• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2003년도 The Fifth Asian Computational Fluid Dynamics Conference
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• pp.291-293
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• 2003

This paper deals with a thrust generation of flapping-airfoil by dynamic stall. From many other previous research results, phase angle $ between pitching and plunging mode of flapping motion must be 90 deg. to satisfy maximum propulsive efficiency. In this case, leading edge vortex is relatively small. This phenomenon is related dynamic stall. So preventing leading edge vortex induced by dynamic stall guarantees maximum propulsive efficiency. But, in this paper we insist the leading edge vortex yields quite a positive influence on thrust generation and propulsive efficiency. In order to certify our opinion, pitching and plunging motions were calculated with the parameter of amplitude and frequency by using the unsteady, incompressible Navier-Stokes flow solver with a two-equation turbulence model. For more efficient computation, it is parallelized by MPI programming method.

• 대한조선학회지
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• 제27권3호
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• pp.89-99
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• 1990

선박의 운항경제성을 개선하기 위해서는 저항이 작고 추진성능은 우수한 선형의 개발이 요구된다. 흔히, 저저항 특성을 갖는 선미선형은 추진효율이 떨어지는 경우가 많고, 반대로 추진효율이 좋은 선형은 저항이 큰 경우가 많아서 결과적으로 소요마력이 작은 선형의 개발은 어려운 과제로 되어 있다. 비대선형에 있어서는 저항 특히, 점성저항이 작은 것으로 알려진 소위 'Buttock-flow type'의 선미형상을 기본으로 하고, 여기에 추진기 앞쪽(Run부)은 추진효율이 높은 재래 선미형상(U-type 또는 Hogner type)과 같이 만들어 저저항 및 고추진효율의 특성을 함께 갖는 선미선형의 개발을 시도하였다. 최초의 모형시험 결과는 이와같은 시도가 선미선형 설계의 한 접근 방법이 될 수 있음을 보여주었으며, 첫 시험결과에 고무되어 계속적으로 이러한 선미선형의 개량에 주력한 결과로, 저저항 고추진 효율을 갖는 선미선형의 개발에 어느정도 성공을 거두었다. 더하여, 이러한 선형은 추진기 주변의 반류분포가 균일하여 우수한 캐비테이션 및 진동 특성도 함께 가질 수 있고, 종래의 '바-지 선형'에 비하여 기관실 이중저의 상면적(床面積)이 넓어, 보다 경제적인 배치가 가능하다는 것도 확인되었다.

• 한국전산유체공학회지
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• 제8권2호
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• pp.24-32
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• 2003

In this work, we propose a new idea of flapping airfoil design for optimal aerodynamic performance from detailed computational investigations of flow physics. Generally, flapping motion which is combined with pitching and plunging motion of airfoil, leads to complex flow features such as leading edge separation and vortex street. As it is well known, the mechanism of thrust generation of flapping airfoil is based on inverse Karman-vortex street. This vortex street induces jet-like flow field at the rear region of trailing edge and then generates thrust. The leading edge separation vortex can also play an important role with its aerodynamic performances. The flapping airfoil introduces an alternative propulsive way instead of the current inefficient propulsive system such as a propeller in the low Reynolds number flow. Thrust coefficient and propulsive efficiency are the two major parameters in the design of flapping airfoil as propulsive system. Through numerous computations, we found the specific physical flow phenomenon which governed the aerodynamic characteristics in flapping airfoil. Based on this physical insight, we could come up with a new kind of airfoil of tadpole-shaped and more enhanced aerodynamic performance.

• 수산해양기술연구
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• 제41권3호
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• pp.227-233
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• 2005

In order to estimate the effective horse power(EHP) in towing net of a bottom trawl ship, the ship's resistance was calculated by using a series data of Yamagata and Wigley formula. Also the effective horse power for a ship(EHPs) was estimated versus the ship speed in sailing and the propulsive efficiency was calculated with the brake horse power and the effective horse power. Then the effective horse power for a ship and a trawl net were estimated in the application of the propulsive efficiency in towing net. The total effective horse power($EHP_T$) was average 187.6kW and the effective horse power for a 1.awl net($EHP_n$) was average 176.7kW at a smooth sea state in towing net. The ratio of $EHP_n$ to $EHP_T$ was about 94.0% and the value was higher slightly than was already informed at a smooth sea state. The power for keeping up a townet speed was required more about 20% of a maximum continuous power at a rather rough sea state than a smooth sea state. In the future, if the residual resistance is considered with a sea state, $EHP_n$ will be estimated more correctly Also the data of EHP estimated by this method will be used as the basic data to design a trawl net.

