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SWIFT
SWIFTsim
Commits
63813f76
Commit
63813f76
authored
Aug 10, 2016
by
Matthieu Schaller
Browse files
Added 2D Sod shock test case
parent
3d3dbda5
Changes
7
Hide whitespace changes
Inline
Side-by-side
examples/SodShock_1D/makeIC.py
View file @
63813f76
...
...
@@ -18,10 +18,9 @@
##############################################################################
import
h5py
import
random
from
numpy
import
*
# Generates a swift IC file for the Sod Shock in a periodic box
# Generates a swift IC file for the
1D
Sod Shock in a periodic box
# Parameters
gamma
=
5.
/
3.
# Gas adiabatic index
...
...
@@ -64,6 +63,7 @@ for i in range(numPart_L):
u
[
i
]
=
P_L
/
(
rho_L
*
(
gamma
-
1.
))
h
[
i
]
=
1.2348
*
delta_L
m
[
i
]
=
boxSize
*
rho_L
/
(
2.
*
numPart_L
)
v
[
i
,
0
]
=
v_L
# Set the particles on the right
for
j
in
range
(
numPart_R
):
...
...
@@ -72,6 +72,7 @@ for j in range(numPart_R):
u
[
i
]
=
P_R
/
(
rho_R
*
(
gamma
-
1.
))
h
[
i
]
=
1.2348
*
delta_R
m
[
i
]
=
boxSize
*
rho_R
/
(
2.
*
numPart_R
)
v
[
i
,
0
]
=
v_R
# Shift particles
coords
[:,
0
]
-=
x_min
...
...
examples/SodShock_1D/plotSolution.py
View file @
63813f76
...
...
@@ -229,7 +229,7 @@ subplot(231)
plot
(
x
,
v
,
'.'
,
color
=
'r'
)
plot
(
x_s
,
v_s
,
'--'
,
color
=
'k'
,
alpha
=
0.8
,
lw
=
1.2
)
xlabel
(
"$x$"
,
labelpad
=
0
)
ylabel
(
"$v$"
,
labelpad
=
0
)
ylabel
(
"$v
_x
$"
,
labelpad
=
0
)
xlim
(
-
0.5
,
0.5
)
ylim
(
-
0.1
,
0.95
)
...
...
examples/SodShock_2D/getGlass.sh
0 → 100755
View file @
63813f76
#!/bin/bash
wget http://virgodb.cosma.dur.ac.uk/swift-webstorage/ICs/glassPlane_128.hdf5
wget http://virgodb.cosma.dur.ac.uk/swift-webstorage/ICs/glassPlane_48.hdf5
examples/SodShock_2D/makeIC.py
0 → 100644
View file @
63813f76
###############################################################################
# This file is part of SWIFT.
# Copyright (c) 2016 Matthieu Schaller (matthieu.schaller@durham.ac.uk)
#
# This program is free software: you can redistribute it and/or modify
# it under the terms of the GNU Lesser General Public License as published
# by the Free Software Foundation, either version 3 of the License, or
# (at your option) any later version.
#
# This program is distributed in the hope that it will be useful,
# but WITHOUT ANY WARRANTY; without even the implied warranty of
# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
# GNU General Public License for more details.
#
# You should have received a copy of the GNU Lesser General Public License
# along with this program. If not, see <http://www.gnu.org/licenses/>.
#
##############################################################################
import
h5py
from
numpy
import
*
# Generates a swift IC file for the 2D Sod Shock in a periodic box
# Parameters
gamma
=
5.
/
3.
# Gas adiabatic index
x_min
=
-
1.
x_max
=
1.
rho_L
=
1.
# Density left state
rho_R
=
0.140625
# Density right state
v_L
=
0.
# Velocity left state
v_R
=
0.
# Velocity right state
P_L
=
1.
# Pressure left state
P_R
=
0.1
# Pressure right state
fileName
=
"sodShock.hdf5"
#---------------------------------------------------
boxSize
=
(
x_max
-
x_min
)
glass_L
=
h5py
.
File
(
"glassPlane_128.hdf5"
,
"r"
)
glass_R
=
h5py
.
File
(
"glassPlane_48.hdf5"
,
"r"
)
pos_L
=
glass_L
[
"/PartType0/Coordinates"
][:,:]
*
0.5
pos_R
=
glass_R
[
"/PartType0/Coordinates"
][:,:]
*
0.5
h_L
=
glass_L
[
"/PartType0/SmoothingLength"
][:]
*
0.5
h_R
=
glass_R
[
"/PartType0/SmoothingLength"
][:]
*
0.5
# Merge things
aa
=
pos_L
-
array
([
0.5
,
0.
