ORCiD
- Deborah Greaves: 0000-0003-3906-9630
- Yeaw Chu Lee: 0000-0002-0463-5586
Description
This experimental dataset was generated as part of a PhD research project on liquid sloshing for next-generation aircraft fuel tank applications (EP/W522223/1). It comprises three distinct experimental campaigns designed to characterise sloshing behaviour under a range of controlled dynamic conditions with water-air. A circular tank under forced horizontal excitation. A circular tank under forced vertical excitation. A circular tank under high-acceleration vertical excitation. Together, these campaigns provide a comprehensive set of measurements capturing fluid response in a circular tank across varied excitation modes and acceleration regimes. The dataset is intended to support further research, model validation, and the development of predictive tools for sloshing dynamics in aerospace fuel systems.
Publication Date
2026-01-31
Deposit Date
January 2026
Publisher
University of Plymouth
Embargo Period
2026-01-31
Keywords
Sloshing, Circular tank
Creative Commons License
This work is licensed under a Creative Commons Attribution 4.0 International License.
Recommended Citation
Colville, S., Gambioli, F., Greaves, D., & Lee, Y. (2026) Experimental data: Sloshing in a circular tank [data set]. University of Plymouth Research Repository. Available at: https://doi.org/10.24382/87c2f31a-524d-41ec-95d4-383fa82b10b8
This item is under embargo until 31 January 2026
