ANS is committed to advancing, fostering, and promoting the development and application of nuclear sciences and technologies to benefit society.
Explore the many uses for nuclear science and its impact on energy, the environment, healthcare, food, and more.
Explore membership for yourself or for your organization.
Conference Spotlight
2026 ANS Annual Conference
May 31–June 3, 2026
Denver, CO|Sheraton Denver
Latest Magazine Issues
Apr 2026
Jan 2026
Latest Journal Issues
Nuclear Science and Engineering
May 2026
Nuclear Technology
March 2026
Fusion Science and Technology
Latest News
A year in orbit: ISS deployment tests radiation detectors for future space missions
The predawn darkness on a cool Florida night was shattered by the ignition of nine Merlin engines on a SpaceX Falcon 9 rocket. The thrust of the engines shook the ground miles away. From a distance, the rocket appeared to slowly rise above the horizon. For the cargo onboard, the launch was anything but gentle, as the ignition of liquid oxygen generated more than 1.5 million pounds of force. After the rocket had been out of sight for several minutes, the booster dramatically returned to Earth with several sonic booms in a captivating show of engineering designed to make space travel less expensive and more sustainable.
Haneen Alzahrani, Kentaro Matsushita, Takaaki Sakai, Toshiki Ezure, Masaaki Tanaka
Nuclear Technology | Volume 211 | Number 10 | October 2025 | Pages 2446-2458
Research Article | doi.org/10.1080/00295450.2025.2472582
Articles are hosted by Taylor and Francis Online.
There is a possibility that argon (Ar) cover gas in the upper part of the reactor vessel (RV) could enter the sodium coolant by vortices, causing output disturbance. Hence, it is necessary to evaluate this gas entrainment phenomenon. To predict the flow pattern in the upper part of the RV using computational fluid dynamics analysis, there is a need to establish an appropriate mesh arrangement.
In this study, the applicability of the adaptive mesh refinement (AMR) method to predict gas entrainment vortices accurately was examined. An initial coarse mesh (20 mm) that simulate the test section of the experimental apparatus in the circulating water loop was created. The initial mesh was refined with two indices: the first index (index 1) is when the second invariant, Q, of the velocity gradient tensor is negative, and the second one (index 2) is the pressure gradient index added to index 1. Transient calculations were then performed on the refined meshes under each condition, and the results were compared with a reference mesh with cubic cells of a 5-mm width.
As a result, comparing the pressure distribution of the reference mesh with the other meshes refined with the two indices, index 2 was found to be more similar to that of the reference mesh. In conclusion, the applicability of the AMR method with the condition of index 2 was confirmed for this experimental system in which unsteady wake vortices are generated.