,
0.
])
pos_LL
=
append
(
pos_L
,
pos_L
+
array
([
0.5
,
0.
,
0.
]),
axis
=
0
)
pos_RR
=
append
(
pos_R
,
pos_R
+
array
([
0.5
,
0.
,
0.
]),
axis
=
0
)
pos
=
append
(
pos_LL
-
array
([
1.0
,
0.
,
0.
]),
pos_RR
,
axis
=
0
)
h_LL
=
append
(
h_L
,
h_L
)
h_RR
=
append
(
h_R
,
h_R
)
h
=
append
(
h_LL
,
h_RR
)
numPart_L
=
size
(
h_LL
)
numPart_R
=
size
(
h_RR
)
numPart
=
size
(
h
)
vol_L
=
0.5
vol_R
=
0.5
# Generate extra arrays
v
=
zeros
((
numPart
,
3
))
ids
=
linspace
(
1
,
numPart
,
numPart
)
m
=
zeros
(
numPart
)
u
=
zeros
(
numPart
)
for
i
in
range
(
numPart
):
x
=
pos
[
i
,
0
]
if
x
<
0
:
#left
u
[
i
]
=
P_L
/
(
rho_L
*
(
gamma
-
1.
))
m
[
i
]
=
rho_L
*
vol_L
/
numPart_L
v
[
i
,
0
]
=
v_L
else
:
#right
u
[
i
]
=
P_R
/
(
rho_R
*
(
gamma
-
1.
))
m
[
i
]
=
rho_R
*
vol_R
/
numPart_R
v
[
i
,
0
]
=
v_R
# Shift particles
pos
[:,
0
]
-=
x_min
#File
file
=
h5py
.
File
(
fileName
,
'w'
)
# Header
grp
=
file
.
create_group
(
"/Header"
)
grp
.
attrs
[
"BoxSize"
]
=
[
boxSize
,
0.5
,
0.1
]
grp
.
attrs
[
"NumPart_Total"
]
=
[
numPart
,
0
,
0
,
0
,
0
,
0
]
grp
.
attrs
[
"NumPart_Total_HighWord"
]
=
[
0
,
0
,
0
,
0
,
0
,
0
]
grp
.
attrs
[
"NumPart_ThisFile"
]
=
[
numPart
,
0
,
0
,
0
,
0
,
0
]
grp
.
attrs
[
"Time"
]
=
0.0
grp
.
attrs
[
"NumFilesPerSnapshot"
]
=
1
grp
.
attrs
[
"MassTable"
]
=
[
0.0
,
0.0
,
0.0
,
0.0
,
0.0
,
0.0
]
grp
.
attrs
[
"Flag_Entropy_ICs"
]
=
0
#Runtime parameters
grp
=
file
.
create_group
(
"/RuntimePars"
)
grp
.
attrs
[
"PeriodicBoundariesOn"
]
=
1
#Units
grp
=
file
.
create_group
(
"/Units"
)
grp
.
attrs
[
"Unit length in cgs (U_L)"
]
=
1.
grp
.
attrs
[
"Unit mass in cgs (U_M)"
]
=
1.
grp
.
attrs
[
"Unit time in cgs (U_t)"
]
=
1.
grp
.
attrs
[
"Unit current in cgs (U_I)"
]
=
1.
grp
.
attrs
[
"Unit temperature in cgs (U_T)"
]
=
1.
#Particle group
grp
=
file
.
create_group
(
"/PartType0"
)
grp
.
create_dataset
(
'Coordinates'
,
data
=
pos
,
dtype
=
'd'
)
grp
.
create_dataset
(
'Velocities'
,
data
=
v
,
dtype
=
'f'
)
grp
.
create_dataset
(
'Masses'
,
data
=
m
,
dtype
=
'f'
)
grp
.
create_dataset
(
'SmoothingLength'
,
data
=
h
,
dtype
=
'f'
)
grp
.
create_dataset
(
'InternalEnergy'
,
data
=
u
,
dtype
=
'f'
)
grp
.
create_dataset
(
'ParticleIDs'
,
data
=
ids
,
dtype
=
'L'
)
file
.
