• 수산해양기술연구
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• 제30권1호
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• pp.13-24
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• 1994

Purse seiner detects a fish school navigating in full speed with the aid of fish finder, sonar, helicopter, etc., and casts a net quickly to enclose the fish school in purse seine net according to the movement of the fish school, wind, and current. At this moment, if the time of casting a net, direction, speed, and turning circle are net suitable, it is unavoidable to lose fish school founded with hard efforts and we only consume our efforts of casting and hauling the net. Therefore, in order to enclose the fish school to enhance the amount of fish for each casting, the author investigated the type of ships equipped with purse seiners and examined maneuvering tests so that we provide some basic information to figure out the ability of steerage correctly. The results obtained are summarized as follows: 1. Block coefficients of pelagic tuna purse seiners with gross tonnage between 500 and 1500 tons are recorded between 0.50 and 0.55 which are greater than those of off shore purse seiners recorded as between 0.44 and 0.54 and less than those of various cargo ships recorded as between 0.56 and 0.84. 2. L/B, L/D, B/D, B/T, and T/D of the class of gross tonnage between 75 and 130 tons are respectively 4.49, 11.00, 2.45, 2.85 and 0.86 as their average and those of the class of between 500 and 1500 tons are 4.89, 10.53, 2.15, 2.73 and 0.75 respectively, which are quite different from those of various cargo ships recorded as 6.0~7.5, 11.0~12.0, 1.6~2.0, 2.2~2.8 and 0.65~0.75 respectively. 3. Rudder area ratio of purse seiners of the class of between 75 and 130 tons is 1/24~1/31 and that of the clase of between 500 and 1500 tons is 1/36~1/42 which is greater than that of various cargo ships recorded as 1.45~1.75. 4. On speed-length ratio of purse seiners. 111 Dong-a has the biggest value 2.94 the class of 130 tons has 2.52 the class of between 75 and 100 tons has 2.30~2.35 and the class of between 500 and 1500 tons has 1.99~2.05. 5. Turning circle of stern trawlers Pusan 404 and Haelim 3 are measured as below according to rudder angles 5$^{\circ}$, 15$^{\circ}$, 25$^{\circ}$ and 35$^{\circ}$ respectively. Advances are 11.3~13.6, 6.0~7.1, 3.6~4.8 and 2.5~3.5 times of LPP respectively. Tactial diameters are 15.2~18.6, 6.9~8.0, 4.2~4.9 and 2.9~3.5 times of LPP. Purse seiner 111 Dong-a with rudder angle 35$^{\circ}$ has a good yaw with quick responsibility since its advance is 2.2~2.3 times of LPP and since its tactial diameter is 2.0~2.1 times of LPP. 6. In full ahead going of purse seiner 111 Dong-a, it takes about 2 minutes and 10.6 times of LPP from the reverse turning its engine into full astern to the ship speed 0. In its full astern going, it takes about 1 minute and 5.1 times of LPP from the reverse turning its engine into full ahead to the ship speed 0. In its full ahead going, it takes about 2 minutes and 50 seconds and 12.3 times of LPP from stopping its engine to the dead slow ahead speed 3.2 knots.

• 대한조선학회지
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• 제22권2호
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• pp.35-48
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• 1985

The present work develops a method of evaluating thrust deduction and wake for different loads of the propeller using the concerted application of the theoretical tools and experimental techniques. It also shows the applicability of the new method to the design of optimum hull form. Firstly, the problem of hull-propeller interaction was analyzed in terms of inviscid as well as viscous components of the thrust deduction and wake. The wavemaking resistance of a hull and propeller were mathematically represented by sources on the hull surface and sink on the propeller plane, respectively. The strength of sink was determined by utilizing the radial distributions of propeller load and nominal wake. The resistance increment due to a propeller and the axial perturbation flow induced by the hull in the propeller plane were calculated. Especially, the inviscid component of the thrust deduction was calculated by subtraction the wavemaking resistance of a bare hull, the wavemaking resistance of a free-running propeller and the augmentation of propeller resistance due to hull action from the wavemaking resistance of the hull with a propeller. The viscous components of the thrust deduction and wake were estimated as functions of propeller load which were established by the propeller load varying test after deduction the calculated inviscid components. Secondly, an analysis method of powering performance was developed based on the potential theory and the propeller load varying test. The hybrid method estimates the thrust deduction, wake and propeller open-water efficiency for different propeller load. This method can be utilized in the analysis of powering performance for the propeller load variation such as the added resistance due to hull surface roughness, the added resistance due to wind, etc. Finally, the hybrid method was applied to the optimum design of hull form. A series of afterbody shapes was obtained by systematically varying the waterplane and section shapes of a parent afterbody without changing the principal dimensions, block coefficient and prismatic coefficient. From the comparison of the predicted results such as wavemaking resistance, thrust deduction, wake and delivered power, an optimum hull form was obtained. The delivered power of the optimized hull form was reduced by 5.7% which was confirmed by model tests. Also the predicted delivered power by the hybrid method shows fairly good agreement with the test result. It is therefore considered that the new analysis method of powering performance can be utilized as a practical tool for the design of optimum hull form as for the analysis of powering performance for the propeller load variation in the preliminary design stage.

