• 대한조선학회지
• /
• 제21권3호
• /
• pp.27-34
• /
• 1984

When a ship is travelling in following seas, the encounter frequency is reduced to be very low. In that case broaching phenomenon is most likely to occur, and it may be due to wave exciting forces acting on ships. It is thought that the wave exciting forces acting on ships in following seas almost consist of two components. One is hydrostatic force due to Froude-Krylov hypothesis, and the other is hydrodynamic lift force due to orbital motion of water particles below the wave surface. In the present paper, the emphasis is laid upon wave exciting sway force, yaw moment and roll moment acting on ships in following seas. The authers take the case that the component of ship speed in the direction of wave propagation is equal to the wave celerity, i.e., the encounter frequency is zero. Hydrostatic force components are calculated by line integral method on Lewis form plane, and hydrodynamic lift components are calculated by lifting surface theory. Furthermore captive model tests are carried out in regular following waves generated by means of a wave making board. Through the comparison between calculated and measured values, it is confirmed that the wave exciting forces acting on ships in following seas can be predicted in terms of present method to a certain extent.

• 해양환경안전학회지
• /
• 제24권4호
• /
• pp.430-437
• /
• 2018

파랑중을 항행하는 선박에는 저항증가와 함께 파랑에 의한 횡력 및 회두모멘트가 정수중과 다르게 작용하여 선박의 조종성능에 영향을 미치게 된다. 따라서 파랑에 의해 발생하는 횡력 및 회두모멘트를 추정하는 것이 중요하므로 본 연구에서는 이와 같은 문제를 해결할 수 있는 수치계산을 이행하였다. 본 연구에서는 CFD를 이용하여 정수중 및 파랑중에서 부선에 작용하는 유체력 계산을 위한 수치시뮬레이션을 수행하였으며, 이 결과를 토대로 최종적으로 파랑중 부선의 침로안정성 특성에 대하여 조사 및 분석하였다. 정수중보다는 파랑중에서 부선에 작용하는 유체력이 강해지고 있으며, 파랑중에서도 파장이 길어질수록 유체력이 커지고 있는 모습을 확인할 수 있다. 장파장 영역에서는 yaw damping lever의 (-) 값이 정수중보다 커지고 있으나, 단파장 영역과 파장이 선박길이와 일치하는 영역에서는 각각 작아지고 있어서 이 영역에서는 침로안정성이 향상되고 있다고 추정할 수 있다. 즉 장파장 영역에서는 침로안정성이 정수중 및 단파장 영역보다 상대적으로 나빠지고 있으므로 항행시 주의가 필요하다고 할 수 있다.

• 해양환경안전학회지
• /
• 제15권1호
• /
• pp.57-62
• /
• 2009

예부선 운항 시 부두의 접안, 이안 및 좁은 수로를 항행할 경우 접할 수 있는 안벽 근처의 항행과, 두 선박이 접근하여 평행 항로상을 반대 방향으로 항과할 경우의 유체력 상호작용을 살펴보기 위하여, 예선의 부선 예항 시뮬레이션을 실시한 후 부선의 선수방향, 예선의 회두 모멘트와 횡방향의 힘과 같은 특성을 조사 및 분석하여 그에 따른 안전한 예부선의 조선 방안을 제시하였다. 그 결과 부선의 과도한 회두운동을 감소시키기 위해서는 예선의 속도가 너무 느리지 않도록 미속상태의 속도를 유지하고, 예인삭의 길이를 가능한 한 부선의 길이만큼 줄여 항행하는 것이 안전예항 업무에 도움이 될 것으로 판단된다.

• 수산해양기술연구
• /
• 제38권3호
• /
• pp.234-240
• /
• 2002

본 연구에서는 전개판의 영각 변화에 따른 정적안정성에 관하여 이론적 해석을 하였다. 또한 전개판의 형상별 유체력에 의한 정적 안정성을 평가하기 위하여 종횡비가 다른 평판과 만곡도가 다른 종만곡판을 사용하여 회류수조에서 유체력 및 모벤트를 측정하고 형상별 압력중섬계수와 모멘트 계수를 계산하였다. 본 연구에서 얻어진 결과를 요약하면 다음과 같다. 1. 전개판의 영각($\alpha$) 변화에 따른 끌줄의 장력과 후릿줄의 장력에 의한 모멘트 변화는 전개판을 항상 정적 안정성을 가지도록 작용한다. 2. 종횡비(λ)가 0.5, 1.0, 1.5인 평판의 압력중심계 수는 영각의 증가와 함께 전연에서 중심쪽으로 이동한다. 이것은 유체력에 의한 모멘트는 항상 정적으로 안정하도록 작용한다는 것을 의미한다. 3. 종횡비가 일정(λ=1.5)하고, 만곡도(CR)가 5%, 10%, 15%, 20%인 만곡판의 유체력에 의한 압력중심계수는 영각의 증가와 함께 후연에서 전연쪽으로 이동한 다음, 다시 만곡판의 중심쪽으로 이동한다 만곡판에 작용하는 유체력에 의한 모멘트는 만곡도가 커질수록 정적으로 불안정한 영각의 범위가 증가한다.

