Difference between revisions of "Archer"
From www.coria-cfd.fr
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*4096 procs on Curie, 12h wall-clock for 25000 time steps. | *4096 procs on Curie, 12h wall-clock for 25000 time steps. | ||
*Simulation is 250000 time steps. | *Simulation is 250000 time steps. | ||
− | + | *[[Media:Anim1 294 crop.avi |Marmotte.avi]] | |
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+ | === 2D gas/liquid shear layer === | ||
+ | <div class="infobox floatright" style="width: 500px;"> | ||
+ | [[File:9_11.jpeg|right|thumb|300px|]] | ||
+ | </div> | ||
+ | *M=<math>\rho_{gas}</math><math>U_{gas}</math>^2 / <math>\rho_{liq}</math><math>U_{liq}</math>^2 = 16 | ||
+ | *Ugas=30 m/s Uliq=0.26 m/s | ||
+ | *<math>\rho_{gas}</math>=1,2 kg/m3 <math>\rho_{liq}</math> =1000 kg/m3 | ||
+ | *Lx=80mm, Ly=40 mm 10mm water + 10mm air + 20mm quiet | ||
+ | *Grid: 1024x512(that is 2048x1024 level set and VOF, mesh is 40 µm) | ||
+ | *512 procs on Curie | ||
+ | *18h wall clock for 100000 time steps. | ||
+ | *Simulation on 2 000 000 time steps | ||
+ | *[[Media:Ite1_20_1sur10_25im.avi|2Dliquid_shear_layer.avi]] |
Revision as of 18:54, 21 November 2013
Contents
OBJECTIVE: Liquid/Gaz Interface Simulations
Describe the interface motion precisely | ![]() |
Level Set Method |
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Handle jump conditions at the interface | without artificial smoothing | ![]() |
Ghost Fluid Method |
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Respect mass conservation | ![]() |
VOF Method |
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Solve incompressible Navier Stokes equations | ![]() |
Projection Method |
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Archer is a 3D incompressible Navier Stokes solver with Level Set-Ghost Fluid-VOF coupling and MPI parallelization
NUMERICS
- Cartesian mesh
- Mac grid (velocities on cell boundaries)
- WENO 5 scheme for convective terms, Adams Bashforth or RK3 or split algorithm in time
- Multigrid algorith for preconditionning Conjugate Gradient Method in Poisson equation solver
- Ghost Fluid method for variable discontinuities at the interface
- CLSVOF for mass conservation
- MPI parallelization
UNDER DEVELOPMENT
- Immersed boundaries
- Adaptive mesh refinement
- Coupling with Lagrangian solver
- New convection scheme (modified Rudman's method)
GALLERY
Turbulent jet
Diesel type Jet Atomization : Diameter: 100µm, Liquid velocity 100 ms-1, Turbulence 5%, gas velocity: 0 ms-1, =696 kgm-3, =25 kgm-3
=1.210-3kgm-1s-1, =10-5kgm-1s-1, =0.06Nm-1 Numerical simulation by coupling Level Set / VOF / Ghost fluid methods
Mesh : 256x256x2048 (130 millions points) MPI parallelization 128 procs.
Triple disk injector
- Coupling between internal flow simulations and DNS of primary breakup
- Radius of the jet exit: 90 microns
- Mesh 256x1024x1024 (~270 millions) dx~1.44 micron
- ~3000 nodes on the (half) jet exit
- 2048 procs
- Triple.avi
Liquid/Gas mixing layer
- Air/water mixing layer
- 30m/s in air, 0.3 in water
- Grid is 512x512x1024 nodes
- Mesh size equals 48 µm.
- 2048 procs, 20 hours for 3500 time steps; Simulation on 70000 time steps, dt~=10-6 s
Air assisted atomization
- Air/water Jet « Marmottant »
- Ugas=35m/s and Uliq=0.2m/s
- =1,2 kg/m3 =1000 kg/m3
- Lx=45.6mm (4mm+1.7mm)x8 that is 4 the « jet +gas » diameter
- Grid: 256x256x256,(512x512x512 for level set and VOF, mesh is 90µm)
- 4096 procs on Curie, 12h wall-clock for 25000 time steps.
- Simulation is 250000 time steps.
- Marmotte.avi
2D gas/liquid shear layer
- M=^2 / ^2 = 16
- Ugas=30 m/s Uliq=0.26 m/s
- =1,2 kg/m3 =1000 kg/m3
- Lx=80mm, Ly=40 mm 10mm water + 10mm air + 20mm quiet
- Grid: 1024x512(that is 2048x1024 level set and VOF, mesh is 40 µm)
- 512 procs on Curie
- 18h wall clock for 100000 time steps.
- Simulation on 2 000 000 time steps
- 2Dliquid_shear_layer.avi