• 한국전산구조공학회논문집
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• 제29권1호
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• pp.29-36
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• 2016

러그는 선박 및 해양구조물의 블록을 이동하거나 반전에 많이 사용되는 부품이다. 선박이나 해양구조물의 제작기술이 발전함에 따라 블록이 점차 대형화되고 있어, 생산성 향상을 위해 블록을 보다 효율적으로 다루는 기술에 대한 중요성이 대두되고 있다. 러그 구조의 안전하고 경제적인 설계를 위하여 비선형 구조해석 결과를 토대로 도출한 최종강도를 기준으로 한 보다 합리적인 설계과정이 필요하다. 본 연구는 조선소에서 자주 사용하는 T형 러그의 최적 구조설계를 다루고 있다. 본 연구에서의 T형 러그에 대한 최적 구조설계 결과는 충분한 구조적 안전성이 보장될 것으로 판단되고, 러그 용량별 최적 구조설계 결과의 중량 감소량에 어떤 규칙성을 발견할 수 없었는데, 이는, 현재의 설계과정에 대한 검토가 필요한 것으로 생각된다. 여기에서 제시한 비선형 구조해석에 기초한 최적 구조설계 과정은 향후 보다 다양한 경우의 러그 설계에 적용될 수 있을 것이다.

• 대한조선학회논문집
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• 제50권5호
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• pp.324-333
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• 2013

Recently, rudder erosion due to cavitation has been frequently reported on a semi-spade rudder of a high-speed large ship. This problem raises economic and safety issues when operating ships. The semi-spade rudders have a gap between the horn/pintle and the movable wing part. Due to this gap, a discontinuous surface, cavitation phenomenon arises and results in unresolved problems such as rudder erosion. In this study, we made a rudder model for 2-D experiments using the NACA0020 and also manufactured gap flow blocking devices to insert to the gap of the model. In order to study the gap flow characteristics at various rudder deflection angles($5^{\circ}$, $10^{\circ}$, $35^{\circ}$) and the effect of the gap flow blocking devices, we carried out the velocity measurements using PIV(Particle Image Velocimetry) techniques and cavitation observation using high speed camera in Seoul National University cavitation tunnel. To observe the gap cavitation on a semi-spade rudder, we slowly lowered the inside pressure of the cavitation tunnel until cavitation occurred near the gap and then captured it using high-speed camera with the frame rate of 4300 fps(frame per second). During this procedure, cavitation numbers and the generated location were recorded, and these experimental data were compared with CFD results calculated by commercial code, Fluent. When we use gap flow blocking device to block the gap, it showed a different flow character compared with previous observation without the device. With the device blocking the gap, the flow velocity increases on the suction side, while it decreases on the pressure side. Therefore, we can conclude that the gap flow blocking device results in a high lift-force effect. And we can also observe that the cavitation inception is delayed.

