0.5d0*rhol*(u**2+v**2+w**2)-
& rhoul*u-rhovl*v-rhowl*w)
dEr = gamma1*(rhoEr+0.5d0*rhor*(u**2+v**2+w**2)-
& rhour*u-rhovr*v-rhowr*w)
f1 = f*(zl*dul + ol*dEl + zr*dur + or*dEr)
f2 = a*f*(ol*dul + zl*dEl + or*dur + zr*dEr)
c
fl(i,1) = rhol *el(2) + rhor *er(2) + f1
fl(i,mu) = rhoul*el(2) + rhour*er(2) + u*f1 - f2
fl(i,mv) = rhovl*el(2) + rhovr*er(2) + v*f1
fl(i,mw) = rhowl*el(2) + rhowr*er(2) + w*f1
fl(i,5) = rhoEl*el(2) + rhoEr*er(2) + H*f1 - u*f2
c
do 20 m = 1,meqn
fr(i,m) = -fl(i,m)
20 continue
c
do 10 mws=1,mwaves
s(i,mws) = dmax1(dabs(el(mws)),dabs(er(mws)))
do 10 m=1,meqn
wave(i,m,mws) = 0.d0
10 continue
c
return
end
c