• Title/Summary/Keyword: 트림탭

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A Study on the Hydrodynamic Performance of High-Speed Vessel with Trim Tab Using Full-Scale CFD Simulation (실선 스케일 CFD 해석 기반 트림 탭이 부착된 고속선의 유체동역학적 성능 분석)

  • Lee, Jonghyeon;Park, Dong-Woo
    • Journal of the Korean Society of Marine Environment & Safety
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    • v.27 no.5
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    • pp.656-665
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    • 2021
  • In this study, trim tabs were attached to end of stern hull of a small high-speed vessel of length approximately 10 m and Froude number 1.0 to improve resistance performance and passenger comfort. Before computational fluid dynamics (CFD) simulations to assess the performance according to various geometries of the trim tab, the scale effect had been found through a previous study, so full-scale simulations were performed. The trim tab chord length was set to 0.5 %, 1.0 % and 1.5 % of LPP, and its angle to base line was varied in intervals of 5°. It decreased trim by stern and flotation: the greater the angle and length, the greater was the effect. Then it had pressure resistance decreased and shear resistance increased, and reduction ratio of total resistance varied accordingly. The results of this study indicated that the resistance performance was improved about 27 % at optimal running attitude that was the trim by stern about 1.5°.

A Study on the Scale Effect and Improvement of Resistance Performance Based on Running Attitude Control of Small High-Speed Vessel (소형 고속선박의 항주자세 제어에 따른 저항성능 개선 및 축척 효과에 관한 연구)

  • Lee, Jonghyeon;Park, Dong-Woo
    • Journal of the Korean Society of Marine Environment & Safety
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    • v.27 no.4
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    • pp.538-549
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    • 2021
  • In this study, a trim tab on the stern hull of a small high-speed vessel of approximately 10 m length sailing at a Froude number of 1.0 was designed for energy efficiency. The running attitude and resistance performance of the bare hull and trim tab hull at several angles to the base line were analyzed for model and full scale ships using computational fluid dynamics, and compared to investigate the scale effect. The analysis results for the bare hull were quite similar, but a difference in the attitude control under same conditions of the trim tab was observed, resulting in the total resistance error. However, there was no significant difference in tendency of the variation in the resistance with the attitude. Thus, the optimum running attitude could be determined from the tendency despite the scale effect, but a full scale analysis is required to analyze the control of the attitude by the trim tab and flow characteristics near the full scale ship.

Resistance and Seakeeping Tests of a LOA 47.7m Class Catamaran (LOA 47.7m급 쌍동선의 저항 및 내항 시험)

  • H.H. Chun;Y.K. Chung;S.S. Chung;R.H. Chang;S.W. Ha;J.M. Kim
    • Journal of the Society of Naval Architects of Korea
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    • v.36 no.4
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    • pp.56-63
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    • 1999
  • The seakeeping and resistance tests of a 47.7m class catamaran are conducted in a towing tank with the 1/21.5 scale model. The effect of the trim tab on the resistance is investigated with the trim tab angle variations and the resistance and trim angle of the catamaran with the trim tab are compared with those without the trim tab. The heave and pitch motions are measured at the three full scale speeds in sea state of 3.4 and 5 and the vertical accelerations at five points on the deck are also measured. The measured accelerations are compared with the criteria of ISO 2631/3 and it is shown that the seakeeping performance of the catamaran is good.

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Study on the Optimal Selection of Rotor Track and Balance Parameters using Non-linear Response Models and Genetic Algorithm (로터 트랙 발란스(RTB) 파라미터 최적화를 위한 비선형 모델링 및 GA 기법 적용 연구)

  • Lee, Seong Han;Kim, Chang Joo;Jung, Sung Nam;Yu, Young Hyun;Kim, Oe Cheul
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.44 no.11
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    • pp.989-996
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    • 2016
  • This paper intends to develop the rotor track and balance (RTB) algorithm using the nonlinear RTB models and a real-coded hybrid genetic algorithm. The RTB response data computed using the trim solutions with variation of the adjustment parameters have been used to build nonlinear RTB models based on the quadratic interpolation functions. Nonlinear programming problems to minimize the track deviations and the airframe vibration responses have been formulated to find optimum settings of balance weights, trim-tab deflections, and pitch-link lengths of each blade. The results are efficiently resolved using the real-coded genetic algorithm hybridized with the particle swarm optimization techniques for convergence acceleration. The nonlinear RTB models and the optimized RTB parameters have been compared with those computed using the linear models to validate the proposed techniques. The results showed that the nonlinear models lead to more accurate models and reduced RTB responses than the linear counterpart.