Study on Floating Motion Characteristics and Stability of Unpowered Underwater Carrier (UUC)

Authors

  • Qianjin Xiao
  • Wei Chen
  • Wei Wei
  • Heyun Cao
  • Xu Hu

DOI:

https://doi.org/10.54097/nxhrt250

Keywords:

Water-exit velocity and attitude; Floating motion characteristics; Stability; UUC.

Abstract

The water-exit velocity and attitude of UUC are crucial for underwater launching aircraft-like payloads. To ensure that the design of the UUC is reasonable, the investigation on motion characteristics and stability of the UUC in vertical floating process are carried out. Firstly, a computational model of the UUC has been established. Then, a combination method of theoretical calculations and CFD simulations has been used to study the relationship between model parameters and hydrodynamics parameters. Finally, stability analysis has been conducted for initial heading angle of 3° and 6°. The results show that increasing the net buoyancy can allow the UUC to obtain a larger water-exit velocity, while to reduce accelerated time and distance. The designed UUC can achieve stably convergence under the disturbance of initial heading angle, indicating that the UUC has a good motion stability in vertical rising process.

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References

Liang Li, Weichen Li, et al. Modeling and simulation of buoy floating process underwater. Digital Ocean & Underwater Warfare, Vol. 4 (2021) No. 3, p. 227-232.

Tianjian Zhang, Chengzhu Wei, et al. Study on floating and diving for deep-water buoyancy-driven vehicle. Ship Engineering, Vol. 39 (2017) No. 12, p. 87-94.

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Qiaosheng Zhao, Tian Fang, et al. Stability analysis and experimental verification of the buoyant body’s rising attitude. Journal of Ship Mechanics, Vol. 46 (2022) No. 1, p. 50-58.

Xuejing Zhang: Design and stability study of buoy launcher (Master Degree, North China Instituet of Aerospace Engineering, China 2022). p. 9-65.

Yujin Lu: Trajectory Modeling and Numerical Simulation of Unpowered Carrier Underwater Launching (Master Degree, Nanjing University of Aeronautics and Astronautics, China 2018). p. 12-78.

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Published

14-03-2024