# Liu et al benchmark

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== Gerris parameter file 'liu.gfs' == | == Gerris parameter file 'liu.gfs' == | ||

+ | |||

+ | The time series of the position of the center of gravity of the solid during the experiment can be downloaded [http://isec.nacse.org/workshop/2004_cornell/data/Benchmark_4_run30.txt here]. | ||

The simulation can be run using: gerris3D -m liu.gfs | The simulation can be run using: gerris3D -m liu.gfs |

## Revision as of 23:55, 23 March 2011

This benchmark for simulations of landslide-generated tsunamis using Gerris is based on these articles:

*P. L.-F. Liu, T.R. Wu, F. Raichlen, C.E. Synolakis, J. C. Borrero* - **Runup and rundown generated by three-dimensional sliding masses**

- Journal of Fluid Mechanics 536:107-144, 2005
- Bibtex

*S. Abadie, D. Morichon, S. Grilli, S. Glockner* - **Numerical simulation of waves generated by landslides using a multiple-fluid Navier-Stokes model**

- Coastal Engineering 57:779-794, 2010
- Bibtex

We focus here on one of the configuration that was retained as one of the benchmark test of the third international workshop on long-wave runup models (run 30). We look at the wave created by the free fall of a half-rectangle slide along a uniform slope.

The design of this page is inspired from that dedicated to the Enet_et_al_benchmark.

## Contents |

## Generating the landslide body geometry

A GTS surface representation of the slide has to be generated to be fed to the moving boundary implementation GfsSolidMoving. This can be done using the following script:

# Generates the points of the triangulation

awk -f liu.awk > points.tmp

# Generates and rotates the triangulation

( wc points.tmp | awk '{print $1" 0 0"}'; cat points.tmp ) | delaunay -d | transform --rx=-90 > liu.gts

The awk script 'liu.awk' allows to generate the points of the triangulation. The notations a and b correspond to that of (Liu et al., 2005)

BEGIN {

a=0.4572

b=0.9144

alpha=atan2(a,b);

h=a*cos(alpha);

l1=b*cos(alpha);

l2=a*sin(alpha);

for (k=0; k <= 100; k++) {

for (i=-10; i <= 100; i++) { printf("%5.4f %5.4f %5.4f\n",l1*i/100, -0.5+k/100 , h*i/100) }

for (i=1; i <= 110; i++) { printf("%5.4f %5.4f %5.4f\n",l1+l2*i/100, -0.5+k/100, h*(1-i/100)) }

}

dx=1.0e-4

k=0.

j=-10.

for (i=-10; i <= 100; i++) { printf("%5.4f %5.4f %5.4f\n",l1*i/100, -0.5+k/100-dx,h*j/100) }

for (i=1; i <= 110; i++) { printf("%5.4f %5.4f %5.4f\n",l1+l2*i/100, -0.5+k/100-dx,h*j/100) }

k=100.

for (i=-10; i <= 100; i++) { printf("%5.4f %5.4f %5.4f\n",l1*i/100, -0.5+k/100+dx,h*j/100) }

for (i=1; i <= 110; i++) { printf("%5.4f %5.4f %5.4f\n",l1+l2*i/100, -0.5+k/100+dx,h*j/100) }

}

## Numerical "wave gauge"

[ The setup of the numerical gauges is identical to that of Enet_et_al_benchmark. Please see Enet_et_al_benchmark for more details. Only the location of the gauges and the angle of the slope angle have to be modified. Consequently the 'distance.awk' which is used to calculate the surface elevation becomes:

BEGIN {

tant = 0.4572/0.9144

norm = sqrt (1. + tant*tant)

FS=" |:"

}

{

if ($1 == "#") {

# get column indices of the relevant fields (X,Y)

for (i = 1; i <= NF; i++) {

if ($i == "T")

iT = $(i-1);

else if ($i == "X")

iX = $(i-1);

else if ($i == "Y")

iY = $(i-1);

}

}

else {

T = $iT

if (T > 0. && T < 1.) {

# the cell contains an interface

x = $iX

y = $iY

print $1,(y - tant*x)/norm;

fflush (stdout);

}

}

}

and the coordinates of the probe 'wires' can be generated using the awk script:

