Loss of vacuum accident (LOVA): Comparison of computational fluid dynamics (CFD) flow velocities against experimental data for the model validation

• Published in: Fusion engineering and design Vol. 86; no. 4; pp. 330 - 340
• Main Authors: Bellecci, C., Gaudio, P., Lupelli, I., Malizia, A., Porfiri, M.T., Quaranta, R., Richetta, M.
• Format: Journal Article
• Language: English
• Published: Amsterdam Elsevier B.V 01-06-2011; Elsevier
• Subjects: Applied sciences; CFD; Controled nuclear fusion plants; Dust; Energy; Energy. Thermal use of fuels; Exact sciences and technology; Installations for energy generation and conversion: thermal and electrical energy; ITER; LOVA; STARDUST; Velocity; CFD; Dust; ITER; LOVA; Velocity; STARDUST; Deuterium; Tokamak; Plasma; LOCA; Coolant; Computational fluid dynamics; Computer simulation; Divertor; Tritium; Nuclear fusion reactor; Aerosols; Flow velocity; Safety
• ISSN: 0920-3796; 1873-7196
• DOI: 10.1016/j.fusengdes.2011.02.057

A recognized safety issue for future fusion reactors fueled with deuterium and tritium is the generation of sizeable quantities of dust. Several mechanisms resulting from material response to plasma bombardment in normal and off-normal conditions are responsible for generating dust of micron and sub-micron length scales inside the VV (Vacuum Vessel) of experimental fusion facilities. The loss of coolant accidents (LOCA), loss of coolant flow accidents (LOFA) and loss of vacuum accidents (LOVA) are types of accidents, expected in experimental fusion reactors like ITER, that may jeopardize components and plasma vessel integrity and cause dust mobilization risky for workers and public. The air velocity is the driven parameter for dust resuspension and its characterization, in the very first phase of the accidents, is critical for the dust release. To study the air velocity trend a small facility, Small Tank for Aerosol Removal and Dust (STARDUST), was set up at the University of Rome “Tor Vergata”, in collaboration with ENEA Frascati laboratories. It simulates a low pressurization rate (300
Pa/s) LOVA event in ITER due to a small air inlet from two different positions of the leak: at the equatorial port level and at the divertor port level. The velocity magnitude in STARDUST was investigated in order to map the velocity field by means of a punctual capacitive transducer placed inside STARDUST without obstacles. FLUENT was used to simulate the flow behavior for the same LOVA scenarios used during the experimental tests. The results of these simulations were compared against the experimental data for CFD code validation. For validation purposes, the CFD simulation data were extracted at the same locations as the experimental data were collected for the first four seconds, because at the beginning of the experiments the maximum velocity values (that could cause the almost complete dust mobilization) have been measured. In this paper the authors present and discuss the computer-simulation data and compare them with data collected in STARDUST.