• Title/Summary/Keyword: 비대칭 쌍동선

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비대칭 고속 쌍동선의 선미터널 입구영역 경사각 변화에 따른 유체역학적 특성 연구

  • Park, Geun-Hong;Lee, Gyeong-U;Seo, Gwang-Cheol;Kim, Sang-Won
    • Proceedings of the Korean Institute of Navigation and Port Research Conference
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    • 2018.11a
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    • pp.218-219
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    • 2018
  • 쌍동선형은 단동선형에 비해 안정성 및 저항성능이 우수하며 그 형상은 일반적으로 대칭 및 비대칭으로 구분한다. 이러한 쌍동선은 고속으로 운항하는 경우 선체사이의 파랑 중첩현상을 줄이기 위해 주로 비대칭선형을 사용한다. 또한, 중소형선박은 선미터널을 적용하여 추력효율을 향상시킨다. 본 연구에서는 비대칭 고속 쌍동선의 선미터널 입구영역의 경사각 변화에 따른 유체역학적 특성(저항성능, 항주자세, 압력분포)에 대한 수치해석 연구를 수행하였다. 수치해석은 상용프로그램 STAR CCM+를 이용하였다.

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Wave-resistance Performance Analysis of the Twin Hull for a Type of the Asymmetric and Symmetric Mono Hull (비대칭과 대칭 단동선형을 가진 쌍동선의 조파저항성능 분석)

  • Choi, Hee-Jong;Park, Dong-Woo
    • Journal of the Korean Society of Marine Environment & Safety
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    • v.19 no.1
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    • pp.78-84
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    • 2013
  • The primary objective of the current work is to develop efficient numerical code to assess the resistance performance of the twin hull form. Resistance performance for the two different twin hull forms with asymmetric and symmetric mono hull using developed code are evaluated. Numerical calculations and model tests have been compared to validate a developed code used in the current work. Comparison were carried out through sinkages of the bow and stern, trim angle and wave-making resistance. Comparative analysis regarding hydrodynamic characteristic of different twin hull forms is worthy of application in the hull form development stage.

The Comparison on Resistance Performance and Running Attitude of Asymmetric Catamaran Changing Angle of Inclination of Tunnel Stern Exit Region (비대칭 고속 쌍동선의 선미터널 출구영역의 경사각 변화에 따른 저항성능 및 항주자세 분석)

  • Kim, Sang-Won;Seo, Kwang-Cheol;Cho, Dea-Hwan;Kim, Byung-Jae;Lee, Gyeong-Woo
    • Proceedings of the Korean Institute of Navigation and Port Research Conference
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    • 2017.11a
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    • pp.232-233
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    • 2017
  • In this research, tunnel stern was applied on the asymmetric high-speed catamaran to evaluate vessel's hydrodynamic performance by numerical method, and the tunnel stern types are distinguished by angle of inclination of tunnel exit region into 3cases ($0^{\circ}$, $3^{\circ}$ and $6^{\circ}$). Consequently, it is confirmed that the total resistances of tunnel stern which have $0^{\circ}$ of inclination are lower about 4.8-17.9% than the bare hull in the wide speed range, but those of $3^{\circ}$ and $6^{\circ}$ of inclination tunnel stern are higher than bare hull about 5-14% and 5-29%, respectively. On the other hand, trim angles of $0^{\circ}$ of inclination tunnel stern show similar trend with those of bare hull in whole ranges of FnV but those of $3^{\circ}$ and $6^{\circ}$ of inclination tunnel stern are stabilized and declined respectively after FnV=1.54. These phenomena indicated that increasing angle of inclination of tunnel exit region had negative influence on resistance performance, however, it could make vessel's operation performance better than bare hull.

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A Study on the Self-Propulsion CFD Analysis for a Catamaran with Asymmetrical Inside and Outside Hull Form (안팎 형상이 비대칭인 쌍동선의 자항성능 CFD 해석에 관한 연구)

  • Jonghyeon Lee;Dong-Woo Park
    • Journal of the Korean Society of Marine Environment & Safety
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    • v.30 no.1
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    • pp.108-117
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    • 2024
  • In this study, simulations based on computational fluid dynamics were performed for self-propulsion performance prediction of a catamaran that has asymmetrical inside and outside hull form and numerous knuckle lines. In the simulations, the Moving Reference Frame (MRF) or Sliding Mesh (SDM) techniques were used, and the rotation angle of the propeller per time step was different to identify the difference using the analysis technique and condition. The propeller rotation angle used in the MRF technique was 1˚ and those used in the SDM technique were 1˚, 5˚, or 10˚. The torque of the propeller was similar in both the techniques; however, the thrust and resistance of the hull were computed lower when the SDM technique was applied than when the MRF technique was applied, and higher as the rotation angle of the propeller per time step in the SDM technique was smaller in the simulations for several revolutions of the propeller to estimate the self-propulsion condition. The revolutions, thrust, and torque of the propeller in the self-propulsion condition obtained using linear interpolation and the delivered power, wake fraction, thrust deduction factor, and revolutions of the propeller obtained using the full-scale prediction method showed the same trend for both the techniques; however, most of the self-propulsion efficiency showed the opposite trend for these techniques. The accuracy of the propeller wake was low in the simulations when the MRF technique was applied, and slight difference existed in the expression of the wake according to the rotation angle of the propeller per time step when the SDM technique was applied.