BEGIN {

angle = atan2(0.4572,0.9144)

for (y = -0.1; y <= 0.1; y+= 0.001) {

x = 1.83

print cos(angle)*x - sin(angle)*y, sin(angle)*x + cos(angle)*y, 0 > "probe1x"

x = 1.2446

print cos(angle)*x - sin(angle)*y, sin(angle)*x + cos(angle)*y, 0.635 > "probe2x"

x = 0

print cos(angle)*x - sin(angle)*y, sin(angle)*x + cos(angle)*y, 0 > "probe3x"

x = 0

print cos(angle)*x - sin(angle)*y, sin(angle)*x + cos(angle)*y, 0.305 > "probe4x"

x = 0

print cos(angle)*x - sin(angle)*y, sin(angle)*x + cos(angle)*y, 0.61 > "probe5x"

}

}

## 3D Results

So far, the full simulations I have managed to run give reasonable results. Those can be commented in the light of Stephane's previous comment on the Enet_et_al_benchmark. Wave gauge comparisons are possibly better for this test case, but we can observe the same trends in the results i.e. the over-prediction of the wave amplitude and the simulation is slightly late on the first trough. While this might not appear to be very satisfactory, this is as good as the results of (Abadie et al., 2010).

Wave generation is generally mainly governed by pressure forces and as a first approximation it was assumed that the fluids here are inviscid. In order to assess whether the validation on this benchmark test can be improved to more runs will be made: one with viscous fluids and a second one with a better resolution.

## 2D/3D Comparisons

Preliminary simulations were run in two-dimension. Great agreement is not expected but this is a useful step to go through to assess the behavior of the code and tune the simulation. Even though the scale are slightly different between the plots of the 3D and 2D simulation presented hereafter, it is possible to see that 2D and 3D simulations remains qualitatively more or less similar during the first half of the simulation. Then wave-breaking occurs with accompanies with a dampening of the wave height in the 3D case, which is not the case in the 2D simulation.

Globally the wave height in 2D are much larger than in 3D or in the laboratory experiments which is not a surprise as momentum cannot travel in the transverse direction. The strong wave-breaking found in 2D makes the wave height at the different gauges hard to assess, but the arrival time of the first wave seem to be predicted well enough while the wave amplitude from the start are two to three time large than what is found in reality.

## Gerris parameter file 'liu.gfs'

The time series of the position of the center of gravity of the solid during the experiment can be downloaded here.

The simulation can be run using: gerris3D -m liu.gfs

Define LEVEL 8

Define LMIN 4

Define RHO MAX(0.01, (0.01*T + (1. - T)))

Define ANGLE (atan2(0.4572,0.9144))

2 1 GfsSimulationMoving GfsBox GfsGEdge { y = 0.5 } {

# Sets the duration of the simulation to 3 time units

Time { end = 3 dtmax = 0.01}

# The CFL tolerance is set to 0.4

AdvectionParams { cfl = 0.4 }

Global { double interface (double x, double y) {

return ((y) - 0.4572/0.9144*x);

}

}

# Initial refinement

Refine LMIN

RefineSurface LEVEL (interface(x,y))

# Physical length of a box

PhysicalParams { L = 5. }

# Tank bottom

Solid ((y) - 0.4572/0.9144*(x- 1.0223302793129*2.44/0.4572))

# Fluid

VariableTracerVOF T

InitFraction T (interface (x,y))

# We lower the tolerance on the Poisson solver

ApproxProjectionParams { tolerance = 1e-5 }

ProjectionParams { tolerance = 1e-5 }

# Definition of functions that read the file containing the time evolution of the position

# of the solid object and derive the corresponding boundary conditions.

Global {

double position (double t) {

FILE * fin = fopen ("Benchmark_4_run30.txt","r");

double t0=0, p0=0, t1=0, p1=0;

g_assert(fscanf(fin,"%lf %lf\n",&t1,&p1));

while (t1 <= t) {

t0=t1; p0=p1;

g_assert(fscanf(fin,"%lf %lf\n",&t1,&p1));

}

fclose (fin);

if (t1 == t) {

return p1/100;

