• 대한기계학회:학술대회논문집
• /
• 대한기계학회 2002년도 학술대회지
• /
• pp.173-176
• /
• 2002

The purpose of this study is to develop a tool for the analysis of the cavitating flow around trans-cavitating marine propellers. In this study, a linearized super-cavitation theory was applied in order to analyze the performance of the 2-dimensional foils. The numerical results correlated very well with experimental data. The trans-cavitating propellers, manufactured and tasted in KRISO, is selected to validate the lifting surface procedure. For a TCP with a Johnson's five term section, the comparison between the numerical prediction and experiments is fairly good and promising. The new lifting surface procedure, developed and validated with 2-D foils and a TCP, is generally considered applicable to the practical design of the trans-cavitating propeller with Johnson's five term section

• Journal of Ship and Ocean Technology
• /
• 제10권4호
• /
• pp.1-11
• /
• 2006

The finite volume based multi-block RANS code, WAVIS developed at MOERI is applied to the numerical self-propulsion test. WAVIS uses the cell-centered finite volume method for discretization of the governing equations. The realizable $k-{\epsilon}$ turbulence model with a wall function is employed for the turbulence closure. The free surface is captured with the two-phase level set method and body forces are used to model the effects of a propeller without resolving the detail blade flow. The propeller forces are obtained using an unsteady lifting surface method based on potential flow theory. The numerical procedure followed the self-propulsion model experiment based on the 1978 ITTC performance prediction method. The self-propulsion point is obtained iteratively through balancing the propeller thrust, the ship hull resistance and towing force that is correction for Reynolds number difference between the model and full scale. The unsteady lifting surface code is also iterated until the propeller induced velocity is converged in order to obtain the propeller force. The self-propulsion characteristics such as thrust deduction, wake fraction, propeller efficiency, and hull efficiency are compared with the experimental data of the practical container ship. The present paper shows that hybrid RANS and potential flow based numerical method is promising to predict the self-propulsion parameters of practical ships as a useful tool for the hull form and propeller design.

• 산업기술연구
• /
• 제5권
• /
• pp.51-57
• /
• 1985

The object of this study is in the development of the computer program to predict the performance of rotor in hovering by getting the aerodynamic load acting on blade. For this work the vortex theory was chosen among the aerodynamic theories, blade was replaced by planar vortex panels, and prescribed wake for the wake geometry was selected and then represented by vortex lattices. To get the aerodynamic load on blade, flow was assumed to be incompressible, irrotational and steady, and the surface boundary condition of inviscid flow was used as boundary condition. Then the relationships between this load and flight condition and blade geometry were examined.

• 대한조선학회논문집
• /
• 제49권6호
• /
• pp.528-533
• /
• 2012

Flexible composite propellers are subject to large deformation under heavy loading, and hence the hydrodynamic performance of deformed propeller might deviate from that of the metallic propeller under negligible deformation. To design the flexible propeller, it is therefore necessary to be able to evaluate the structural response of the blades to the hydrodynamic loadings, and then the influence of the blade deformation upon the hydrodynamic loadings. We use the lifting-surface-theory-based propeller analysis and design codes in solving the hydrodynamic problem, and the finite-element-method program formulated with 20-node iso-parametric solid elements for the analysis of the structural response. The two different hydrodynamic and structural programs are arranged to communicate through the carefully-designed interface scheme which leads to the derivation of the geometric parameters such as the pitch, the rake and the skew distributions common to both programs. The design of flexible propellers, suitable for manufacturing, is shown to perform the required thrust performance when deformed in operation. Sample design shows the fast iteration scheme and the robustness of the design procedure of the flexible propellers.

• 대한조선학회지
• /
• 제26권4호
• /
• pp.27-34
• /
• 1989

부분 캐비티가 발생한 2차원 수중익 문제를 해결하기 위하여 포텐시얼을 기저로 한 양력판 이론이 정식화 되었다. 본 이론은 수중익 표면에 다이폴과 쏘오스를 분포함으로써 각각 양력 및 캐비티 문제를 표현하고 있다. 날개표면의 접수부에서의 운동학적 경계조건은 날개의 내부유동에서의 전체 포텐시얼이 영이 된다는 대등한 조건으로 만족되었다. 캐비티 표면에서의 역학적 경계조건은 압력이 일정하다는 즉 속도가 일정하다는 조건을 거쳐 포텐시얼이 선형적으로 변한다는 조건으로 대치되었으며, 운동학적 조건은 특이함수의 세기가 결정된 후에 적분에 의하여 캐비티의 형상을 구하는데에 사용되었다. 따라서 Green 정리를 사용하면, 속도를 기저로 하는 통상적인 정식화가 아닌, 포텐시얼을 기저로 한 경계치 문제가 완성된다. 또한 수중익의 정확한 표면에 특이함수를 분포함으로써, 날개두께가 영인 수중익 신경 이론에 비하여, 날개표면에서의 압력분포의 정도를(특히 날개 앞날부근에서) 향상시켰다. 본 이론에서는 캐비티 길이를 가정하고 이에 대응하는 캐비티의 모양과 캐비테이션수를 계산하였다. 계산정도의 향상을 위하여 약 5회정도의 반복계산이 필요하지만 공학적 목적을 위해서는 2회의 반복계산이 충분함을 보였다.

