• 한국안전학회지
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• 제28권4호
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• pp.14-18
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• 2013

Blades of horizontal axis are nowadays made of composite materials. Generally, composite materials satisfy design provides lower weight and good stiffness, while laminate composites have often damages as like the delamination and cracks at the interface of laminates. The box spar and tail parts of a blade are composed of the CFRP/GFRP hybrid laminate composites. However, delamination and the interfacial crack often occur in the interface of CFRP/GFRP hybrid laminate composites under the mixed mode fracture condition, especially mode I and mode II. Therefore, there is a need for the evaluation of the mixed mode fracture behavior during the delamination of CFRP/GFRP hybrid laminates. This study shows the experimental results for the delamination fracture toughness in CFRP/GFRP hybrid laminate composites. Fracture toughness experiments and estimation are performed by using DMMB(Dissimilar mixed mode bending) specimen. The materials used in the test are a commercial woven type CFRP(Carbon fiber reinforced plastic) prepreg(CF3327) and UD type GFRP(Glass fiber reinforced plastic) prepreg(HD224A). A CFRP/GFRP hybrid laminate composite is composed by the 10 plies CFRP and GFRP prepreg for DMMB. A thickness of CFRP and GFRP layer is 2.5mm and 3.0mm, respectively. Also the fulcrum location which is a loading parameter is changed from 80 to 100mm on the specimen of length 120mm because it defines the ratio of mode I to mode II. In this study, the effects of the fulcrum location are evaluated in the viewpoint of energy release rate in mode I and mode II contribution. The results show that the delamination crack initiates at higher displacement and lower load according to the increase of the fulcrum location ratio. And the variation of the energy release rate for mode I and II contributions for the mode mixity are shown.

• 한국유체기계학회 논문집
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• 제14권6호
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• pp.96-101
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• 2011

Korea Aerospace Research Institute is performing 3 stage transonic axial compressor development program. This paper introduces design step of the compressor, the performance test results and its analysis. In the fore part of the paper, aerodynamic process of the 3 stage axial compressor is presented. To satisfy both of the mass flow and pressure rise, the compressor should rotate at a high rotational speed. Therefore the transonic flow field forms in the rotor stages and it is designed with a relatively high pressure rise per stage to satisfy its design target. The compressor stage consists of 3 stages, and the bulk pressure ratio is 2.5. The first stage is burdened with the highest pressure ratio and less pressure rises occur in the following stages. Also it is designed that tip Mach number of the first rotor row does not exceed 1.3, while the maximum relative Mach number in the rotor stage is between 1.3~1.4 to increase the compressor flow coefficient. The final design has been confirmed by iterating three dimensional CFD calculations to verify design target and some design intentions. In the latter part of the paper, its performance test processes and results are presented. The performance test result shows that the overall compressor performance targets; pressure ratio and efficiency are well achieved. The stator static pressure distributions show that the blade loading is gradually increasing from the downstream of the compressor.

• 한국세라믹학회지
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• 제38권9호
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• pp.860-865
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• 2001

본 논문은 출발물로서 2mol% CdO가 치환된 $0.05Pb(Mn_{1/3}Sb_{2/3})O_3-0.95Pb(Zr_{0.52}Ti_{0.48})O_3$ 분말을 제조 후, 닥터 블레이드 방법으로 green sheet를 제조하기 위한 slurry의 최적 공정첨가제 조성에 관한 연구를 수행하였다. 또한, 제조된 green sheet에 대하여 소결 특성과 두께 변환에 따른 유전 및 압전 특성을 관찰하였다. 공정첨가제의 첨가에 따른 점도거동을 통하여 slurry를 최적화하였고, TGA 분석으로 소결조건을 정하였으며, sheet의 특성에 미세구조와 XRD 등으로 측정하였다. 최적의 slurry는 고형분량 30vol%에 대해 분산제 3.0wt%에서 가장 안정화되었고, 이후 바인더/가소제(0.75/0.25) 3.0wt% 첨가시 점도는 7.55Pa${\cdot}$s이었다. Green sheet의 유전 및 압전 특성들은 각각 900$^{\circ}$C, 950$^{\circ}$C, 1000$^{\circ}$C로 소결온도를 증가함에 따라 다소 증가하였지만, 두께에 따른 특성들은 큰 변화가 관찰되지 않음을 확인하였다.

• 대한조선학회논문집
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• 제49권6호
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• pp.528-533
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• 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.