close
()
examples/SodShock_2D/plotSolution.py
0 → 100644
View file @
63813f76
###############################################################################
# This file is part of SWIFT.
# Copyright (c) 2016 Matthieu Schaller (matthieu.schaller@durham.ac.uk)
#
# This program is free software: you can redistribute it and/or modify
# it under the terms of the GNU Lesser General Public License as published
# by the Free Software Foundation, either version 3 of the License, or
# (at your option) any later version.
#
# This program is distributed in the hope that it will be useful,
# but WITHOUT ANY WARRANTY; without even the implied warranty of
# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
# GNU General Public License for more details.
#
# You should have received a copy of the GNU Lesser General Public License
# along with this program. If not, see <http://www.gnu.org/licenses/>.
#
##############################################################################
# Computes the analytical solution of the Sod shock and plots the SPH answer
# Generates the analytical solution for the Sod shock test case
# The script works for a given left (x<0) and right (x>0) state and computes the solution at a later time t.
# The code writes five files rho.dat, P.dat, v.dat, u.dat and s.dat with the density, pressure, internal energy and
# entropic function on N points between x_min and x_max.
# This follows the solution given in (Toro, 2009)
# Parameters
gas_gamma
=
5.
/
3.
# Polytropic index
rho_L
=
1.
# Density left state
rho_R
=
0.140625
# Density right state
v_L
=
0.
# Velocity left state
v_R
=
0.
# Velocity right state
P_L
=
1.
# Pressure left state
P_R
=
0.1
# Pressure right state
import
matplotlib
matplotlib
.
use
(
"Agg"
)
from
pylab
import
*
import
h5py
# Plot parameters
params
=
{
'axes.labelsize'
:
10
,
'axes.titlesize'
:
10
,
'font.size'
:
12
,
'legend.fontsize'
:
12
,
'xtick.labelsize'
:
10
,
'ytick.labelsize'
:
10
,
'text.usetex'
:
True
,
'figure.figsize'
:
(
9.90
,
6.45
),
'figure.subplot.left'
:
0.045
,
'figure.subplot.right'
:
0.99
,
'figure.subplot.bottom'
:
0.05
,
'figure.subplot.top'
:
0.99
,
'figure.subplot.wspace'
:
0.15
,
'figure.subplot.hspace'
:
0.12
,
'lines.markersize'
:
6
,
'lines.linewidth'
:
3.
,
'text.latex.unicode'
:
True
}
rcParams
.
update
(
params
)
rc
(
'font'
,
**
{
'family'
:
'sans-serif'
,
'sans-serif'
:[
'Times'
]})
snap
=
int
(
sys
.
argv
[
1
])
# Read the simulation data
sim
=
h5py
.
File
(
"sodShock_%03d.hdf5"
%
snap
,
"r"
)
boxSize
=
sim
[
"/Header"
].
attrs
[
"BoxSize"
][
0
]
time
=
sim
[
"/Header"
].
attrs
[
"Time"
][
0
]
scheme
=
sim
[
"/HydroScheme"
].
attrs
[
"Scheme"
]
kernel
=
sim
[
"/HydroScheme"
].
attrs
[
"Kernel function"
]
neighbours
=
sim
[
"/HydroScheme"
].
attrs
[
"Kernel target N_ngb"
]
eta
=
sim
[
"/HydroScheme"
].
attrs
[
"Kernel eta"
]
x
=
sim
[
"/PartType0/Coordinates"
][:,
0
]
v
=
sim
[
"/PartType0/Velocities"
][:,
0
]
u
=
sim
[
"/PartType0/InternalEnergy"
][:]
S
=
sim
[
"/PartType0/Entropy"
][:]
P
=
sim
[
"/PartType0/Pressure"
][:]
rho
=
sim
[
"/PartType0/Density"
][:]
N
=
1000
# Number of points
x_min
=
-
1.
x_max
=
1.
x
+=
x_min
# ---------------------------------------------------------------
# Don't touch anything after this.
# ---------------------------------------------------------------
c_L
=
sqrt
(
gas_gamma
*
P_L
/
rho_L
)
# Speed of the rarefaction wave
c_R
=
sqrt
(
gas_gamma
*
P_R
/
rho_R
)
# Speed of the shock front
# Helpful variable
Gama
=
(
gas_gamma
-
1.
)
/
(
gas_gamma
+
1.
)
beta
=
(
gas_gamma
-
1.
)
/
(
2.
*
gas_gamma
)
# Characteristic function and its derivative, following Toro (2009)
def
compute_f
(
P_3
,
P
,
c
):
u
=
P_3
/
P
if
u
>
1
:
term1
=
gas_gamma
*
((
gas_gamma
+
1.
)
*
u
+
gas_gamma
-
1.
