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First International Conference on HYDROGEN SAFETY. On numerical simulation of liquefied and gaseous hydrogen releases at large scales. V. Molkov, D. Makarov, E . Prost. 8-10 September 2005, Pisa, Italy.
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First International Conference on HYDROGEN SAFETY On numerical simulation of liquefied and gaseous hydrogen releases at large scales V. Molkov, D. Makarov, E. Prost 8-10 September 2005, Pisa, Italy
Introduction of hydrogen as an energy carrier makes great demands on hydrogen safety. Development of robust and reliable risk assessment methodologies requires all-round validation of models and tools. • The need to model non-uniform hydrogen-air mixture formation at real scales is important to have realistic initial conditions for subsequent modelling of partially premixed hydrogen combustion. • The aim of this study is validations of the LES model in application to large-scale hydrogen release scenarios and formulation of tasks for future research in this area.
Contents • The LES model • LH2 release in open atmosphere • GH2 release in a closed vessel
LES model (1/2) • Conservation of mass • Conservation of momentum • Conservation of energy
LES model (2/2) • RNG SGS turbulence model • Conservation of “H2”concentration
NASA experiment Chirivella J.E., Witcofski, R.D. Am. Inst. Chem. Eng. Symp., 82, No 251, 1986, pp.120-142: - Spill 5.11 m3 (361.8 kg) of LH2 in 38 s - LH2 pool radius between 2 and 3 m - Total evaporation time 43 s - Wind speed ~2.2 m/s at height 10 m
Calculation domain (1/2) Spill area and instrumentation towers area Cloud propagation area 70 m 180 m Characteristic size of CV: Numerical grid: 156133 CV • tower location 1.0 - 2.0 m • cloud area 2.0 - 3.0 m • the rest of domain up to 10 m
Calculation domain (2/2) Cloud propagation area Spill area 70 m 180 m Characteristic size of CV: Numerical grid: 103163 CV • spill area 0.6 - 1.0 m • cloud area 2.0 - 3.0 m • the rest of domain up to 10 m
Numerical details • Initial conditions • atmosphere velocity profile: • where(provided u=2.2 m at H=10 m) • Boundary conditions • velocity profile at inflow • prescribed pressure conditions at outflow boundaries, p=0 Pa • H2 injection • mass injection rate • Run 1: injection area radius • Run 2: injection area radius • average injection velocity • instant injection velocity • Run 1: turbulence • Run 2: turbulence • Geomerty: Run 1 (no pool border, no obstacles), Run 2 (+)
H2 concentration (Run 1) Texp = 21.33 s Tsim = 21.36 s
H2 concentration (Run 2) Texp = 21.33 s Tsim = 21.35 s
Phenomena to be addressed • Condensation of air in temperature range 20-90 K (with heat release) and evaporation above 90 K • Two phase flow (gas: hydrogen-air; solid: air ice) • Detailed spill modelling (initial fractions of GH2 and LH2; heat transfer to the ground: initial violent evaporation stage, etc)
5.5m 2.2m Experiment Volume injection rate: V=4.5 l/s Time of release = 60 seconds 1.4m H2
Calculation domain Non-uniform tetrahedral grid CV number: 54004 CV size: 0.01-0.10 m close to place of H2 injection CV size: up to 0.20 m in the rest of domain “Uniform” grid CV number: 28440 CV size: 0.14-0.20 m 3-251 min 0-180 s
Numerical details • Initial conditions • quiescent air, u=0 m/s, • initial air concentration Yair=1.0, • initial temperature T=293K • Boundary conditions • t=0-1s: Vinj increased from 0 to 57.5 m/s • t =1-59s: Vinj=57.5 m/s • t=59-60s: decrease from 57.5 to 0 m/s • t=60s-251min: Vinj=0 m/s • YH2=1.0, Tinj=293K • Numerical details • explicit linearisationof the governing equations • implicit method for solution of linear equation set • second order accurate upwind scheme for convection terms, central-difference scheme for diffusion terms • Time steps: t=0-180 s: t=0.01 s; t=3-251 min: t=0.01-1.0 s
Hydrogen distribution 1 2 min 50 min 100 min 250 min
Residual velocities 50min: Vmax=10 cm/s 100min: Vmax=8 cm/s 250min: Vmax=5 cm/s
Conclusions • The LES model has been applied to analyse large-scale experimental LH2 and GH2 releases. • The simulation of non-uniform flammable cloud formation, resulting from a LH2 spill, reproduced a characteristic structure of the turbulent eddies and the direction of cloud propagation. • The simulation results were found to depend on initial and boundary conditions. • The air condensation-evaporation sub-model may improve predictive capabilities of the LES model
Conclusions • Good agreement was achieved with experimental data on GH2 release in 20-m3 closed vessel up to t=250 min after the 1 minute release. • The LES results demonstrated that random flow field remains in the vessel long time after the injection and this is presumably responsible for H2 transport. • Further experiments with observation of velocity field after release and simulations with higher accuracy are required to give final answer to this question.