• 대한조선학회논문집
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• 제39권2호
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• pp.1-10
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• 2002

선체-프로펠러-타의 상호작용 해석을 반복계산에 의해 수행하였다. 계측된 공칭속도를 입력자료로 하고 보오텍스 링 이론을 이용하여 유효속도를 계산함으로써 선체와 프로펠러사이의 상호작용을 고려하였고, 계산된 유효속도를 입력자료로 하여 프로펠러-타 상호작용을 계산할 수 있는 포텐셜 기저 패널법을 개발하였다. 프로펠러에 의해 타에 유기되는 속도와 반대로 타에 의해 프로펠러에 유기되는 속도는 수렴된 해가 얻어질 때까지 반복 계산하여 타 주위의 정상유동 해석을 수행하였다. 이와 함께 삼성중공업의 대형 캐비테이션 터널에서 L.D.V를 사용하여 프로펠러 및 타 주위의 유동장을 계측하였고 수치계산 결과와 비교하였다. 실선에 설치되고 있는 혼 타주위의 유동장 계산을 위해 gap flow 모델을 적용하였고, 여러 가지 타각에 대한 수치계산을 수행하여 대형캐비테이션 터널에서 계측된 타 표면에서의 압력과 비교하였으며, 계산된 표면 압력 치는 실험 값과 비교적 일치되는 만족스러운 결과를 얻었다.

• 대한조선학회논문집
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• 제44권2호
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• pp.101-110
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• 2007

Recently, rudder erosion due to cavitation frequently has occurred at large high speed container carriers. Especially, in the case of a horn-type rudder, the rudder erosion is severe around a gap. The gap-flow characteristics are investigated through a computational method to understand the effects of a gap on the cavitation and rudder efficiency. A viscous flow theory utilizing a cavitation model is applied to calculate the flow around idealized 2-dimensional rudder sections in a full scale. The effects of gap clearance and flow-control projection are also investigated. From the computational results, the mass flow rate through a gap is found to be one of the important parameters to affect the cavitation and rudder efficiency.

• 한국정보통신학회논문지
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• 제26권11호
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• pp.1672-1678
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• 2022

본 논문에서는 28GHz 대역의 5G 이동 통신 중계용 혼 안테나의 방사 패턴, 반사손실 등의 성능을 고려하여 중계용 안테나를 설계하였다. 안테나 소자를 위상 배열하여 5G 이동통신 중계기용 혼 Array를 설계하고 성능을 분석하였다. 밀리미터파 대역 통신에서는 기존의 WCDMA(3G), LTE(4G)와 달리 송수신 간의 높은 경로 손실이 발생한다. 5G 밀리미터파 혼 안테나 설계에서는 안테나의 이득, 대역폭뿐만 아니라, 안테나 소자 간 격리도, 이득 등의 안테나 성능을 추가로 고려해야 한다. 28GHz 대역의 단일 혼 안테나(1×1)와 배열 혼 안테나(2×4)의 안테나 이득은 각각 약 10.44dBi와 19.58dBi, 반사손실도 -18dB 이하의 특성을 되도록 설계하여 측정 결과로부터 구현의 타당함을 입증하였고, 5G 이동 통신 중계 시스템에 응용에 적합함을 보였다.

• 대한조선학회논문집
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• 제43권5호
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• pp.578-585
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• 2006

Cavitation related erosion damages on semi-spade rudder generally occur at around leading edge of lower-face and behind gap of lower pintle. To get the idea of gap entrance profile for the latter case, a series of tests with large models has been carried out at MOERI. In the tests, the flow pattern around lower pintle have been investigated and visualized by high speed camera. Additionally, cavitation inception tests and pressure measurements have also been conducted for better comparison. As a result a new model (F rudder) has been developed. The new model turned out to have stable pressure distribution along the surface and so the cavitation inception speeds within ${\pm}5^{\circ}$ of rudder angle were delayed approx. 4 knots in average.

• 대한조선학회논문집
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• 제47권4호
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• pp.543-552
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• 2010

The Coanda effect is noticeable when a jet stream is applied tangential to a curved surface since then the jet stream remains attached to the surface beyond the point where flow separates otherwise and results in augmentation of circulation and lift. Numerous experimental and numerical studies have been performed in various fields of aerodynamics to exploit the Coanda effect and many of them found to be useful. It can be speculated that the Coanda effect may have practical application to the field of marine hydrodynamics as well since various control surfaces are being used to control behaviors of ships and offshore structures. In the present study, the Coanda effect has been applied to a horn type rudder and a series of numerical computations and model experiments are performed to find the practical applicability. The results indicate that the Coanda jet increases the lift coefficient of the rudder as much as 52% at the momentum coefficient $C_j$ = 0.1 and the rudder angle ${\alpha}=10^{\circ}$.