• 한국해양환경ㆍ에너지학회지
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• 제6권2호
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• pp.46-53
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• 2003

본 연구는 항만공사시 발생되는 부유토사의 거동특성을 분석하기 위하여 항만공사 중 부유토사의 발생이 가장 많은 공정인 직접투하방식에 의한 매립공사 및 그랩준설공사륵 대상으로 부유토사 발생거동에 대해 조사하였다. 본 조사결과에 의하면 700ton급 대선을 이용해 준설토를 직접 투하하는 방식에 의한 매립공사의 경우 매립토 직투(700㎥)후 부유토사가 순간적으로 매우 높은 농도로 발생하여 부유토사는 60분간 지속되었다. 그랩준설공사시의 부유토사의 거동에 대한 조사결과 발생원 주변에서 수심에 관계없이 고농도의 부유토사가 발생하여 부유토사는 띠를 형성하며 조류방향을 따라 이동하여 700m이상 확산되었다. 본 연구결과를 토대로 볼 때 부유토사의 발생을 저감시키기 위해 항만공사시 설치하는 오탁방지막의 설치위치를 가능한 공사지점으로부터 가까운 거리에 설치하는 것이 부유토사의 확산을 저감하는데 효율적이며, 오탁방지막의 막체길이는 가능한 길게 설치하도록 하여 저층으로 확산되는 부유토사의 확산을 저감시키는 것이 바람직할 것으로 판단된다.

• 비교문화연구
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• 제45권
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• pp.7-32
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• 2016

이 논문은 재일코리언 김시종의 장편시집 "니이가타"의 표현을 고찰해 식민 이후와 분단의 시대를 살아가는 '재일'의 의미를 생각해본 것이다. "니이가타"는 1959년에 니이가타 항에서 재일코리언이 북한으로 귀국하는 모습을 바라보며, 제주 4.3사건 이후 정부 당국에 쫓겨 1949년에 일본으로 건너와 현재에 이르기까지 재일의 삶을 살고 있는 김시종의 '재일'에 대한 적극적인 의미 표명을 상징적인 표현을 통해 잘 보여주고 있는 시집이다. 김시종은 스스로를 재일 2세로 정위하고 일본사회 속에서 현실적이고 주체적으로 살아가는 길을 모색해왔다. 그는 남북 분단의 현장이며 38도 선의 연장선상에 있는 니이가타에서 조국에서는 넘을 수 없었던 분단을 넘는 상상을 한다. 이는 재일의 삶을 살고 있기에 가능한 공간 확장의 상상이라고 할 수 있다. "니이가타"는 '재일'이 한국과 일본 사이에 끼어 정체성의 불안을 느끼는 네거티브한 존재가 더 이상 아니라, 한국과 북한, 그리고 일본을 모두 포괄하며 이들을 새로운 의미로 관련지을 수 있는 존재임을 보여주고 있다. 식민과 분단의 어두운 기억 속에서 살던 자아를 깨워 새로운 공간의 상상력을 펼침으로써 남북을 총칭하는 '조선'과 일본을 아우르는 지점에서 재일을 사는 의미를 찾고자 한 시인의 적극적 의지 표명을 읽어낼 수 있다.

• 해양환경안전학회지
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• 제28권7호
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• pp.1267-1273
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• 2022

최근 한국 조선업계가 세계 선박 발주 물량의 대부분을 수주하고 있지만, 생산 현장에서는 인력난으로 생산공정 차질을 겪고 있다. 오랜 조선업 불황으로 일감과 임금 모두 줄어든 탓에 근로자들이 조선소를 떠났기 때문이다. 수주가 증가한 주요 요인은 카타르 LNG선 대량 발주였으며, 선박에 요구되는 기술 사양이 복잡해지는 상황도 유리하게 작용하고 있다. 선박은 계약한 인도 시점이 무엇보다도 중요하기 때문에, 조선소의 주요 공정 중 도크 진수 계획이 무엇보다도 중요한 관리 아이템이다. 도크에서 건조되는 구조물은 의장 작업을 남긴 선체 혹은 완성형 선박일 수 있으며, 때에 따라서 선체의 일부 블록 수준일 경우도 많다. 진수 시, 선체는 유체력에 의한 호깅(hogging) 혹은 새깅(sagging) 모멘트 영향을 받게 되고, 블록 연결부의 구조강도에 대한 안전성 확보가 무엇보다도 중요하다. 정상적인 공정이라면 연결 부재는 용접을 끝낸 상태에서 진수하지만, 실제 조선사에서는 도크 일정을 준수하기 위하여 구조 안전성이 확보되는 조건에 대한 빠른 의사결정이 필요하다. 본 연구에서는 앞서 언급한 문제점들을 엔지니어링 관점에서 합리적으로 판단하기 위하여 휨 응력평가법과 유한요소해석 모델링을 사용한 상세 해석법과 적용성을 분석하였다. 논문에서 언급된 주요 내용은 향후 유사 구조 강도 평가의 진행 시 좋은 사례로 활용될 수 있을 것으로 생각한다.

