inputs
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50
input/cfd_input.yaml
Executable file
50
input/cfd_input.yaml
Executable file
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#################################################
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#
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# Input file for CFD Monolithic Solver
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#
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#################################################
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mesh_path : '/home/p283370/Desktop/PhD/AORTA/MESH/aorta_fine/aorta_fine_marked.h5'
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write_xdmf : False
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savepath : '/home/yeye/Desktop/PhD/AORTA/DATA/monolithic/'
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write_checkpoint : False
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checkpoint_path : '/home/yeye/Desktop/PhD/AORTA/DATA/monolithic/checkpoint/'
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write_outlets : False
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outlets_path : '/home/yeye/Desktop/PhD/AORTA/DATA/monolithic/outlets/'
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Tf : 0.9 # seg
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density : 1.2 # gr/cm3
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dynamic_viscosity : 0.035
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dt : 0.005
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dt_write : 0.01
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checkpoint_dt : 0.02
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stab:
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pspg : 1
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epsilon : 0.01
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backflow : 1
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back_id : [3,4,5,6]
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temam : 1
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supg : 0
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pssu : 0
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param:
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U : 60
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period : 0.7
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Nvel : 1
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Npress : 1
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theta : 1
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windkessel:
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id : [3,4,5,6]
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R_p : {'3':100 , '4':250, '5':250 , '6':250 }
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R_d : {'3':1000, '4':8000, '5':8000 , '6':8000}
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C : {'3':0.01, '4':0.0001, '5':0.00001, '6':0.0001}
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alpha : {'3':0 , '4':0 , '5':0 , '6':0}
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beta : {'3':0 , '4':0 , '5':0 , '6':0}
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gamma : {'3':0 , '4':0 , '5':0 , '6':0}
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