• 대한조선학회논문집
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• 제44권3호
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• pp.228-237
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• 2007

The flow characteristics around a horn-type rudder behind an operating propeller of a high-speed large container carrier are studied through a numerical method in fully wetted and cavitating flow conditions. The computations are carried out in a small scale ratio of 10.00(gap space=5mm) to consider the gap effects. The Reynolds averaged Navier-Stokes equation for a mixed fluid and vapor transport equation applying cavitation model are solved. The axisymmetry body-force distribution technique is utilized to simulate the flow behind an operating propeller. The gap flow, the three-dimensional flow separation, and the cavitation are the flow characteristics of a horn-type rudder. The pattern of three-dimensional flow separation is analyzed utilizing a topological rule. The various cavity positions predicted by CFD were shown to be very similar to rudder erosion positions in real ship rudder. The effect of a preventing cavitation device, a horizontal guide plate, is also investigated.

• 대한조선학회논문집
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• 제45권3호
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• pp.238-246
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• 2008

In the present study, the influences on the gap cavitaiton of the semi-spade rudder are investigated experimentally in the condition with propeller and hull wakes. To reduce the scale effect in the given experimental conditions, 1/28.5-scale-down models of propeller and rudder are manufactured. We have the propeller rotate ahead of the rudder, inducing the three dimensional effects originated from the propeller action. Experimental methods are composed of the cavitation observation using high speed camera, PIV (particle image velocimetry) measurements to visualize the cavitaition and flows around the gap. The propeller slipstream affects both of the gap flows and cavitation of the rudder.

• 산업진흥연구
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• 제8권1호
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• pp.119-134
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• 2023

이 연구는 여러 가지 혼인 택일법 중에 기문둔갑으로 보는 혼인 택일법에 관한 연구이다. 특히 운곡 기문둔갑 이론을 바탕으로 혼인 택일법의 효용 가치와 타당성을 확인하고자 하였다. 즉 조선 시대에서 행사했던 관혼상제, 일반적인 공용(共用)의 날로 택일(擇日) 선시(選時)를 하는 것과는 확실히 다르게, 운곡기문 택일법은 본인의 사주에 맞게 개인만의 택일을 하는 차이가 있다. 운곡 기문학은 홍국수(洪局數)로 동양철학의 기본원리를 이용하여, 논리상 필연적(必然的)인 결론(結論)을 내게 한다는 연역법(演繹法)을 활용한다. 건명 또는 곤명의 결혼 날가림을 홍국수로 합생(合生)의 기본원리인 삼합, 반합, 육합, 생극, 그리고 형살(刑殺)과 삼살(三殺)을 이용하여, 시운(時運)은 일운(日運)에 귀속(歸屬)된다. 또한 일운(日運)은 월운(月運)에 귀속(歸屬)되고, 월운(月運)은 소운(小運)에 귀속(歸屬)되고, 소운(小運)은 대운(大運)에 귀속(歸屬)되고, 대운(大運)은 세(世)에 귀속(歸屬)된다. 이러한 논점의 운곡기문 혼인 택일법에 관한 이론 고찰 및 사례 분석을 통하여 타당성을 검증하였다. 연구의 결과는 운곡 기문둔갑의 혼인 택일법은 타 혼인 택일법에 비하여 다소 적중률이 높게 나타났음이 확인되었다.

• 한국기계가공학회지
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• 제17권5호
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• pp.84-90
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• 2018

When producing a plastic horn cover for an automobile, since the interval between the ribs on the inner surface is narrow, conventional cooling channels cannot be applied and cooling of the mold is difficult. For this reason, the molding operation cannot be completed within a set cycle time. In this study, a conformal cooling channel was applied on the mold to solve the cooling problem. Injection molding simulation was carried out to confirm the effectiveness of the conformal cooling channel. In the analysis results, the mold temperature at the rib section decreased by 33%, and the mold temperature also decreased by 31%. This reduction in temperature allowed for molding within a set cycle time and demonstrated the effectiveness of the conformal cooling channel.

• 대한조선학회 특별논문집
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• 대한조선학회 2009년도 특별논문집
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• pp.47-51
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• 2009

It is well known that a rudder is influential devices to help ship maintain its stable performances, such as a course-keeping and maneuverability. In the procedures of a commercial ship design proper rudder dimensions (area and shape) ensuring better ship maneuverability have been settled in an initial concept design stage performed by a preceding department, without little structural consideration. It is true that there are time discrepancy between an initial design and a structural analysis stage. Therefore structural analysis results would sometimes cause a rudder to modify its dimensions. Most of these cases, however, ship design and performance tests had been finished. In this matter, only limited modifications of redder could be carried out. Besides, these could also cause bad effects on productivity. Finally, it is necessary to develop a new program considering co-relationship between an initial rudder design and a following work, a structural strength analysis, in order to enhance productivity and minimize a rate of redesign procedures.