The Study of Triangular Flow Regulators
The paper presents the results of tests of flow regulators with a triangular prismatic cross-section chamber. The aim of the paper was to experimentally and numerically (CFD) assess the water flow for different design variants of the regulators. Three variants of flow regulators with a triangular prismatic cross-section chamber were analysed: without a barrier (FRWB), with a short barrier (FRSB), and with a long barrier (FRLB). Simultaneously, numerical simulations were carried out using the SST k-ω turbulence model (CFD). The obtained flow characteristics Q = f(H) showed the clear effect of the presence and length of the barrier on the efficiency of flow restriction. The regulators with a long barrier (FRLB) provided the highest flow damping and the highest stability of the system’s operation, which was confirmed by the experimental tests and CFD analyses. The regulators without a barrier (FRWB) were characterized by the highest liquid flow rate and the lowest damping efficiency. The use of a long barrier allowed for an increased control efficiency and improved predictability of the device’s operation. The triangular cross-section of the chamber favours the formation of a stable vortex flow and increases the efficiency of the regulator’s operation.
Authors
- Andżelika Krupińska (ORCID: https://orcid.org/0000-0002-1485-9794)
- Daniel Janecki (ORCID: https://orcid.org/0000-0003-4462-5128)
- Magdalena Matuszak
- Sylwia Włodarczak (ORCID: https://orcid.org/0000-0003-0561-0177)
- Marek Ochowiak (ORCID: https://orcid.org/0000-0003-1543-9967)
- Magdalena Olszewska (ORCID: https://orcid.org/0009-0009-0093-9265)
Institutions
- Bydgoszcz University of Science and Technology (PL)
- University of Opole (PL)
- Poznań University of Technology (PL)
- AGH University of Krakow (PL)
Publication Details
- Journal
- Applied Sciences
- Published
- 2025-11-20
- DOI
- https://doi.org/10.3390/app152212325
- Primary Topic
- Plasma and Flow Control in Aerodynamics
- Type
- article
- Field-Weighted Citation Impact
- 0.00