2017
DOI: 10.1007/s10891-017-1641-7
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Computational and Experimental Investigations of the Coolant Flow in the Cassette Fissile Core of a KLT-40S Reactor

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Cited by 12 publications
(4 citation statements)
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“…1) is an aerodynamic open loop. It was designed for research of local values of flow velocity and pressure, as well as mixing of coolant in models of main equipment of nuclear reactors [10][11][12][13]. The stand includes: high-pressure fan, receiver tank, pipeline system, experimental model, measuring devices.…”
Section: Experimental Facilitymentioning
confidence: 99%
“…1) is an aerodynamic open loop. It was designed for research of local values of flow velocity and pressure, as well as mixing of coolant in models of main equipment of nuclear reactors [10][11][12][13]. The stand includes: high-pressure fan, receiver tank, pipeline system, experimental model, measuring devices.…”
Section: Experimental Facilitymentioning
confidence: 99%
“…Another study of the hydrodynamic aspects at the fuel assembly-level has also been carried out by manufacturing a prototype of KLT-40S fuel device with the same geometry scale [7]. An experimental system was made by adding instrumentation and control aspects to the experimental model.…”
Section: Introductionmentioning
confidence: 99%
“…The most accurate method of obtaining these data can be an aerodynamic experiment using an enlarged model of the fuel assembly [12][13][14][15]. However, taking into account the active use of CFD programs for thermal-hydraulic calculations in nuclear industry [16][17][18][19][20], the authors of this work carried out a numerical simulation of the coolant flow in the fragment of a fuel assembly using Ansys CFX. The results of the calculations were compared with the experimental data in order to evaluate the capabilities of the selected program for carrying out similar studies.…”
Section: Introductionmentioning
confidence: 99%