• 농업과학연구
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• 제43권3호
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• pp.432-440
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• 2016

The consumption of pre-treated vegetables (including fresh-cut vegetables) that are washed, peeled, and trimmed has been significantly increased because of their easy use for cooking. Vegetable cutting machines have been widely utilized for producing fresh-cut vegetables or agricultural products of different sizes; however, the design standard is not established for specific types of agricultural products. Therefore, this study was conducted to determine mechanical properties (compressive and shear forces) of targeted agricultural products (radish, carrot, squash, cucumber, shiitake mushroom, and sweet potato) for developing a multipurpose vegetable cutting machine. According to ASAE standard (s368.3), compressive and shear forces of targeted agricultural products were measured by using a custom built UTM (universal testing machine). Shape type of samples and speed ranges (5 - 15 mm/min) of loading rate on bioyield and shear points varied depending on the targeted agricultural product. The range of averaged bioyield points of targeted agricultural products were between 7.89 and 146.98 N. On the other hand, their averaged shear points ranged from 22.50 to 53.47 N. Results clearly showed that the bioyield and shear points of targeted agricultural products were thoroughly affected by their components. As measuring compressive and shear forces of a variety of agricultural products, it will be feasible to calculate blade cutting force for designing multipurpose vegetable cutting machine.

• 대한조선학회논문집
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• 제50권1호
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• pp.1-7
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• 2013

The high-skewed and/or composite propellers of current interests to reduce the ship vibration and to increase the acoustic performance are likely to be exposed to the unexpected structural problems. One typical example is that the added mass effect on the propellers working in the non-uniform wake field reduces the natural frequency of the propeller leading to the resonance with the low-frequency excitation of the external forces. To avoid this resonance problem during the design stage, the technique of fluid-structure interaction has been developed, but the higher-order effect of the blade geometry deformation is not yet considered in evaluating the added mass effects. In this paper the fluid boundary-value problem is formulated by the potential-based panel method in the inviscid fluid region with the velocity inflow due to the body deformation, and the structural response of the solid body under the hydrodynamic loading is solved by applying the finite element method which implements the 20-node iso-parametric element model. The fluid-structure problem is solved iteratively. A basic fluid-sturcture interaction study is performed with the simple rectangular plates of thin thickness with various planform submerged in the water of infinite extent. The computations show good correlation with the experimental results of Linholm, et al. (1965).

• 대한조선학회논문집
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• 제31권3호
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• pp.135-144
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• 1994

본 논문에서는 한 차량운반선에서 발생했던 진동문제와 그 해결과정에 대하여 연구하였다. 선박의 거주구를 포함한 선미부 전체가 프로펠러의 날개주파수와 공진하는 매우 규모가 큰 진동문제였다. 일반적으로 차량운반선은 구조적 특성때문에 진동에 취약한 것으로 알려져 있다. 본 선박은 일반차량운반선과는 달리 트레일러, 특수차량 및 비정형 대형화물을 위한 선박이기 때문에 거주구 하부 및 화물창 내부에 횡격벽과 기둥이 전혀 없는 구조적 특징을 갖고있다. 이외에 과도진동의 원인이라고 생각되는 여러가지 구조적인 문제점을 살펴보았고 향후의 방진설계를 위한 개선대책을 검토하였다. 실선계측을 통한 진동양상의 파악과 유한요소해석을 통해 예측된 여러 보강안들의 효과를 비교 검토한 후에 비교적 적은 보강재를 사용하여 진동레벨을 50-80% 감소시킨 성과를 얻었다. 아울러 강제진동응답, 구조보강의 효과 그리고 화물적재에 따른 진동특성의 변화에 대해 실선계측치와 유한 요소해석의 결과를 비교 검토하였다.

• 해양환경안전학회지
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• 제25권1호
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• pp.130-137
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• 2019

원심 해수냉각 펌프를 분석하기 위하여 다른 운전 유량에 대한 캐비테이션 거동을 조사하였다. 3D 2상 해석은 ANSYS-CFX 상용코드로 수행되었다. 해석에는 $k-{\varepsilon}$ 난류와 Rayleigh-Plesset cavitation 모델이 사용되었다. 수치 예측에 기초하여 세 가지 토출 유량값에 대하여 헤드 드롭 특성곡선이 작성되었다. 더 높은 유량에서 임펠러는 버블 캐비테이션에 보다 취약하다. 0.7Q, Q 및 1.3Q(Q: 설계 유량)에서 작동하는 펌프의 3 % 헤드 드롭 위치는 각각 NPSHa 1.21 m, 1.83 m 및 3.45 m에 해당한다. 증기 기포의 볼륨이 예측되고 캐비테이션의 위치는 임펠러 내에서 발생하는 캐비티를 시각화하여 예상하였다. 또한, 압력계수와 날개 부하 분포가 구체적으로 제시되어 캐비테이션이 펌프 운전에 미치는 해로운 영향을 나타냈다. 또한, 압력계수 분포와 날개부하 차트가 구체적으로 제시되어, 펌프 운전에 캐비테이션이 미치는 해로운 영향을 나타냈다.

