#################################################
#
#   Input file for CFD Monolithic Solver
#
#################################################
mesh_path           : '/home/p283370/Desktop/PhD/AORTA/MESH/aorta_fine/aorta_fine_marked.h5'
write_xdmf          : False
savepath           : '/home/yeye/Desktop/PhD/AORTA/DATA/monolithic/'
write_checkpoint    : False
checkpoint_path     : '/home/yeye/Desktop/PhD/AORTA/DATA/monolithic/checkpoint/'
write_outlets       : False
outlets_path        : '/home/yeye/Desktop/PhD/AORTA/DATA/monolithic/outlets/'

Tf                  : 0.9               # seg
density             : 1.2               # gr/cm3
dynamic_viscosity   : 0.035
dt                  : 0.005
dt_write            : 0.01
checkpoint_dt       : 0.02


stab:
    pspg     : 1
    epsilon  : 0.01
    backflow : 1
    back_id  : [3,4,5,6]
    temam    : 1
    supg     : 0
    pssu     : 0

param:
    U             : 60
    period        : 0.7
    Nvel          : 1
    Npress        : 1
    theta         : 1
   
windkessel:
    id        : [3,4,5,6]
    R_p       : {'3':100 , '4':250,    '5':250 ,    '6':250 }
    R_d       : {'3':1000, '4':8000,   '5':8000 ,   '6':8000}
    C         : {'3':0.01, '4':0.0001, '5':0.00001, '6':0.0001}
    alpha     : {'3':0 ,   '4':0 ,     '5':0 ,      '6':0}
    beta      : {'3':0 ,   '4':0 ,     '5':0 ,      '6':0}
    gamma     : {'3':0 ,   '4':0 ,     '5':0 ,      '6':0}