• 한국항해항만학회지
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• 제33권9호
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• pp.629-634
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• 2009

Vessels stability problems need to resolve the nonlinear mathematical models of rolling motion. For nonlinear systems subjected to random excitations, there are very few special cases can obtain the exact solutions. In this paper, the specific differential equations of rolling motion for intact ship considering the restoring and damping moment have researched firstly. Then the partial stochastic linearization method is applied to study the response statistics of nonlinear ship rolling motion in beam seas. The ship rolling nonlinear stochastic differential equation is then solved approximately by keeping the equivalent damping coefficient as a parameter and nonlinear response of the ship is determined in the frequency domain by a linear analysis method finally.

• 수산해양교육연구
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• 제29권2호
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• pp.415-421
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• 2017

This study is aiming to find one of working conditions for loading and unloading a large ship at game port. Firstly, for dynamic analysis of the moored ships, the motion characteristics of ship according to loading condition are figured out. The motion characteristics of ship is related to environmental factors such as current, wind, mooring line, fender and etc. As a result, it is ascertained through numerical simulation using the AQUA MARINE developed by ANSYS INC. This study might contribute to make a new method of mooring stability of target ship.

• 한국군사과학기술학회지
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• 제5권2호
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• pp.37-49
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• 2002

In this paper, flyout stability of missile that is launched in inclined launcher using sabots is analyzed. To include missile bending motion during flyout, FEA model of missile is converted into eight concentrated mass and equivalent stiffness matrix. Six d.o.f ship motion that have influence on flyout stability is modeled and missile firing time is modeled as probability variable to take arbitrary ship attitude into account. Gap between missile and sabot is modeled as normal distribution probability variable and Monte Carlo simulation is performed. As results, the coriolis acceleration effects by ship motion are analyed and statistical results of missile pitch rate are shown.

• 한국항해항만학회:학술대회논문집
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• 한국항해항만학회 2009년도 추계학술대회
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• pp.239-240
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• 2009

Vessels stability problems need to resolve the nonlinear mathematical models of rolling motion. For nonlinear systems subjected to random excitations, there are very few special cases can obtain the exact solutions. In this paper, the specific differential equations of rolling motion for intact ship considering the restoring and damping moment have researched firstly. Then the partial stochastic linearization method is applied to study the response statistics of nonlinear ship rolling motion in beam seas. The ship rolling nonlinear stochastic differential equation is then solved approximately by keeping the equivalent damping coefficient as a parameter and nonlinear response of the ship is determined in the frequency domain by a linear analysis method finally.

• 한국항해학회지
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• 제3권1호
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• pp.1-17
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• 1979

It is very important for both naval architects and ship's officers to know the maneuvering characteristics of their ships. As the abilities of a rudder which controlls a ship can be determined clearly by analyzing the results of Kempf's zig-zag maneuver and directional stability of a ship also known by Dieudonn spiral maneuver, the importance of turning test which takes much time is recently apt to be neglected. But because the test can be executed comparatively more simply than any other maneuvering tests, it gives some informations on the directional stability, and turning characteristics may be expressed simply by the results of the test, it is still often performed. In this paper several assumptions are made to simplify the turning motion of a ship. The equations of initial transient phase, the radius ofsteady turning circle, and the center of the steady turning point are derived by using the hydrodynamic derivatives. And then the approximate method of drawing the turning circle geometrically is suggested.

• 한국정밀공학회지
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• 제15권9호
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• pp.33-42
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• 1998

If a ship diesel engine is operated by consolidated control with Controllable Pitch Propeller(CPP), the minimum fuel consumption is achieved together with the demanded ship speed. For this, it is necessary that the ship is operated on the ideal operating line which satisfies the minimum fuel consumption and that the pitch angle of CPP and throtle valve angle are controlled simultaneously. In this point of view, this paper presents a controller design method for a ship propulsion system with CPP based on the decoupling control theory. To do this, Linear Matrix Inequality(LMI) approach is introduced for the control system to satisfy the given $H_\infty$ control performance and robust stability in the presence of physical parameter perturbations. The validity and applicability of this approach are illustrated by simulation in the all operating ranges.