• Strategy21
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• 통권34호
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• pp.128-148
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• 2014

In south Korea, the so-called 'conservative-liberal' rivalry over the assessment of the government's North Korean policies is seen to be impeding the road to right policy choices. For example, the liberals accused former President Lee Myung-bak's hardline policy of provoking Pyongyang and leading to a deterioration of inter-Korean relations, while the conservatives appreciated it for helping nurture mutually beneficial inter-Korean relations in the longer term by compelling North Korea to observe international norms. However, such debate over the vices and virtues of Seoul's North Korea policies is hardly meaningful as the measuring sticks used by the liberals and the conservatives are entirely different matters. The two major goals South Korea must pursue with its North Korean policies should be 'peaceful management of division' and 'change in North Korea'. The former is related to maintaining stability within South Korea and promoting co-prosperity with North Korea. For this, the nation needs to engage, encompass and assist the Pyongyang regime. The second goal is also necessary since South Korea, as a divided nation, must seek a unified Korea under the system of democracy and market economies by bringing change in North Korea. For this, South Korea needs powerful leverages with which it can persuade and coerce the North. This means that the nation is destined to simultaneously chase the above-mentioned two goals, while also both recognizing and negating the legitimacy of the North Korean regime. This situation necessitates Seoul to apply flexibility in reconciling with Pyongyang while applying firm principles to sever the vicious circle involving the North's military provocations. The May 25 Measures, which banned trade and economic cooperation with the North except those related to humanitarian assistance, were taken as sanctions against Pyongyang for sinking the South Korean corvette Chonan in March 2010. The Measures were taken by the Seoul government immediately after a multinational investigation team discovered evidence confirming that the South Korean naval ship had been torpedoed by a midget North Korean submarine. Naturally, the May 24 Measures have since then become a major stumbling block in inter-Korean exchange, prompting opposition politicians and concerned entrepreneurs to demand Seoul to unilaterally lift the Measures. Given the significant damages the Measures have inflicted on inter-Korean economic relations, removing them remains as homework for both Koreas. However, the Measures pertains to the 'principles on national security' the Seoul government must adhere to under all circumstances. This is why North Korea's apology and promises not to repeat similar provocations must come first. For now, South Korea has no alternative but to let North Korea solve the problems it has created. South Korea's role is to help the North do so.

• 융합신호처리학회논문지
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• 제24권1호
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• pp.27-33
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• 2023

최근 기후변화로 인한 물 부족 현상이 발생하고 있으며 저수지의 녹조 발생으로 농업용수의 물 관리 필요성이 증대되고 있다. 기존의 녹조 방지는 많은 사람이 현장에 투입돼 운영되고 보트를 통한 이동으로 최적의 살포 시간을 놓치고 있다. 이를 해결하기 위해서는 오염을 사전에 차단하고 시간 내 이동하여 균일하게 복합 미생물을 균일하게 살포하는 기술이 필요하다. 방제 드론은 농약 살포에 활용되고 있으며 방제 드론을 활용하여 녹조 방지 업무에 적용이 가능하다. 본 논문에서는 해양 방제 시스템 구축을 위한 기초연구로 저수지 환경 적용을 위해 수행되었으며, 그 결과물의 하나로 방제 드론에 사용 가능한 핵심기술인 드론 전용 노즐의 특성을 산출하였다. 특히, 기존의 농업용 방제 드론이 제시된 살포 간격 내에서 농도가 불균일하다는 단점이 있음을 파악하였고, 이를 보완하기 위해 노즐 위치선정 및 노즐 살포 균일도를 산출하였다. 실험 결과를 바탕으로 저수지 환경의 녹조 감시 시스템 구축의 핵심 알고리즘을 개발하고 추후 해양 방제 업무 적용에 활용이 가능하도록 정밀 방제 기술을 제안한다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2011년도 제36회 춘계학술대회논문집
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• pp.1-2
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• 2011

