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6.1 - Fluid Structure Coupling

6.1 - Fluid Structure Coupling

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6.1 - Fluid Structure Coupling

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Title

Fuel tank - Fluid Structure Coupling

rad_ex_6.1

Number

6.1

Brief Description

Sloshing inside a fuel tank by simulating the fluid structure coupling. The tank deformation is achieved by applying an imposed velocity on the left corners. Water and air inside the tank are modeled with the ALE formulation. The tank container is described using a Lagrangian formulation.

Keywords

Fluid structure coupling simulation, and ALE formulation
Shell and brick elements
Hydrodynamic and bi-phase liquid gas material (/MAT/LAW37)

RADIOSS Options

ALE boundary conditions (/ALE/BCS)
J. Donea Grid Formulation (/ALE/GRID/DONEA)
Boundary conditions (/BCS)
Gravity (/GRAV)
Imposed velocity (/IMPVEL)
ALE material formulation (/ALE/MAT)

Input File

Fluid_structure_coupling: <install_directory>/demos/hwsolvers/radioss/06_Fuel_tank/1-Tank_sloshing/Fluid_structure_coupling/TANK*

Technical / Theoretical Level

Advanced

Overview


Aim of the Problem

A numerical simulation of fluid-structure coupling is performed on sloshing inside a deformable fuel tank. This example uses the ALE (Arbitrary Lagrangian Eulerian) formulation and the hydrodynamic bi-material law (/MAT/LAW37) to model interaction between water, air and the tank container.

Physical Problem Description

A rectangular tank made of steel is partially filled with water, the remainder being supplemented by air. The initial distribution pressure is known and supposed homogeneous. The tank container dimensions are 460 mm x 300 mm x 10 mm, with thickness being at 2 mm.

Deformation of the tank container is generated by an impulse made on the left corners of the tank for analyzing the fluid-structure coupling.

rad_ex_6-1

Fig 1: Problem description.

The steel container is modeled using the elasto-plastic model of Johnson-Cook law (/MAT/LAW2) with the following parameters:

Density:  0.0078 g/mm3
Young’s modulus:  210000 MPa
Poisson’s ratio:  0.29
Yield stress:  180 MPa
Hardening parameter:  450 MPa
Hardening exponent:  0.5

The material air-water bi-phase is described in the hydrodynamic bi-material liquid-gas law (/MAT/LAW37). Material law 37 is specifically designed to model bi-material liquid gas.

The equations used to describe the state of viscosity and pressure are:

Viscosity:

ex_6_equation

Liquid EOS:

ex_6_liquid_eq

where, ex_6_liquid_eq2

Gas EOS:

ex_6_gas_equation

The equilibrium is defined by: Pl = Pg

Where, Sij is the deviatoric stress tensor and eij is the deviatoric strain tensor.

Material parameters are:

For liquid:
Liquid reference density: 0.001 g/mm3
ClLiquid bulk modulus: 2089 N/mm2
alInitial mass fraction liquid proportion: 100%
ratioShear kinematic viscosity (= symbol_u / ):  0.001 mm2/ms
For gas:
Gas reference density: 1.22x10-6 g/mm3
ratiogShear kinematic viscosity (= symbol_u / ): 0.00143 mm2/ms
YConstant perfect gas: 1.4
P0Initial pressure reference gas: 0.1 N/mm2

The main solid type 14 properties for air/water parts are:

Quadratic bulk viscosity/linear bulk viscosity: 10-20
Hourglass bulk coefficient: 10-5

Analysis, Assumptions and Modeling Description


Modeling Methodology

Air and water are modeled using the ALE formulation and the bi-material law (/MAT/LAW37). The tank container uses a Lagrangian formulation and an elasto-plastic material law (/MAT/LAW2).

rad_ex_fig_6-8

Fig 2: Air and water mesh (ALE brick elements).

rad_ex_fig_6-3

Fig 3: Tank container mesh (shell elements).

Using the ALE formulation, the brick mesh is only deformed by tank deformation the water flowing through the mesh. The Lagrangian shell nodes still coincide with the material points and the elements deform with the material: this is known as a Lagrangian mesh. For the ALE mesh, nodes on the boundaries are fixed in order to remain on the border, while the interior nodes are moved.

RADIOSS Options Used

Velocities (/IMPVEL) are imposed on the left corners in the X direction.

 

Table 1: Imposed velocity versus time curve

Velocity (ms-1)

0

5

0

0

Time (ms)

0

12

12.01

50

 

rad_ex_fig_6-4

Fig 4: Kinematic condition: imposed velocities.

Regarding the ALE boundary conditions, constraints are applied on:

Material velocity
Grid velocity

All nodes, except those on the border have grid (/ALE/BCS) and material (/BCS) velocities fixed in the Z-direction. The nodes on the border only have a material velocity (/BCS) fixed in the Z-direction.

Both the ALE materials air and water must be declared ALE using /ALE/MAT. Lagrangian material is automatically declared Lagrangian.

The /ALE/GRID/DONEA option activates the J. Donea grid formulation to compute the grid velocity. See the RADIOSS Theory Manual for further explanations about this option.

Simulation Results and Conclusions


Curves and Animations

Fluid – Structure Coupling

ex6_x_momentum_variation

Fig 5: X – momentum variation for each part.

Kinematic conditions generate oscillations of the structure.

ex6_density_attached_variation

Fig 6: Density attached to the various brick elements.

Fluid Structure Coupling

Time = 0 ms

Density

density-0

Velocity

velocity-0

 

Fluid Structure Coupling

Time = 12 ms

Density

density-12

Velocity

velocity-12

 

Fluid Structure Coupling

Time = 42 ms

Density

density-42

Velocity

velocity-42