)
term2
=
sqrt
(
2.
/
term1
)
fp
=
(
u
-
1.
)
*
c
*
term2
dfdp
=
c
*
term2
/
P
+
(
u
-
1.
)
*
c
/
term2
*
(
-
1.
/
term1
**
2
)
*
gas_gamma
*
(
gas_gamma
+
1.
)
/
P
else
:
fp
=
(
u
**
beta
-
1.
)
*
(
2.
*
c
/
(
gas_gamma
-
1.
))
dfdp
=
2.
*
c
/
(
gas_gamma
-
1.
)
*
beta
*
u
**
(
beta
-
1.
)
/
P
return
(
fp
,
dfdp
)
# Solution of the Riemann problem following Toro (2009)
def
RiemannProblem
(
rho_L
,
P_L
,
v_L
,
rho_R
,
P_R
,
v_R
):
P_new
=
((
c_L
+
c_R
+
(
v_L
-
v_R
)
*
0.5
*
(
gas_gamma
-
1.
))
/
(
c_L
/
P_L
**
beta
+
c_R
/
P_R
**
beta
))
**
(
1.
/
beta
)
P_3
=
0.5
*
(
P_R
+
P_L
)
f_L
=
1.
while
fabs
(
P_3
-
P_new
)
>
1e-6
:
P_3
=
P_new
(
f_L
,
dfdp_L
)
=
compute_f
(
P_3
,
P_L
,
c_L
)
(
f_R
,
dfdp_R
)
=
compute_f
(
P_3
,
P_R
,
c_R
)
f
=
f_L
+
f_R
+
(
v_R
-
v_L
)
df
=
dfdp_L
+
dfdp_R
dp
=
-
f
/
df
prnew
=
P_3
+
dp
v_3
=
v_L
-
f_L
return
(
P_new
,
v_3
)
# Solve Riemann problem for post-shock region
(
P_3
,
v_3
)
=
RiemannProblem
(
rho_L
,
P_L
,
v_L
,
rho_R
,
P_R
,
v_R
)
# Check direction of shocks and wave
shock_R
=
(
P_3
>
P_R
)
shock_L
=
(
P_3
>
P_L
)
# Velocity of shock front and and rarefaction wave
if
shock_R
:
v_right
=
v_R
+
c_R
**
2
*
(
P_3
/
P_R
-
1.
)
/
(
gas_gamma
*
(
v_3
-
v_R
))
else
:
v_right
=
c_R
+
0.5
*
(
gas_gamma
+
1.
)
*
v_3
-
0.5
*
(
gas_gamma
-
1.
)
*
v_R
if
shock_L
:
v_left
=
v_L
+
c_L
**
2
*
(
P_3
/
p_L
-
1.
)
/
(
gas_gamma
*
(
v_3
-
v_L
))
else
:
v_left
=
c_L
-
0.5
*
(
gas_gamma
+
1.
)
*
v_3
+
0.5
*
(
gas_gamma
-
1.
)
*
v_L
# Compute position of the transitions
x_23
=
-
fabs
(
v_left
)
*
time
if
shock_L
:
x_12
=
-
fabs
(
v_left
)
*
time
else
:
x_12
=
-
(
c_L
-
v_L
)
*
time
x_34
=
v_3
*
time
x_45
=
fabs
(
v_right
)
*
time
if
shock_R
:
x_56
=
fabs
(
v_right
)
*
time
else
:
x_56
=
(
c_R
+
v_R
)
*
time
# Prepare arrays
delta_x
=
(
x_max
-
x_min
)
/
N
x_s
=
arange
(
x_min
,
x_max
,
delta_x
)
rho_s
=
zeros
(
N
)
P_s
=
zeros
(
N
)
v_s
=
zeros
(
N
)
# Compute solution in the different regions
for
i
in
range
(
N
):
if
x_s
[
i
]
<=
x_12
:
rho_s
[
i
]
=
rho_L
P_s
[
i
]
=
P_L
v_s
[
i
]
=
v_L
if
x_s
[
i
]
>=
x_12
and
x_s
[
i
]
<
x_23
:
if
shock_L
:
rho_s
[
i
]
=
rho_L
*
(
Gama
+
P_3
/
P_L
)
/
(
1.
+
Gama
*
P_3
/
P_L
)
P_s
[
i
]
=
P_3
v_s
[
i
]
=
v_3
else
:
rho_s
[
i
]
=
rho_L
*
(
Gama
*
(
0.
-
x_s
[
i
])
/
(
c_L
*
time
)
+
Gama
*
v_L
/
c_L
+
(
1.