Hybrid rockets have lately attracted attention as a strong candidate of small, low cost, safe and reliable launch vehicles. A significant topic is that the first commercially sponsored space ship, SpaceShipOne vehicle chose a hybrid rocket. The main factors for the choice were safety of operation, system cost, quick turnaround, and thrust termination. In Japan, five universities including Hokkaido University and three private companies organized "Hybrid Rocket Research Group" from 1998 to 2002. Their main purpose was to downsize the cost and scale of rocket experiments. In 2002, UNISEC (University Space Engineering Consortium) and HASTIC (Hokkaido Aerospace Science and Technology Incubation Center) took over the educational and R&D rocket activities respectively and the research group dissolved. In 2008, JAXA/ISAS and eleven universities formed "Hybrid Rocket Research Working Group" as a subcommittee of the Steering Committee for Space Engineering in ISAS. Their goal is to demonstrate technical feasibility of lowcost and high frequency launches of nano/micro satellites into sun-synchronous orbits. Hybrid rockets use a combination of solid and liquid propellants. Usually the fuel is in a solid phase. A serious problem of hybrid rockets is the low regression rate of the solid fuel. In single port hybrids the low regression rate below 1 mm/s causes large L/D exceeding a hundred and small fuel loading ratio falling below 0.3. Multi-port hybrids are a typical solution to solve this problem. However, this solution is not the mainstream in Japan. Another approach is to use high regression rate fuels. For example, a fuel regression rate of 4 mm/s decreases L/D to around 10 and increases the loading ratio to around 0.75. Liquefying fuels such as paraffins are strong candidates for high regression fuels and subject of active research in Japan too. Nakagawa et al. in Tokai University employed EVA (Ethylene Vinyl Acetate) to modify viscosity of paraffin based fuels and investigated the effect of viscosity on regression rates. Wada et al. in Akita University employed LTP (Low melting ThermoPlastic) as another candidate of liquefying fuels and demonstrated high regression rates comparable to paraffin fuels. Hori et al. in JAXA/ISAS employed glycidylazide-poly(ethylene glycol) (GAP-PEG) copolymers as high regression rate fuels and modified the combustion characteristics by changing the PEG mixing ratio. Regression rate improvement by changing internal ballistics is another stream of research. The author proposed a new fuel configuration named "CAMUI" in 1998. CAMUI comes from an abbreviation of "cascaded multistage impinging-jet" meaning the distinctive flow field. A CAMUI type fuel grain consists of several cylindrical fuel blocks with two ports in axial direction. The port alignment shifts 90 degrees with each other to make jets out of ports impinge on the upstream end face of the downstream fuel block, resulting in intense heat transfer to the fuel. Yuasa et al. in Tokyo Metropolitan University employed swirling injection method and improved regression rates more than three times higher. However, regression rate distribution along the axis is not uniform due to the decay of the swirl strength. Aso et al. in Kyushu University employed multi-swirl injection to solve this problem. Combinations of swirling injection and paraffin based fuel have been tried and some results show very high regression rates exceeding ten times of conventional one. High fuel regression rates by new fuel, new internal ballistics, or combination of them require faster fuel-oxidizer mixing to maintain combustion efficiency. Nakagawa et al. succeeded to improve combustion efficiency of a paraffin-based fuel from 77% to 96% by a baffle plate. Another effective approach some researchers are trying is to use an aft-chamber to increase residence time. Better understanding of the new flow fields is necessary to reveal basic mechanisms of regression enhancement. Yuasa et al. visualized the combustion field in a swirling injection type motor. Nakagawa et al. observed boundary layer combustion of wax-based fuels. To understand detailed flow structures in swirling flow type hybrids, Sawada et al. (Tohoku Univ.), Teramoto et al. (Univ. of Tokyo), Shimada et al. (ISAS), and Tsuboi et al. (Kyushu Inst. Tech.) are trying to simulate the flow field numerically. Main challenges are turbulent reaction, stiffness due to low Mach number flow, fuel regression model, and other non-steady phenomena. Oshima et al. in Hokkaido University simulated CAMUI type flow fields and discussed correspondence relation between regression distribution of a burning surface and the vortex structure over the surface.