• 대한조선학회논문집
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• 제28권2호
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• pp.52-68
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• 1991

캐비테이션 특성이 우수하고 넓은 받음각에서 양력-향력비가 큰 새로운 날개단면(KH18 단면)을 사용하여 체계적인 방법으로 기하학적 형상을 변화시켜 설계된 새로운 계열 프로펠러의 개발을 시도하였다. 새로운 계열 프로펠러의 형상을 설계함에 있어 기존의 계열 프로펠러와는 달리 선택된 반류분포의 회전방향 평균 반류분포를 입력자료로 하여 반경방향 부하분포와 코오드 방향 부하분포를 동일하게 유지하면서 피치 및 캠버의 형상을 결정하였다. 또한 코오드 길이, 두께, 스큐 및 레이크 분포와 같은 형상은 최근 실적선 프로펠러의 형상 특성을 정형화하여 선택되었기 때문에 초기설계시 설계된 형상이 최종 설계 프로펠러의 형상과 크게 다르지 않을 것으로 생각되어 초기성능을 보다 정확하게 추정할 수 있게 하였다. 설계된 계열 프로펠러는 날개수 4개인 프로펠러를 대상으로 날개 전개면적비 4개($A_{E}/A_{O}$=0.3, 0.45, 0.6, 0.75)에 대하여 각 전개면적비에서 평균피치비를 5개(P/D=0.5, 0.65, 0.8, 0.95, 1.1)로 변화시켜 총 20개의 프로펠러로 구성되었으며 KD-프로펠러 씨리즈(KRISO-DAEWOO Propeller Series)라 명명하였다. 설계된 계열 프로펠러들에 대하여 단독특성시험, 캐비테이션 관찰시험, 변동압력 계측시험을 수행하였다. 프로펠러 단독특성 시험결과의 회귀해석결과로 부터 $B_{P}-\delta$ 곡선을 도출하여 초기설계 단계에서 최적 프로펠러 직경등을 쉽게 결정할 수 있게 하였다. 기준으로 선택된 반류분포(2700TEU 콘테이너선의 반류) 후류에서 프로펠러 추력계수 및 캐비테이션 수를 체계적으로 변화시킨 상태에서 캐비테이션 관찰시험 및 변동압력계측시험을 수행하였다. 양력면이론에 의한 비정상 프로펠러 성능해석에 의해 계산된 최대 국부양력계수 ($C^{max}_{l,0.8R}$)와 국부캐비테이션 수(${\sigma}_0=\frac{p-p_v}{\frac{1}{2}{\rho}V^2_{0.8R}}$)를 기준으로 캐비테이션 관찰시험 결과를 정리하여 KD-캐비테이션 챠트를 도출하였다. 기존의 캐비테이션 챠트는 균일류중의 시험 결과를 정리하여 작성되었으나 KD-캐비테이션 챠트는 반류분포중에서 시험된 프로펠러 관찰시험 결과로 부터 도출되었으므로 초기설계 단계에서 보다 정확한 캐비테이션 발생량 추정이 가능하리라 예상된다.

• Ocean Systems Engineering
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• 제1권4호
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• pp.285-296
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• 2011

Spar platforms have several advantages for deploying wind turbines in offshore for depth beyond 120 m. The merit of spar platform is large range of topside payloads, favourable motions compared to other floating structures and minimum hull/deck interface. The main objective of this paper is to present the response analysis of the slack moored spar platform supporting 5MW wind turbine with bottom keel plates in regular and random waves, studied experimentally and numerically. A 1:100 scale model of the spar with sparD, sparCD and sparSD configuration was studied in the wave basin ($30{\times}30{\times}3m$) in Ocean engineering department in IIT Madras. In present study the effect of wind loading, blade dynamics and control, and tower elasticity are not considered. This paper presents the details of the studies carried out on a 16 m diameter and 100 m long spar buoy supporting a 90 m tall 5 MW wind turbine with 3600 kN weight of Nacelle and Rotor and 3500 kN weight of tower. The weight of the ballast and the draft of the spar are adjusted in such a way to keep the centre of gravity below the centre of buoyancy. The mooring lines are divided into four groups, each of which has four lines. The studies were carried out in regular and random waves. The operational significant wave height of 2.5 m and 10 s wave period and survival significant wave height of 6 m and 18 s wave period in 300 m water depth are considered. The wind speed corresponding to the operational wave height is about 22 knots and this wind speed is considered to be operating wind speed for turbines. The heave and surge accelerations at the top of spar platform were measured and are used for calculating the response. The geometric modeling of spar was carried out using Multisurf and this was directly exported to WAMIT for subsequent hydrodynamic and mooring system analysis. The numerical results were compared with experimental results and the comparison was found to be good. Parametric study was carried out to find out the effect of shape, size and spacing of keel plate and from the results obtained from present work ,it is recommended to use circular keel plate instead of square plate.