• 한국항공우주학회지
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• 제34권1호
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• pp.32-41
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• 2006

본 논문에서는 직렬 배치된 익형이 동시에 플래핑 운동을 할 때의 추력 생성 과정과 유동특성에 대한 연구를 수행하였다. 이를 위해 익형의 운동 주파수, 진폭 및 전후방 익형 간의 상대거리 등에 대한 계산을 체계적으로 실시하여 다음과 같은 사실을 확인할 수 있었다. 먼저, 위상차 없이 전후방 익형이 동시에 병진운동을 할 경우 대부분의 주파수와 진폭 영역에서 후방익형의 추력과 추진효율이 최대화됨을 알 수 있었다. 플래핑 진폭이 0.2 코드, 무차원주파수가 0.75일 경우, 후방익형의 추진효율이 전방익형보다 37% 이상 개선되는 것으로 계산되었다. 단, 익형의 운동 진폭과 주파수가 임계치를 초과할 경우 전방익형의 뒷전와류에 의해 후방익형의 앞전와류의 강도가 강화되면서 전체적인 추력과 효율이 저하될 수 있다. 둘째, 전후방익형이 180도의 위상차를 갖고 운동을 할 경우에는 전방익형의 후류와 후방익형이 서로 반대방향으로 상호작용을 함으로써 결과적으로 공력특성이 악화되는 것을 알 수 있었다. 셋째, 후방익형의 배치 위치에 따른 특성은 수평방향으로는 두 익형사이의 거리가 멀어질수록 추력과 효율이 동시에 떨어지며, 수직방향 위치변화에 따른 차이는 크지 않은 것으로 나타났다.

• Journal of Advanced Marine Engineering and Technology
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• 제33권1호
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• pp.52-61
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• 2009

This experiment was conducted in attempt of improving hydrodynamic efficiency of the propulsion mechanism by installing a spring to the wing so that the opening angle of the wing in one stroke can be changed automatically, compared to the existing method of fixed maximum opening angle in Weis-Fogh type ship propulsion mechanism. Average thrust coefficient was almost fixed with all velocity ratio with the prototype, but with the spring type, thrust coefficient increased sharply as velocity ratio increased. Average propulsive efficiency was larger with bigger opening angle in the prototype, but in the spring type, the one with smaller spring coefficient had larger value. In the range over 1.0 in velocity ratio where big thrust can be generated, spring type had more than twice of propulsive efficiency increase compared to the prototype.

• Journal of Ship and Ocean Technology
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• 제8권1호
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• pp.31-41
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• 2004

A ducted marine propulsor has been widely used for the thruster of underwater vehicles for protecting collision damage, increasing propulsive efficiency, and reducing cavitation. Since a single-stage ducted propulsor contains a set of rotor and stator inside an annular duct, the numerical analysis becomes extremely complex and computationally expensive. However, the accurate prediction of viscous flow past a ducted marine propulsor is essential for determining hydrodynamic forces and the propulsive performances. To analyze a ducted propulsor having rotor-stator Interaction, the present work has solved 3D incompressible RANS equations on the sliding multiblocked grid. The flow of a single stage turbine flow was simulated for code validation and time averaged pressure coefficients were compared with experiments. Good agreement was obtained. The hydrodynamic performance coefficients were also computed.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2009년 추계학술대회논문집
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• pp.159-163
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• 2009

In this paper, the fluid dynamic forces and performances of a moving airfoil in the low Reynolds number flow is addressed. In order to calculate the necessary propulsive force for the moving airfoil in a low Reynolds number flow, a lattice-Boltzmann method is used. The critical Reynolds and Strouhal numbers for the thrust generation are investigated for the four propulsion types. It was found that the Normal P&D type produces the largest thrust with highest efficiency among the investigated types. The leading edge of the airfoil has an effect of deciding the force production types, whereas the trailing edge of the airfoil plays an important role in augmenting or reducing the instability produced by the leading edge oscillation. It is believed that present results can be used to decide the optimal propulsion devices for the given Reynolds number flow.

• Journal of Advanced Marine Engineering and Technology
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• 제39권1호
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• pp.1-7
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• 2015

최근에 CO2 배출에 대한 환경 규제가 마련되었고, 연료유 가격은 계속해서 상승하고 있다. 이런 상황들을 극복하기 위해 연료소모량을 감소시키고 추진효율을 개선한 에너지 저감 추진장치들이 계속해서 개발되고 있다. 본 논문에는 핸디형 산적화물선에 적용한 PBCF, SCHNEEKLUTH duct, 비대칭 러더 벌브, Mewis duct의 성능 실험을 서술하였다. 그 결과, SCHNEEKLUTH duct가 다른 에너지 저감 장치들에 비해 연료소모량 절감과 추진효율의 향상 측면에서 더 효과적이었다. 또한 SCHNEEKLUTH duct가 거주구 진동에도 효과가 있음을 확인하였다. 그리고 연료소모량은 주기관 de-rating을 통해서도 절감할 수 있었다.

• Journal of Advanced Marine Engineering and Technology
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• 제29권2호
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• pp.161-167
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• 2005

The improvements of the propulsive engine efficiencies could reduce the fuel consumption. Therefore. for a marine main diesel engine the substantial increase of stroke bore ratio. so that the engine speed can be significantly reduced in order to increase the Propulsive efficiency. As a typical example. a Sulzer RTA 60C engine has acylinder diameter of 600 mm and each cylinder is capable of delivering 2.369 kW in the speed range 91-114 rpm. In order to Provide basic data for thermal system of marine engine. this work performs an experimental study of heat transfer in a square channel with one rib-roughened wall under sin91e mode of reciprocating oscillation. A selection of heat transfer measurements illustrates the manner by which the reciprocating channel with two opposite heating walls has the higher heat transfer Performance than with four heating wall.