Two-objective optimisation of an intake diffuser for outboard dynamic-inlet waterjets
The Outboard Dynamic-inlet Waterjet (ODW) represents one of the latest advances in marine propulsion, providing several propulsive benefits over the existing technologies. Similar to aero-engines, the ODW consists of a single axisymmetric nacelle housing a pump which pressurises the flow that is accelerated through a nozzle. This study progresses current research on the system, improving the efficiency of the existing design through a two-objective optimisation of the propulsor inlet, whose shape directly affects drag. Adapting a thrust/drag bookkeeping scheme from aeronautical studies, the investigation optimises the system net thrust by balancing two conflicting targets: minimum inlet drag and maximum pressure recovery. Propulsive statistics are extracted by modelling the 2D axisymmetric geometry with Reynolds-Averaged Navier–Stokes (RANS) equations and processed by a genetic algorithm, controlling the manipulation of the baseline parameterisation. Optimised individuals indicate that decreasing the intake length and thickness can reduce the initial drag by 18% with marginal improvements on the pressure recovery, not exceeding 0.3%. Highlighting the specific role of each force component on the two objectives, the study shows that, adopting the present bookkeeping scheme, the proposed approach can optimise ODW performance through a fine control of the correlations between the geometrical parameters and the multiple drag terms.
Authors
- Andrea Magrini (ORCID: https://orcid.org/0000-0002-3539-149X)
- Ernesto Benini (ORCID: https://orcid.org/0000-0002-5061-4284)
- Francesco De Vanna (ORCID: https://orcid.org/0000-0001-6627-5451)
- Filippo Avanzi (ORCID: https://orcid.org/0000-0001-7671-1181)
Publication Details
- Journal
- Ocean Engineering
- Published
- 2025-04-15
- DOI
- https://doi.org/10.1016/j.oceaneng.2025.121187
- Citations
- 1
- Primary Topic
- Cavitation Phenomena in Pumps
- Type
- article
- Field-Weighted Citation Impact
- 0.86
Funders
- Università degli Studi di Padova