• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 춘계학술대회논문집B
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• pp.561-567
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• 2000

This paper is concerned with the viscous interaction between rotor and stator. The viscous interaction is caused by wakes from upstream blades. The rotor cascade in the experiment was composed with five blades, and cylinders were placed to make the stator wakes and their locations were about 50 percent upstream of blade chord. The locations of cylinders were varied in the direction of cascade axis with 0, 12.5, 25, 50, and 75 percent of pitch length. The static pressure distributions on the blade surfaces and the velocity distributions in the cascade flow were measured. From the experimental result it was found that the value of velocity defect by a cylinder wake might vary depending on the wake position within the cascade but the value at the cascade exit approached to some constant value regardless of the difference of wake locus. The momentum defect at the downstream from the cascade and the pressure distribution on the blade surfaces showed that the wake flowing near the blade surfaces caused the decrease of lift and the increase of drag regardless of the disappearance of flow separation.

• 한국유체기계학회 논문집
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• 제11권2호
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• pp.20-28
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• 2008

Recently, butterfly valves are used as control valves for industrial process. However, there are not so many reports on cryogenic butterfly valves in spite of broad application in LNG storage station and LNG carriers. Present study is focused on the investigation of the detailed hydrodynamic and aerodynamic characteristics of cryogenic butterfly valves to contribute to the operation during the handling on LNG transportation system, and to the practical utilization in design of butterfly valves and actuators. The results show that large recirculation vortices in the region downstream of the valve are founded and the cavitation flows are intensively generated on the surface of valve disc at the relatively small opening angle. The aerodynamic characteristics, lift, drag and torque, acting on the valve disc are calculated. The pressure distribution and the pressure loss coefficient of the cryogenic butterfly valve show almost similar pattern with those of the butterfly valve which is used on the normal temperature.

• 한국추진공학회지
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• 제12권3호
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• pp.49-59
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• 2008

본 연구에서는 155 mm 고체연료 램제트 추진 탄의 설계방법을 제시하였고 수학적 모델링을 통한 비행성능 해석 프로그램을 개발하였다. 비행성능 해석을 통하여 추력, 비추력, 압력 회복률, 충격파의 위치, 항력의 크기 등 비행 중 램제트 성능을 예측하였다. 비행탄도 해석결과 RAP에 비하여 90 % 정도의 사거리 증대효과를 나타내었다. 또한 노즐 출구 면적비와 흡입구 면적의 변화에 따른 사거리 변화의 추이를 살펴보았다. 제시된 모델링과 시뮬레이션 방법은 램제트 탄의 개발에 필요한 설계 자료로 매우 유용할 것이다.

• 대한기계학회논문집B
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• 제22권3호
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• pp.346-359
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• 1998

The aerodynamic forces and wake structure of the non-rotating downstream circular cylinder, of which the uniform freestream flow is interfered with another spinning upstream cylinder having the same diameter that is located upstream in a line have been investigated experimentally. When the spin rate of the downstream cylinder defined as the ratio of tangential surface velocity of the spinning cylinder to the freestream velocity increases gradually from zero to 1.4, the change of surface pressure distribution, aerodynamic forces of the non-rotating downstream cylinder were measured in case of several distance ratios of 1.5, 3.0, and 4.5 defined as the ratio of distance between the centers of two cylinders to the diameter. The wake flow patterns behind the cylinder were also investigated in each case. From the present experiments, it has been found that the spin rate significantly influences the aerodynamic forces and near-wake flow phenomena of the downstream cylinder in such a way that the drag increases as the spin rate and distance ratio increase and the wake width increases as the distance ratio increases.

• 한국해안·해양공학회논문집
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• 제27권2호
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• pp.113-117
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• 2015

본 연구에서는 연결재(커플러)로 결합된 라이저의 외부흐름에 따른 3차원 유동-구조 연동해석을 수행하였다. 두 가지 연결재(평면 커플러, 곡면 커플러)를 고려하였으며 ANSYS CFX를 사용하여 수치해석을 수행하였다. 유동해석에서 유동공간은 유입구, 유출구와 대칭 경계조건으로 구성되었으며 연결재의 형상에 따른 항력계수와 유속 분포 결과를 비교하였다. 구조해석에서는 라이저의 응답(최대 변위 및 최대 등가응력)을 통해 연결재의 유용성을 확인하였다.