}

else {

return (p0*(t1-t)+p1*(t-t0))/(100*(t1-t0));

}

}

double instant_vel (double t) {

FILE * fin = fopen ("Benchmark_4_run30.txt","r");

double t0=0, p0=0, t1=0, p1=0;

g_assert(fscanf(fin,"%lf %lf\n",&t1,&p1));

while (t1 <= t) {

t0=t1; p0=p1;

g_assert(fscanf(fin,"%lf %lf\n",&t1,&p1));

}

fclose (fin);

return (p1-p0)/(t1-t0);

}

double vel_x (double t, double dt) {

if (dt == 0.)

return (instant_vel (t));

else

return ((position(t+dt)-position(t))/dt);

}

}

# Setup of the moving slide

SolidMoving liu.gts {

tx = 0.14142135623731

ty = 1e-6

sz = 0.6525

flip = 1

} { level = LEVEL }

#

SurfaceBc U Dirichlet (vel_x (t, dt))

# Setup of mesh refinement on the solid boundaries

RefineSolid ( x < 1.5 ? LEVEL : LMIN)

# Density

PhysicalParams { alpha = 1./RHO }

# Use the reduced gravity approach

VariablePosition Y T y

VariablePosition X T x

SourceTension T -9.81*cos(ANGLE)*(0.01 - 1.) Y

SourceTension T 9.81*sin(ANGLE)*(0.01 - 1.) X

AdaptFunction { istart = 1 istep = 1 } {

cmax = 0

maxlevel = (x < 4. ? LEVEL : LEVEL - 2)

minlevel = (T < 1. ? LMIN:0)

} (T > 0 && T < 1)

AdaptVorticity { istep = 1 } {

cmax = 1.0

maxlevel = LEVEL

minlevel = LMIN

}

# Wave gauges

OutputLocation { istep = 1 } { awk -f distance.awk > probe1 } probe1x { interpolate = 0 }

OutputLocation { istep = 1 } { awk -f distance.awk > probe2 } probe2x { interpolate = 0 }

OutputLocation { istep = 1 } { awk -f distance.awk > probe3 } probe3x { interpolate = 0 }

OutputLocation { istep = 1 } { awk -f distance.awk > probe4 } probe4x { interpolate = 0 }

OutputLocation { istep = 1 } { awk -f distance.awk > probe4 } probe5x { interpolate = 0 }

# Output control statistics on the simulation

OutputTime { istep = 1 } stderr

OutputBalance { istep = 1 } stderr

OutputProjectionStats { istep = 1 } stderr

# Output simulation files every 0.1 second

OutputSimulation { step = 0.1 end = 3} sim-%g.gfs

# Viscosity using a fully implicit scheme

SourceViscosity {} (1./(T/1.78e-5+(1-T)/1.015e-3)) { beta = 1}

# Generates a movie

GModule gfsview

OutputView { step = 2e-2 } { ppm2mpeg > movie.mpg } { width = 800 height = 600 } view3D.gfv

}

GfsBox {

left = BoundaryOutflow

top = BoundaryOutflow

}

GfsBox {

top = BoundaryOutflow

}

1 2 right

## GfsView3D file 'view3D.gfv'

Generated by GfsView

# GfsView 3D View { tx = -0.303493 ty = 0.0588803 sx = 1 sy = 1 sz = 1 q0 = -0.175687 q1 = 0.0609815 q2 = 0.294233 q3 = 0.937466 fov = 4.37797 r = 0.3 g = 0.4 b = 0.6 res = 1 lc = 0.001 reactivity = 0.1 } VOF { r = 1 g = 1 b = 1 shading = Constant maxlevel = -1 font_size = 1 raster_font = 1 } { n.x = 0 n.y = 0 n.z = 1 pos = 0 } P { amin = 1 amax = 1 cmap = Jet } T { reversed = 1 use_scalar = 0 draw_edges = 0 interpolate = 0 } Solid { r = 1 g = 1 b = 1 shading = Constant maxlevel = -1 font_size = 1 raster_font = 1 } { n.x = 0 n.y = 0 n.z = 1 pos = 0 } P { amin = 1 amax = 1 cmap = Jet } { reversed = 0 use_scalar = 0 }