c
c
c =========================================================
subroutine rp1eum(maxmx,meqn,mwaves,mbc,mx,ql,qr,maux,
& auxl,auxr,wave,s,amdq,apdq)
c =========================================================
c
c # solve Riemann problems for the 1D two-component
c # Euler equations using Roe's approximate Riemann solver.
c
c # Keh-Ming Shyue "An efficient shock-capturing algorithm for
c # compressible multicomponent problems", J. Comput. Phys., Vol. 142,
c # pp 208-242, 1998
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 # On output, wave contains the waves,
c # s the speeds,
c # amdq the left-going flux difference A^- \Delta q
c # apdq the right-going flux difference A^+ \Delta q
c
c # Note that the i'th Riemann problem has left state qr(i-1,:)
c # and right state ql(i,:)
c # From the basic routine step1, rp is called with ql = qr = q.
c
c # Copyright (C) 2002 Ralf Deiterding
c # Brandenburgische Universitaet Cottbus
c
c # Copyright (C) 2003-2007 California Institute of Technology
c # Ralf Deiterding, ralf@amroc.net
c
implicit double precision (a-h,o-z)
dimension ql(1-mbc:maxmx+mbc, meqn)
dimension qr(1-mbc:maxmx+mbc, meqn)
dimension s(1-mbc:maxmx+mbc, mwaves)
dimension wave(1-mbc:maxmx+mbc, meqn, mwaves)
dimension amdq(1-mbc:maxmx+mbc, meqn)
dimension apdq(1-mbc:maxmx+mbc, meqn)
c
c # local storage
c ---------------
parameter (max2 = 100002) !# assumes at most 100000 grid points with mbc=2
dimension delta(5)
dimension u(-1:max2),enth(-1:max2),a(-1:max2),
& g1a2(-1:max2),euv(-1:max2),p(-1:max2)
logical efix
c
data efix /.true./ !# use entropy fix for transonic rarefactions
c
c # Riemann solver returns flux differences
c ------------
common /rpnflx/ mrpnflx
mrpnflx = 0
c
c # Compute Roe-averaged quantities:
c
do 10 i = 2-mbc, mx+mbc
rhsqrtl = dsqrt(qr(i-1,1))
rhsqrtr = dsqrt(ql(i,1))
pl = (qr(i-1,3) - 0.5d0*(qr(i-1,2)**2)/qr(i-1,1)
& - qr(i-1,5) ) / qr(i-1,4)
pr = (ql(i,3) - 0.5d0*(ql(i,2)**2)/ql(i,1)
& - ql(i,5) ) / ql(i,4)
rhsq2 = rhsqrtl + rhsqrtr
gamma1 = rhsq2 / ( qr(i-1,4)*rhsqrtl + ql(i,4)*rhsqrtr )
xjota = ( pl*qr(i-1,4)*rhsqrtl + pr*ql(i,4)*rhsqrtr ) / rhsq2
p(i) = xjota*gamma1
u(i) = (qr(i-1,2)/rhsqrtl + ql(i,2)/rhsqrtr) / rhsq2
enth(i) = (((qr(i-1,3)+pl)/rhsqrtl
& + (ql(i,3)+pr)/rhsqrtr)) / rhsq2
a2 = gamma1*(enth(i) - .5d0*u(i)**2)
a(i) = dsqrt(a2)
g1a2(i) = gamma1 / a2
euv(i) = enth(i) - u(i)**2
10 continue
c
c
c # now split the jump in q at each interface into waves
c
c # find a1 thru a5, the coefficients of the 5 eigenvectors:
do 20 i = 2-mbc, mx+mbc
do n = 1, 5
delta(n) = ql(i,n) - qr(i-1,n)
enddo
a2 = g1a2(i) * (euv(i)*delta(1) + u(i)*delta(2) - delta(3)
& + p(i)*delta(4) + delta(5))
a3 = (delta(2) + (a(i)-u(i))*delta(1) - a(i)*a2) / (2.d0*a(i))
a1 = delta(1) - a2 - a3
a4 = delta(4)
a5 = delta(5)
c
c # Compute the waves.
c # Note that the 2-wave as well as the 4-wave and 5-wave
c # travel at the same speed and are lumped together in wave(.,.,2).
c # The 3-wave is then stored in wave(.,.,3).
c
wave(i,1,1) = a1
wave(i,2,1) = a1*(u(i)-a(i))
wave(i,3,1) = a1*(enth(i) - u(i)*a(i))
wave(i,4,1) = 0.d0
wave(i,5,1) = 0.d0
s(i,1) = u(i)-a(i)
c
wave(i,1,2) = a2
wave(i,2,2) = a2*u(i)
wave(i,3,2) = a2*0.5d0*u(i)**2 + a4*p(i) + a5
wave(i,4,2) = a4
wave(i,5,2) = a5
s(i,2) = u(i)
c
wave(i,1,3) = a3
wave(i,2,3) = a3*(u(i)+a(i))
wave(i,3,3) = a3*(enth(i)+u(i)*a(i))
wave(i,4,3) = 0.d0
wave(i,5,3) = 0.d0
s(i,3) = u(i)+a(i)
20 continue
c
c
c # compute flux differences amdq and apdq.