• 동력기계공학회지
• /
• 제16권5호
• /
• pp.40-46
• /
• 2012

본 연구에서는 자유표면 유동문제를 효율적으로 계산하기 위한 방법으로서, 수치 파수조를 구현하여 잠수체에 의한 조파현상을 시간영역에서 다룰 수 있는 수치해법에 대하여 소개하였다. 그리고 이를 이용하여 수행된 연구내용들을 검토하고 양력물체의 경우를 포함하기 위하여 개선된 수학적 정식화 및 수치해법의 개요를 다루었다. 임의의 운동을 하는 양력물체에 의한 조파현상을 전산기로 구현하는 수치 파수조는 과중한 계산시간이 문제가 되는데, 이는 수치 Kutta 조건의 구현과 양력표면 후방의 wake 영역을 계산에서 고려해야 하기 때문이다. 따라서 한층 더 수치계산의 효율성이 중요하다고 판단되므로, 본 연구에서 소개된 3차원 고차 스펙트럴/경계요소법(High-Order Spectral/Boundary Element Method)은 자유표면 요소수를 N이라 할 때 그 계산량이 NlogN에 비례(N이 클 때는 거의 선형적으로 비례)하여 증가하므로 기존의 방법들 보다 매우 효율적인 수치해법이라 할 수 있다. 향후, 본 연구의 타당성 검증을 위한 수치코드의 개선과 여러 가지 수치계산결과 비교 등의 노력이 더 필요하다고 생각된다.

• 대한조선학회지
• /
• 제27권4호
• /
• pp.15-26
• /
• 1990

본 연구는 표면 양력관 이론을 이용하여 초월 공동이 발생한 2차원 날개의 유동해석을 위한 제반 경계 조건을 검증하고 공동 뒷부분의 모형을 비교 검토한다. 해석해가 존재하는 2차원 대칭 스트럿 주위의 초월 공동 현상을 수치적으로 해석하여 그 결과를 해석해와 비교함으로써 표면 양력판 이론에 의한 프로펠러 공동 문제 해석의 가능성을 입증하였다. 특히, 공동 뒷부분의 비 선형 닫힘 모형, 타원형 닫힘 모형, 그리고 선형 닫힘 조건을 서로 비교 분석함으로써 공동 문제 해결에서 가장 중요한 공동 닫힘 조건의 영향을 보였다.

• Wind and Structures
• /
• 제32권1호
• /
• pp.1-9
• /
• 2021

Vortex generators are commonly used in mechanical engineering and the aerospace industry to suppress flow separation owing to their advantages of simple structure, economic viability, and high level of efficiency. Owing to the flow separation of the incoming wind on the leading edge, a suction area is formed on the roof surface, which results in a lifting effect on the roof. In this research, vortex generators were installed on the windward surface of a flat roof and used to disturb to roof flow field and reduced suction based on flow control theory. Computational fluid dynamics (CFD) simulations were performed in this study to investigate the effects of vortex generators on reduce suction. It was determined that when the vortex generator was installed on the top of the roof on the windward surface, it had a significant control effect on reduce suction on the roof leading edge. In addition, the influence of parameters such as size, placement interval, and placement position of the vortex generator on the control effect of the roof's suction is also discussed.

• 한국기계연구소 소보
• /
• 제4권2호
• /
• pp.49-63
• /
• 1982

In this paper, a classical gust problem is treated by using the numerical lifting¬-surface theory to verify the effect of gust-a sudden fluctuating fluid velocity around an object, which is normal to the main stream direction-on the hydrody¬namic forces, especially the mean thrust in upstream direction, acting on the two¬-dimensional flat plate. In this case, the mean thrust wholly resorts to the leading edge suction, and it is the same situation to the case of the heaving plate in uniform flow. The ph¬enomenon of leading edge suction is very important for the flapping propulsion of animals, typical to fish and birds, and can be related to the prediction of the hydrodynamic forces acting on marine propellers operating in gustlike wakes of ships. The results of this paper can be easily superposed to those of the reference [1J in order to solve the problem of the two-dimensional oscillacting plate in gust

• 대한조선학회논문집
• /
• 제41권2호
• /
• pp.12-20
• /
• 2004

In this study, a linearized super-cavitation theory was applied in order to analyse the performance of the 2-dimensional foils. For flat plate with non-thickness, the numerical results correlated very well with Nishiyama's theoretical results for closed cavitation model. For plano-convex section, the numerical results correlated very well with Wade's experimental data. The new lifting surface procedure, developed and validated in this study, is generally considered applicable to the performance analyses of the super-cavitating propeller and trans-cavitating propeller.