• 대한조선학회논문집
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• 제49권1호
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• pp.52-59
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• 2012

Among many factors to be considered for higher safety level requirements, the hull stability in intact and damaged conditions in seaways is of utmost importance. Since the assessment of a damaged ship is complicated due to the highly non-linear behavior, it is widely acknowledged that computational fluid dynamics (CFD) methods are one of the most feasible approaches. Although many research activities are being reported on the damaged ship stability recently, most of them are not designed for validation of CFD studies. In this study, well-designed model tests were performed to build a CFD validation database, which is essential in developing better CFD methods for the damage stability assessment. The geometry of the damaged compartment and test conditions were determined based on preliminary CFD simulations. Free roll decay tests in calm water with both intact and damaged ships were performed and the roll motion characteristics were compared. The damaged ship showed a larger roll damping coefficient and more rapid decrease of roll amplitude than the intact ship. The primary reason of these efforts can be explained by the movement of the flooded water.

• 한국항해학회지
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• 제25권1호
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• pp.1-9
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• 2001

1993년 IMO가 채택한 조종성 잠정기준에서 요구되는 4가지 항목 중, 특히 비대 선박의 경우, 침로 안정성이 문제시될 수 있다는 것은 잘 알려진 사실이다. 본 연구에서는 비대 선박의 조종운동시 타의 크기에 따른 선미 유동 특성을 조사하기 위해서 회류수조에서 사항상태의 조건 하에 두 종류의 모형실험을 수행하였다. 즉, 첫번째 실험은 타에 유입하는 흐름의 정류효과 측정에 대한 것이고, 두번째 실험은 타 상부와 선미오버행 하부 공간 주위의 흐름가시화에 대한 것이다. 실험결과, 타의 크기에 따른 선미 유동 특성과 타에 유입하는 흐름의 정류효과의 상관관계를 규명하였고, 타 상부와 선미오버행 하부의 공간은 침로 안정성에 있어서 중요한 역할을 한다는 것을 알 수 있었으며, 특히 타 상부와 선미오버행 하부의 공간이 작을수록 침로 안정성이 저하될 가능성이 높다는 것을 확인하였다.

• 한국수산과학회지
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• 제18권2호
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• pp.94-100
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• 1985

부산수산대학 실습선 부산403호의 내부개조 및 중량물의 철거로 인한 복원성의 변화를 측정하기 위하여 경사시험을 실시하고, 개조전과 시험시의 GM, K, GA의 값을 비교하였으며, 또한 어선 설비 등에 관한 규칙 및 IMO 규정에 비추어 복원성능을 검토하였다. 1. 경하 및 만재출항상태에서의 GZ값은 각각 0.307m 및 0.325 m 여서 복원성에는 이상이 없는 것으로 판단된다. 2. 경하상태에서는 개조전보다 GM이 0.046m 작고, KG 0.141 m 크나, 복원성에는 지장이 없는것으로 보아진다. 3. 만재출항상태에서 탱크 내 액체의 자유표면의 유동을 고려하지 않을 때는 개조전보다 GM이 0.163 m 작고 KG가 0.173 m 크나 복원성에는 지장이 없는 것으로 간주된다. 그러나 탱크 내 액체의 자유표면의 유동을 고려하면 GM 0.275m는, 어선 설비 등에 관한 규칙에서 산정한 GM의 기준치인 0.353m에 미치지 못하므로 이에 대한 보완이 필요하다고 본다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2007년도 춘계학술대회B
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• pp.3080-3085
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• 2007

Shape optimization of the 3-dimensional WIG airfoil with 3.0-aspect ratio has been performed by using the multi-objective genetic algorithm. The WIG ship effectively floating above the surface by the ram effect and the virtual additional aspect ratio by a ground is one of next-generation and cost-effective transportations. Unlike the airplane flying out of the ground effect, a WIG ship has possibility to capsize because of unsatisfying the static stability. The WIG ship should satisfy aerodynamic properties as well as a static stability. They tend to strong contradict and it is difficult to satisfy aerodynamic properties and static stability simultaneously. It is inevitable that lift force has to scarify to obtain a static stability. Multi-objective optimization technique that the individual objectives are considered separately instead of weighting can overcome the conflict. Due to handling individual objectives, the optimum cannot be unique but a set of nondominated potential solutions: pareto optimum. There are three objectives; lift coefficient, lift-to-drag ratio and static stability. After a few evolutions, the non-dominated pareto individuals can be obtained. Pareto sets are all the set of possible and excellent solution across the design space. At any selections of the pareto set, these are no better solutions in all design space