• 대한조선학회논문집
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• 제30권1호
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• pp.104-114
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• 1993

본 논문에서는 점성유동에 미치는 자유표면의 영향을 조사하기 위하여 자유표면을 수직으로 관통하는 원통 주위의 유동을 수치 시뮬레이션 하였다. 수치해석 방법으로서 Artificial Compressibility Method를 사용하였으며, 계산은 낮은 레이놀드수의 영역에 국한하였다. 계산결과는 자유표면에 가까운 유체영역에서 유선, 점성항력 등에 적지않은 영향이 있음을 보여주고 있다. 자유표면의 존재는 물체 후류 중의 와류를 물체로 부터 분리시키는 방향으로, 점성항력을 감소시키는 방향으로 작용하는 것으로 보인다.

• 대한조선학회논문집
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• 제56권4호
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• pp.327-334
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• 2019

Recently, there has been a growing interest in artificial supercavitation as a way to reduce friction drag of submerged vehicles. A cavitator plays an important role to generate the supercavity, so many studies have focused on the case of cavitator only. However, the body shape behind the cavitator affects the growth of the supercavity and this effect must be considered for evaluating the overall performance of the system. In this work, we conducted experimental investigation on artificial supercavitation generated by different combinations of the cavitator and body. We observed the supercavity pattern by using a high-speed camera and measured the pressure inside the cavity by using an absolute pressure transducer. We estimated the relation between the amount of injected air and the supercavity shape for different combinations. In summary, the disk type cavitator generates larger supercavity than that of the cone and ellipsoidal cavitators, but cavity development speed is relatively slower rather than the others. Furthermore, fore body angle plays an important role to generate the supercavity enveloping the entire body.

• International Journal of Naval Architecture and Ocean Engineering
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• 제12권1호
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• pp.38-47
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• 2020

The partial air cushion supported catamaran (PACSCAT) is a novel Surface Effect Ship (SES) and possesses distinctive resistance performance due to the presence of planing bottom. In this paper, the design of PACSCAT and air cushion system are described in detail. Model tests were carried out for Froude numbers ranging from 0.1 to 1.11, the focus is on the influence of air cushion system on resistance characteristics. Drag-reducing effect of air cushion system was proved by means of contrast tests in cuhionborne and non-cushionborne mode. Wave-making characteristics reflect that the PACSCAT would eventually enter planing regime, in which the air could just escape under the seals and the hull body could operate in a steady state. To acquire different air cushion pressure, air flow rate and leakage height were adjusted during tests. Experimental results show that the resistance performance in planing regime would decrease evidently as the increased air flow rate, however, the scheme with medium leakage height presents the best resistance performance in the hump region.

• Wind and Structures
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• 제35권1호
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• pp.67-81
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• 2022

While the aerodynamics of solid bluff bodies is reasonably well-understood and methodologies for their reliable numerical simulation are available, the aerodynamics of porous bluff bodies formed by assembling perforated plates has received less attention. The topic is nevertheless of great technical interest, due to their ubiquitous presence in applications (fences, windbreaks and double skin facades to name a few). This work follows previous investigations by the authors, aimed at verifying the consistency of numerical simulations based on the explicit modelling of the perforated plates geometry and their representation by means of pressure-jumps. In this work we further expand such investigations and, contextually, we provide insight into the flow arrangement and its sensitivity to important modelling and setup configurations. To this purpose, Unsteady Reynolds-Averaged Navier-Stokes (URANS) and Large-Eddy Simulations (LES) are performed for a 5:1 rectangular cylinder at null angle of attack. Then, using URANS, porosity and attack angle are simultaneously varied. To the authors' knowledge this is the first time in which LES are used to model a porous bluff body and compare results obtained using the explicit modelling approach to those obtained relying on pressure-jumps. Despite the flow organization often shows noticeable differences, good agreement is found between the two modelling strategies in terms of drag force.

• 한국구조물진단유지관리공학회 논문집
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• 제21권6호
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• pp.126-131
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• 2017

저유속 조건에서 소수력 에너지 생산 효율 증진을 위한 항력식 수직축 수차를 개발하기 위하여 전산 유체 동역학(CFD) 기법을 이용하여 수치해석을 수행하였다. 1.0~3.0 m/s의 유속 조건에서 수차 블레이드의 타공 유무에 따른 블레이드 압력 변화와 내부유동을 분석하였다. 수치해석 결과, 타공이 있는 경우 유속에 따라 수차 블레이드의 압력 및 유체 속도가 영향을 크게 받는 것으로 나타난 반면에, 타공이 없는 경우에는 유속에 따른 수차 블레이드의 압력 및 유체 속도의 영향이 상대적으로 감소하는 것으로 나타났다. 또한, 타공이 포함되지 않은 수차 블레이드에 비교하여 타공이 포함된 수차 블레이드 표면에서 압력 분포와 유체의 속도가 고르게 나타났으며, 따라서 수차 블레이드에 타공을 형성하는 것이 구조안전성 측면에서 도움이 될 것으로 판단된다.