-
Gama
))
**
(
2.
/
(
gas_gamma
-
1.
))
P_s
[
i
]
=
P_L
*
(
rho_s
[
i
]
/
rho_L
)
**
gas_gamma
v_s
[
i
]
=
(
1.
-
Gama
)
*
(
c_L
-
(
0.
-
x_s
[
i
])
/
time
)
+
Gama
*
v_L
if
x_s
[
i
]
>=
x_23
and
x_s
[
i
]
<
x_34
:
if
shock_L
:
rho_s
[
i
]
=
rho_L
*
(
Gama
+
P_3
/
P_L
)
/
(
1
+
Gama
*
P_3
/
p_L
)
else
:
rho_s
[
i
]
=
rho_L
*
(
P_3
/
P_L
)
**
(
1.
/
gas_gamma
)
P_s
[
i
]
=
P_3
v_s
[
i
]
=
v_3
if
x_s
[
i
]
>=
x_34
and
x_s
[
i
]
<
x_45
:
if
shock_R
:
rho_s
[
i
]
=
rho_R
*
(
Gama
+
P_3
/
P_R
)
/
(
1.
+
Gama
*
P_3
/
P_R
)
else
:
rho_s
[
i
]
=
rho_R
*
(
P_3
/
P_R
)
**
(
1.
/
gas_gamma
)
P_s
[
i
]
=
P_3
v_s
[
i
]
=
v_3
if
x_s
[
i
]
>=
x_45
and
x_s
[
i
]
<
x_56
:
if
shock_R
:
rho_s
[
i
]
=
rho_R
P_s
[
i
]
=
P_R
v_s
[
i
]
=
v_R
else
:
rho_s
[
i
]
=
rho_R
*
(
Gama
*
(
x_s
[
i
])
/
(
c_R
*
time
)
-
Gama
*
v_R
/
c_R
+
(
1.
-
Gama
))
**
(
2.
/
(
gas_gamma
-
1.
))
P_s
[
i
]
=
p_R
*
(
rho_s
[
i
]
/
rho_R
)
**
gas_gamma
v_s
[
i
]
=
(
1.
-
Gama
)
*
(
-
c_R
-
(
-
x_s
[
i
])
/
time
)
+
Gama
*
v_R
if
x_s
[
i
]
>=
x_56
:
rho_s
[
i
]
=
rho_R
P_s
[
i
]
=
P_R
v_s
[
i
]
=
v_R
# Additional arrays
u_s
=
P_s
/
(
rho_s
*
(
gas_gamma
-
1.
))
#internal energy
s_s
=
P_s
/
rho_s
**
gas_gamma
# entropic function
# Plot the interesting quantities
figure
()
# Velocity profile --------------------------------
subplot
(
231
)
plot
(
x
,
v
,
'.'
,
color
=
'r'
)
plot
(
x_s
,
v_s
,
'--'
,
color
=
'k'
,
alpha
=
0.8
,
lw
=
1.2
)
xlabel
(
"$x$"
,
labelpad
=
0
)
ylabel
(
"$v_x$"
,
labelpad
=
0
)
xlim
(
-
0.5
,
0.5
)
ylim
(
-
0.1
,
0.95
)
# Density profile --------------------------------
subplot
(
232
)
plot
(
x
,
rho
,
'.'
,
color
=
'r'
)
plot
(
x_s
,
rho_s
,
'--'
,
color
=
'k'
,
alpha
=
0.8
,
lw
=
1.2
)
xlabel
(
"$x$"
,
labelpad
=
0
)
ylabel
(
"$
\\
rho$"
,
labelpad
=
0
)
xlim
(
-
0.5
,
0.5
)
ylim
(
0.05
,
1.1
)
# Pressure profile --------------------------------
subplot
(
233
)
plot
(
x
,
P
,
'.'
,
color
=
'r'
)
plot
(
x_s
,
P_s
,
'--'
,
color
=
'k'
,
alpha
=
0.8
,
lw
=
1.2
)
xlabel
(
"$x$"
,
labelpad
=
0
)
ylabel
(
"$P$"
,
labelpad
=
0
)
xlim
(
-
0.5
,
0.5
)
ylim
(
0.01
,
1.1
)
# Internal energy profile -------------------------
subplot
(
234
)
plot
(
x
,
u
,
'.'
