Effects of the partially movable control fin with end plate of underwater vehicle
- Authors
- Jung, Chul-Min; Paik, Bu-Geun; Park, Warn-Gyu
- Issue Date
- 1월-2017
- Publisher
- SOC NAVAL ARCHITECTS KOREA
- Keywords
- Control fin; End plate; Low aspect ratio control fin; Wing-tip vortex; CFD analysis and experiment
- Citation
- INTERNATIONAL JOURNAL OF NAVAL ARCHITECTURE AND OCEAN ENGINEERING, v.9, no.1, pp 55 - 65
- Pages
- 11
- Journal Title
- INTERNATIONAL JOURNAL OF NAVAL ARCHITECTURE AND OCEAN ENGINEERING
- Volume
- 9
- Number
- 1
- Start Page
- 55
- End Page
- 65
- URI
- https://www.kriso.re.kr/sciwatch/handle/2021.sw.kriso/591
- DOI
- 10.1016/j.ijnaoe.2016.07.005
- ISSN
- 2092-6782
2092-6790
- Abstract
- Underwater torpedo has control fin with very low aspect ratio due to launching from limited size of cylindrical torpedo tube. If the aspect ratio of control fin of underwater vehicle is very low three-dimensional flow around control fin largely reduces control forces. In this study, the end plate was applied to reduce the three-dimensional flow effects of partially movable control fin of underwater vehicle. Through numerical simulations the flow field around control fin was examined with and without end plate for different flap angles. The pressure, voracity, lift and torque on the control fin were analyzed and compared to experiments. The comparison have shown a reasonable agreement between numerical and experimental results and the effect of end plate on a low aspect ratio control fin. When the end plate was attached to the movable control fin, the lift increased and the actuator shaft torque did not significantly change. As this means less consumption of the actuator shaft torque compared to the control fin that has the same control force, the inner actuator capacity can be reduced and energy consumption can be saved. Considering this, it is expected to be effectively applied to the control fin design of underwater vehicles such as torpedoes. Copyright (C) 2016 Society of Naval Architects of Korea. Production and hosting by Elsevier B.V.
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