2014
DOI: 10.1016/j.fusengdes.2014.02.005
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Simulation of neutral gas flow in a tokamak divertor using the Direct Simulation Monte Carlo method

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Cited by 20 publications
(16 citation statements)
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“…It has to be noted that this strong recycle pattern has not been found in the calculations with the previous divertor design for which the pumped flow and the backflow was of similar magnitude [4]. In 2D DSMC calculations on the intra cassette flow pattern [5,6], a reversed behaviour was found, indicating a much stronger flow towards the pumps than towards the plasma. This seems to indicate that the ITERVAC results discussed above are mainly due to the flows in the gaps in between the cassettes.…”
Section: Simulation Results For the Burn Phasementioning
confidence: 77%
See 1 more Smart Citation
“…It has to be noted that this strong recycle pattern has not been found in the calculations with the previous divertor design for which the pumped flow and the backflow was of similar magnitude [4]. In 2D DSMC calculations on the intra cassette flow pattern [5,6], a reversed behaviour was found, indicating a much stronger flow towards the pumps than towards the plasma. This seems to indicate that the ITERVAC results discussed above are mainly due to the flows in the gaps in between the cassettes.…”
Section: Simulation Results For the Burn Phasementioning
confidence: 77%
“…The power crossing the magnetic separatrix and entering the scrape-off layer was 100 MW. The input parameters for these simulations were also used for DSMC simulations and the comparison with ITERVAC, described in [5].…”
Section: Simulation Results For the Burn Phasementioning
confidence: 99%
“…For lower density cases the same/similar dependence was obtained with the DIVGAS code utilising Direct Simulation Monte Carlo (DSMC, [33]), and both DIVGAS and EIRENE were positively benchmarked against each other [34]. For higher densities and detached JET-ILW divertors the DSMC model conjectures a significant effect of the neutral viscosity at Knudsen numbers Kn < 1.…”
Section: Particle and Power Exhaustmentioning
confidence: 63%
“…Plasma plumes exist widely in aerospace propulsion [1], industrial coating [2,3] and nuclear reactors [4,5] such as plasma thrusters in the aerospace propulsion system [6] and micro-cathode vacuum arc thrusters for microsatellites [7]. In the thruster devices described above, plasma is injected to the environmental medium at an extremely high speed, and a feather-like jet flow called a plume is diffused into the surrounding environment rapidly.…”
Section: Introductionmentioning
confidence: 99%