,
color
=
'r'
)
plot
(
x_s
,
u_s
,
'--'
,
color
=
'k'
,
alpha
=
0.8
,
lw
=
1.2
)
xlabel
(
"$x$"
,
labelpad
=
0
)
ylabel
(
"$u$"
,
labelpad
=
0
)
xlim
(
-
0.5
,
0.5
)
ylim
(
0.8
,
2.2
)
# Entropy profile ---------------------------------
subplot
(
235
)
plot
(
x
,
S
,
'.'
,
color
=
'r'
)
plot
(
x_s
,
s_s
,
'--'
,
color
=
'k'
,
alpha
=
0.8
,
lw
=
1.2
)
xlabel
(
"$x$"
,
labelpad
=
0
)
ylabel
(
"$S$"
,
labelpad
=
0
)
xlim
(
-
0.5
,
0.5
)
ylim
(
0.8
,
3.8
)
# Information -------------------------------------
subplot
(
236
,
frameon
=
False
)
text
(
-
0.49
,
0.9
,
"Sod shock with $
\\
gamma=%.3f$ in 2D at $t=%.2f$"
%
(
gas_gamma
,
time
),
fontsize
=
10
)
text
(
-
0.49
,
0.8
,
"Left:~~ $(P_L,
\\
rho_L, v_L) = (%.3f, %.3f, %.3f)$"
%
(
P_L
,
rho_L
,
v_L
),
fontsize
=
10
)
text
(
-
0.49
,
0.7
,
"Right: $(P_R,
\\
rho_R, v_R) = (%.3f, %.3f, %.3f)$"
%
(
P_R
,
rho_R
,
v_R
),
fontsize
=
10
)
plot
([
-
0.49
,
0.1
],
[
0.62
,
0.62
],
'k-'
,
lw
=
1
)
text
(
-
0.49
,
0.5
,
scheme
,
fontsize
=
10
)
text
(
-
0.49
,
0.4
,
kernel
,
fontsize
=
10
)
text
(
-
0.49
,
0.3
,
"$%.2f$ neighbours ($
\\
eta=%.3f$)"
%
(
neighbours
,
eta
),
fontsize
=
10
)
xlim
(
-
0.5
,
0.5
)
ylim
(
0
,
1
)
xticks
([])
yticks
([])
savefig
(
"SodShock.png"
,
dpi
=
200
)
examples/SodShock_2D/run.sh
0 → 100755
View file @
63813f76
#!/bin/bash
# Generate the initial conditions if they are not present.
if
[
!
-e
glassPlane_128.hdf5
]
then
echo
"Fetching initial glass file for the Sod shock example..."
./getGlass.sh
fi
if
[
!
-e
sodShock.hdf5
]
then
echo
"Generating initial conditions for the Sod shock example..."
python makeIC.py
fi
# Run SWIFT
../swift
-s
-t
1 sodShock.yml
python plotSolution.py 1
examples/SodShock_2D/sodShock.yml
0 → 100644
View file @
63813f76
# Define the system of units to use internally.
InternalUnitSystem
:
UnitMass_in_cgs
:
1
# Grams
UnitLength_in_cgs
:
1
# Centimeters
UnitVelocity_in_cgs
:
1
# Centimeters per second
UnitCurrent_in_cgs
:
1
# Amperes
UnitTemp_in_cgs
:
1
# Kelvin
# Parameters governing the time integration
TimeIntegration
:
time_begin
:
0.
# The starting time of the simulation (in internal units).
time_end
:
0.2
# The end time of the simulation (in internal units).
dt_min
:
1e-7
# The minimal time-step size of the simulation (in internal units).
dt_max
:
1e-2
# The maximal time-step size of the simulation (in internal units).
# Parameters governing the snapshots
Snapshots
:
basename
:
sodShock
# Common part of the name of output files
time_first
:
0.
# Time of the first output (in internal units)
delta_time
:
0.2
# Time difference between consecutive outputs (in internal units)
# Parameters governing the conserved quantities statistics
Statistics
:
delta_time
:
1e-2
# Time between statistics output
# Parameters for the hydrodynamics scheme
SPH
:
resolution_eta
:
1.2348
# Target smoothing length in units of the mean inter-particle separation (1.2348 == 48Ngbs with the cubic spline kernel).
delta_neighbours
:
0.1
# The tolerance for the targetted number of neighbours.
max_smoothing_length
:
0.02
# Maximal smoothing length allowed (in internal units).
CFL_condition
:
0.1
# Courant-Friedrich-Levy condition for time integration.
# Parameters related to the initial conditions
InitialConditions
:
file_name
:
./sodShock.hdf5
# The file to read
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