Hi Weiguang,
thank you for your reply. Unfortunately I think this is not the problem: the inflow waveform seems correctly imposed as you can see in the Fig_1 attached
![Fig_1.png](./download/file.php?id=3634&sid=7e82bf4ce3fbee54c0c5ecb38d9ed191)
- Fig_1.png (14.8 KiB) Viewed 335 times
related to Flow rate at the inlet and outlet faces by using the inlet.flow waveform, the 3element windkessel model and the deformable (constant) wall condition.
Moreover the .svpre command for the inlet is the same for both simulations.
.svpre files for rigid case:
mesh_and_adjncy_vtu mesh-complete/mesh-complete.mesh.vtu
set_surface_id_vtp mesh-complete/mesh-complete.exterior.vtp 1
set_surface_id_vtp mesh-complete/mesh-surfaces/Anonima.vtp 2
set_surface_id_vtp mesh-complete/mesh-surfaces/Carotide.vtp 3
set_surface_id_vtp mesh-complete/mesh-surfaces/Discendente.vtp 4
set_surface_id_vtp mesh-complete/mesh-surfaces/Inlet.vtp 5
set_surface_id_vtp mesh-complete/mesh-surfaces/Succlavia.vtp 6
fluid_density 1.06
fluid_viscosity 0.04
initial_pressure 0
initial_velocity 0.0001 0.0001 0.0001
prescribed_velocities_vtp mesh-complete/mesh-surfaces/Inlet.vtp
bct_analytical_shape parabolic
bct_period 1
bct_point_number 201
bct_fourier_mode_number 20
bct_create mesh-complete/mesh-surfaces/Inlet.vtp Inlet.flow
bct_write_dat bct.dat
bct_write_vtp bct.vtp
pressure_vtp mesh-complete/mesh-surfaces/Anonima.vtp 0
pressure_vtp mesh-complete/mesh-surfaces/Carotide.vtp 0
pressure_vtp mesh-complete/mesh-surfaces/Discendente.vtp 0
pressure_vtp mesh-complete/mesh-surfaces/Succlavia.vtp 0
noslip_vtp mesh-complete/walls_combined.vtp
write_geombc geombc.dat.1
write_restart restart.0.1
.svpre files for deformable case:
mesh_and_adjncy_vtu mesh-complete/mesh-complete.mesh.vtu
set_surface_id_vtp mesh-complete/mesh-complete.exterior.vtp 1
set_surface_id_vtp mesh-complete/mesh-surfaces/Anonima.vtp 2
set_surface_id_vtp mesh-complete/mesh-surfaces/Carotide.vtp 3
set_surface_id_vtp mesh-complete/mesh-surfaces/Discendente.vtp 4
set_surface_id_vtp mesh-complete/mesh-surfaces/Inlet.vtp 5
set_surface_id_vtp mesh-complete/mesh-surfaces/Succlavia.vtp 6
fluid_density 1.06
fluid_viscosity 0.04
initial_pressure 126000
initial_velocity 0.0001 0.0001 0.0001
prescribed_velocities_vtp mesh-complete/mesh-surfaces/Inlet.vtp
bct_analytical_shape parabolic
bct_period 1
bct_point_number 201
bct_fourier_mode_number 20
bct_create mesh-complete/mesh-surfaces/Inlet.vtp Inlet.flow
bct_write_dat bct.dat
bct_write_vtp bct.vtp
pressure_vtp mesh-complete/mesh-surfaces/Anonima.vtp 0
pressure_vtp mesh-complete/mesh-surfaces/Carotide.vtp 0
pressure_vtp mesh-complete/mesh-surfaces/Discendente.vtp 0
pressure_vtp mesh-complete/mesh-surfaces/Succlavia.vtp 0
deformable_wall_vtp mesh-complete/walls_combined.vtp
deformable_thickness 0.2
deformable_E 6.04e6
deformable_nu 0.5
deformable_kcons 0.833333
deformable_pressure 126000
deformable_solve_displacements
wall_displacements_write_vtp displacement.vtp
write_geombc geombc.dat.1
append_displacements restart.0.1
In order to be clearer, I briefly describe the procedure I followed in the attached pdf :
I notice one your response on post "Fails to apply initial conditions for deformable wall simulation", Posted on Mon Sep 16, 2019
Maybe is something related to the same problem, but I am trying to follow your instructions
Assume the restart file for the last step in a rigid simulation is restart.100.0.
Copy it to your current simulation dir. and rename it as restart.0.1
In your svpre file, remove "initial_pressure 0" and "initial_velocity 0.000 0.000 0.000".
Rerun the presolver script in the command line by typing "svpre xxxx.svpre"
But I am still not able to achieve a good solution.
The IC File should appear somewhere in the .svpre or in the solver.inp files?
Thanks,
Michela