Abstract
This study summarizes the experimental effort to characterize the flow fields of various interior subchannels in a 61-pin wire-wrapped hexagonal fuel bundle prototypical for a sodium fast reactor. The objective was to generate high spatiotemporal velocity field data for computational fluid dynamics turbulence model validation. The experimental facility employed the matched-index-of-refraction and modern laser-based optical measurement techniques. It is the largest transparent hexagonal test fuel assembly. Measurements were performed in two planes parallel to the axial flow, Interior-1 and Center-2. The Interior-1 location captured fluid interactions in four narrower subchannels formed by the exterior row of pins near the hexagonal duct wall. The Center-2 location captured fluid interactions in two wider subchannels spanning from the center pin out to the hexagonal duct wall. All measurements have been performed at a Reynolds number of 19,000. Results include discussion about statistical convergence of the dataset, along with flow statistics such as ensemble-averaged velocity, root-mean-square fluctuating velocity, Reynolds stress, and integral length scales.
Original language | English |
---|---|
Pages (from-to) | 295-304 |
Number of pages | 10 |
Journal | International Journal of Heat and Fluid Flow |
Volume | 71 |
DOIs | |
State | Published - Jun 2018 |
Externally published | Yes |
Funding
This material is based upon work supported by the U.S. Department of Energy under Award Numbers DE-NE0008321 and DE-NE0008652 . The experimental flow facility was designed and constructed under DE-NE0008321 with technical collaboration from Areva, Argonne National Laboratory, and TerraPower. Data analysis has been performed under DE-NE0008652. Special thanks go out to Dr. Brian Jackson for his technical feedback and recommendations throughout the course of this work.
Funders | Funder number |
---|---|
U.S. Department of Energy | DE-NE0008652, DE-NE0008321 |