c ---------------------------------------
c
if (efix) go to 110
c
c # no entropy fix
c ----------------
c
c # amdq = SUM s*wave over left-going waves
c # apdq = SUM s*wave over right-going waves
c
do 100 m=1,5
do 100 i=2-mbc, mx+mbc
amdq(i,m) = 0.d0
apdq(i,m) = 0.d0
do 90 mw=1,mwaves
if (s(i,mw) .lt. 0.d0) then
amdq(i,m) = amdq(i,m) + s(i,mw)*wave(i,m,mw)
else
apdq(i,m) = apdq(i,m) + s(i,mw)*wave(i,m,mw)
endif
90 continue
100 continue
go to 900
c
c-----------------------------------------------------
c
110 continue
c
c # With entropy fix
c ------------------
c
c # compute flux differences amdq and apdq.
c # First compute amdq as sum of s*wave for left going waves.
c # Incorporate entropy fix by adding a modified fraction of wave
c # if s should change sign.
c
do 200 i = 2-mbc, mx+mbc
c
c # check 1-wave:
c ---------------
c
rhoim1 = qr(i-1,1)
pim1 = (qr(i-1,3) - 0.5d0*(qr(i-1,2)**2)/qr(i-1,1)
& - qr(i-1,5) ) / qr(i-1,4)
gamma1 = 1.d0/qr(i-1,4)
gamma = gamma1 + 1.d0
pinf = qr(i-1,5)*gamma1/gamma
cim1 = dsqrt(gamma*(pim1+pinf)/rhoim1)
s0 = qr(i-1,2)/rhoim1 - cim1 !# u-c in left state (cell i-1)
c # check for fully supersonic case:
if (s0.ge.0.d0 .and. s(i,1).gt.0.d0) then
c # everything is right-going
do 60 m=1,5
amdq(i,m) = 0.d0
60 continue
go to 200
endif
c
rho1 = qr(i-1,1) + wave(i,1,1)
rhou1 = qr(i-1,2) + wave(i,2,1)
en1 = qr(i-1,3) + wave(i,3,1)
p1 = (en1-0.5d0*(rhou1**2)/rho1-qr(i-1,5))/qr(i-1,4)
c1 = dsqrt(gamma*(p1+pinf)/rho1)
s1 = rhou1/rho1 - c1 !# u-c to right of 1-wave
if (s0.lt.0.d0 .and. s1.gt.0.d0) then
c # transonic rarefaction in the 1-wave
sfract = s0 * (s1-s(i,1)) / (s1-s0)
else if (s(i,1) .lt. 0.d0) then
c # 1-wave is leftgoing
sfract = s(i,1)
else
c # 1-wave is rightgoing
sfract = 0.d0 !# this shouldn't happen since s0 < 0
endif
do 120 m=1,5
amdq(i,m) = sfract*wave(i,m,1)
120 continue
c
c # check 2-wave:
c ---------------
c
if (s(i,2) .ge. 0.d0) go to 200 !# 2- and 3- waves are rightgoing
do 140 m=1,5
amdq(i,m) = amdq(i,m) + s(i,2)*wave(i,m,2)
140 continue
c
c # check 3-wave:
c ---------------
c
rhoi = ql(i,1)
pi = (ql(i,3) - 0.5d0*(ql(i,2)**2)/ql(i,1)
& - ql(i,5) ) / ql(i,4)
gamma1 = 1.d0/ql(i,4)
gamma = gamma1 + 1.d0
pinf = ql(i,5)*gamma1/gamma
ci = dsqrt(gamma*(pi+pinf)/rhoi)
s3 = ql(i,2)/rhoi + ci !# u+c in right state (cell i)
c
rho2 = ql(i,1) - wave(i,1,3)
rhou2 = ql(i,2) - wave(i,2,3)
en2 = ql(i,3) - wave(i,3,3)
p2 = (en2-0.5d0*(rhou2**2)/rho2-ql(i,5))/ql(i,4)
c2 = dsqrt(gamma*(p2+pinf)/rho2)
s2 = rhou2/rho2 + c2 !# u+c to left of 3-wave
if (s2 .lt. 0.d0 .and. s3.gt.0.d0) then
c # transonic rarefaction in the 3-wave
sfract = s2 * (s3-s(i,3)) / (s3-s2)
else if (s(i,3) .lt. 0.d0) then
c # 3-wave is leftgoing
sfract = s(i,3)
else
c # 3-wave is rightgoing
go to 200
endif
c
do 160 m=1,5
amdq(i,m) = amdq(i,m) + sfract*wave(i,m,3)
160 continue
200 continue
c
c # compute the rightgoing flux differences:
c # df = SUM s*wave is the total flux difference and apdq = df - amdq
c
do 220 m=1,5
do 220 i = 2-mbc, mx+mbc
df = 0.d0
do 210 mw=1,mwaves
df = df + s(i,mw)*wave(i,m,mw)
210 continue
apdq(i,m) = df - amdq(i,m)
220 continue
c
900 continue
return
end