• 대한조선학회논문집
• /
• 제61권1호
• /
• pp.29-43
• /
• 2024

The present study concerns a feasibility study for applying principal component analysis to ship dynamics in maneuver. Using the four degrees of freedom standard modular model for ship dynamics maneuver simulations of large angle zigzag tests with rudder deflection angle variations are conducted. The datasets of ship motion, hydrodynamic force, and moment during the maneuver are acquired to identify the principal modes. The covariance matrix of obtained ship dynamics variables shows a strong linear correlation between the motion, hydrodynamic force, and moment, except the surge force. Four eigenvectors of the covariance matrix are selected as the principal modes of ship dynamics. Using the principal modes, ship motion in turning circle and zigzag tests is reconstructed, showing good agreement with the original data.

• 한국해양공학회지
• /
• 제34권4호
• /
• pp.237-244
• /
• 2020

In this study, we investigate surge force, heave force, and pitch moment, which are vertical plane hydrodynamics acting on Manta-type unmanned underwater vehicles (UUVs), using a model test and computational fluid dynamics (CFD) simulation. Assessing the maneuvering hydrodynamic characteristic of an underwater glider in the initial design stage is crucial. Although a model test is the best approach for obtaining the maneuvering hydrodynamic derivatives for underwater vehicles, numerical methods, such as Reynolds averaged Navier-Stokes (RANS) equations, have been used owing to their efficiency in terms of time and cost. Therefore, we conducted an RANS-based CFD calculation and a model test for Manta-type UUVs. In addition, we conducted a validation study through a comparison with a model test conducted at a circular water channel (CWC) in Korea Maritime & Ocean University Furthermore, two RANS solvers (Star-CCM+ and OpenFOAM) were used and compared. Finally, the maneuvering hydrodynamic forces obtained from the static drift and resistance tests for a Manta-type UUV were presented.

• 대한조선학회지
• /
• 제14권3호
• /
• pp.13-22
• /
• 1977

The hydrodynamic forces acting on a forced oscillating 2-dimensional cylinder on a free surface of a fluid of a finite depth are calculated by distributing singularities on the immersed body surface. And the Haskind-Newman relation in a fluid of a finite depth is derived. The wave exciting force of the cylinder to an oscillation is also calculated by using the above relation. The method is applied to a circular cylinder swaying in a water of finite depth, and then, to a rectangular cylinder heaving, swaying, and rolling. The results of above cases give a good agreement with those by earlier investigators such as Bai, Keil, and Yeung. Also, this method is applied to a Lewis form cylinder with a half beam-to-draft ratio of 1.0 and a sectional area coefficient of 0.941, and to a bulbous section cylinder which is hard to represent by a mapping function. The results reveal that the hydrodynamic forces in heave increase as the depth of a water decrease, but in sway or roll, the tendency of the hydrodynamic forces is difficult to say in a few words. The exciting force to heave for a bulbous section cylinder becomes zero at two frequencies. The added mass moment of inertia for roll is seemed to mainly depend on the sectional shape than the water depth.

• 대한조선학회논문집
• /
• 제59권5호
• /
• pp.288-295
• /
• 2022

In this study, the force and moment acting on a Joubert BB2 submarine model at depths near the free surface were measured through a captive model test with the scale ratio of 1/15. Based on the experiment, the pitch moment and heave force due to the "Tail suction effect", including the change in surge force with depth near the free surface, were quantitatively analyzed. The change of force and moment according to the relative position of the sail and the free surface was reviewed with the free surface waves generated for each depths. As a result, the angle of attack of the hull to counteract the pitch moment induced by the tail suction effect was derived. The effect of the hydrostatic moment component according to the angle of attack on the equilibrium of pitch moment was also taken into account. The control plane performance tests for the X-type rudder and sail plane were conducted in snorkel and surface depth conditions to figure out the control plane angles for the neutral level flight of the submarine at near free surface. The results of this study are expected to be used as a reference data for the neutral level flight of the submarine at near free surface operation in the free running model test as well as numerical studies.

• 한국군사과학기술학회지
• /
• 제19권2호
• /
• pp.227-235
• /
• 2016

Heavy-weight high speed underwater vehicle(HSUV) is launched from the submerged mother ship. For the safety point of view, it is important to confirm whether the HSUV would touch the launching mother ship. In this paper, the hydrodynamic force and moment were modeled by the polynomials of motion variables and the simple lift and drag acting on a plate and cylinder which consist of the HSUV's several parts. The mother ship was assumed as the Rankine half body to consider the flow field near the moving ship. Such hydrodynamic force and moment were included in the 6 DOF equations of motion of the HSUV and the dynamic simulations for the various conditions of the HSUV until the propeller activation were performed. Developed simulation program is expected to reduce the number of expensive sea trial test to develop safety logic of the HSUV at the initial firing stage.

• 한국소음진동공학회논문집
• /
• 제12권9호
• /
• pp.717-724
• /
• 2002

In this study, a numerical analysis for the piston secondary dynamics of small refrigeration reciprocating compressors is performed. In general, the length of cylinder in this class of compressors is shortened to diminish the frictional losses of the piston-cylinder system. So, the contacting length between piston and cylinder wall is in variable with the rotating crank angle around the BDC of the reciprocating piston. In the problem formulation of the piston dynamics, the change in bearing length of the piston and all corresponding forces and moments are considered in order to determine the piston trajectory, velocity and acceleration at each step. A Newton-Raphson procedure was employed in solving the secondary dynamic equations of the piston. The developed computer program can be used to calculate the entire piston trajectory and the hydrodynamic force and moment as functions of crank angle under compressor running conditions. The results explored the effects of the radial clearance, lubricant viscosity, length of the cylinder wall, and pin location on the stability of the piston.