• 한국추진공학회지
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• 제8권1호
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• pp.70-80
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• 2004

본 연구에서는 한국과 같이 비교적 저 풍속인 지역에 적용 가능하도록 피치제어장치를 가진 1kW급 소형 풍력발전 시스템의 개발 결과를 제시하였다. 공력설계에서는 블레이드의 직경이 동급의 상용 블레이드 보다 과도하게 크지 않으면서도 저 풍속 지역에서 보다 효율적인 형상설계를 위해 여러 가지 설계 변수분석을 통한 파라미터 연구가 수행되었다. 또한 구조설계를 통해 풍력발전기에 작용하는 다양한 하중을 효과적으로 견딜 수 있는 경량의 복합재 구조가 설계되었다. 구조설계의 평가를 위해 유한요소 구조해석이 수행되었으며, 실물 구조시험을 수행하여 구조적 안전성을 확인하였다.

• 대한조선학회논문집
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• 제35권2호
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• pp.94-103
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• 1998

최근 선박의 고속화와 경량화가 중요시되면서 고속화에 적합한 선형과 경량화를 위한 재질의 연구가 활발히 진행되고 있다. 따라서 본 논문에서는 고속화와 경량화에 적합한 복합재료를 이용한 쌍동형 초고속선의 최소 중량 설계를 위한 구조 설계 기법과 전산 프로그램을 개발하였다. 또한 개발된 프로그램을 이용하여 복합재료의 대표적인 구조 형식인 샌드위치 형식과 Single skin 형식, 두가지가 혼용되는 Hybrid 형식에 대하여 각각 최적 설계를 수행하여 우열을 비교 검토하였다. 설계과정은 먼저 종강도 관점에서 주요 부재의 최적 설계를 수행하고, 쌍동선형 특유의 비틀림 모멘트를 고려하여 횡부재 설계를 수행하였다. 전체적인 설계 알고리즘은 미해군의 군함설계방법(Structural Synthesis Design Program)을 따르고 설계하중, 강도기준은 DnV 선급규정을 적용하였으며, 최적화 알고리즘은 ES 1+1을 사용하였다.

• 한국유체기계학회 논문집
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• 제15권6호
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• pp.11-17
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• 2012

The one way fluid structure interaction analysis on advanced propeller blade for next generation turboprop aircraft. HS1 airfoil series are selected as a advanced propeller blade airfoil. Adkins method is used for aerodynamic design and performance analysis with respect to the design point. Adkins method is based on the vortex-blade element theory which design the propeller to satisfy the condition for minimum energy loss. propeller geometry is generated by varying chord length and pitch angle at design point. Blade sweep is designed based on the design mach number and target propulsion efficiency. The aerodynamic characteristics of the designed Advanced propeller were verified by CFD(Computational Fluid Dynamic) and showed the enhanced performance than the conventional propeller. The skin-foam sandwich structural type is adopted for blade. The high stiffness, strength carbon/epoxy composite material is used for the skin and PMI(Polymethacrylimide) is used for the foam. Aerodynamic load is calculated by computational fluid dynamics. Linear static stress analysis is performed by finite element analysis code MSC.NASTRAN in order to investigate the structural safety. The result of structural analysis showed that the design has sufficient structural safety. It was concluded that structural safety assessment should incorporate the off-design points.

• 복합신소재구조학회 논문집
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• 제2권3호
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• pp.12-17
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• 2011

본 논문은 노후교량바닥판 대체용으로서 하이브리드 GFRP-강재 바닥판의 휨거동을 구조적 거동특성을 기술하고 있다. 하이브리드 GFRP-강재 바닥판의 구조적 특성을 조사하기 위해 정적하중의 실험적 연구를 수행하였다. 하이브리드 바닥판의 파괴모드는 초기항복을 지나서 연성거동을 나타내었다. 결과는 유한요소프로그램 ANSYS의 값과 비교하였다. 제안된 하이브리드 바닥판이 교량적용에 유용함을 확인하였다. 하이브리드 바닥판의 두께는 유사한 휨 강성을 갖는 완전복합신소재 바닥판께와 비교하였을 때 감소될 수 있었다.

• Steel and Composite Structures
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• 제33권3호
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• pp.333-346
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• 2019

Foam ceramic materials contribute to the explosion effect weakening on concrete structures, due to the corresponding excellent energy absorption ability. The blast resistance of concrete members could be improved through steel-foam ceramics as protective cladding layers. An approach for the modeling of dynamic response of steel-foam ceramic protected reinforced concrete (Steel-FC-RC) slabs under blast loading was presented with the LS-DYNA software. The orthogonal analysis (five factors with five levels) under three degrees of blast loads was conducted. The influence rankings and trend laws were further analyzed. The dynamic displacement of the slab bottom was significantly reduced by increasing the thickness of steel plate, foam ceramic and RC slab, while the displacement decreased slightly as the steel yield strength and the compressive strength of concrete increased. However, the optimized efficiency of blast resistance decreases with factors increase to higher level. Moreover, an efficient design method was reported based on the orthogonal analysis.

• Steel and Composite Structures
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• 제32권5호
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• pp.671-686
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• 2019

Active control of solar panels with honeycomb core and carbon nanotube reinforced composite (CNTRC) facesheets for smart structures using piezoelectric patch sensor and actuator to reduce the amplitude of vibration is a lack of the previous study and it is the novelty of this research. Of active control elements are piezoelectric patches which act as sensors and actuators in many systems. Their low power consumption is worth mentioning. Thus, deriving a simple and efficient model of piezoelectric patch's elastic, electrical, and elastoelectric properties would be of much significance. In the present study, first, to reduce vibrations in composite plates reinforced by carbon nanotubes, motion equations were obtained by the extended rule of mixture. Second, to simulate the equations of the system, up to 36 mode shape vectors were considered so that the stress strain behavior of the panel and extent of displacement are thoroughly evaluated. Then, to have a more acceptable analysis, the effects of external disturbances (Aerodynamic forces) and lumped mass are investigated on the stability of the system. Finally, elastoelectric effects are examined in piezoelectric patches. The results of the present research can be used for micro-vibration suppression in satellites such as solar panels, space telescopes, and interferometers and also to optimize active control panel for various applications.

• Steel and Composite Structures
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• 제31권2호
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• pp.133-148
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• 2019

This paper reports on the energy absorption characteristics of a lattice-web reinforced composite sandwich cylinder (LRCSC) which is composed of glass fiber reinforced polymer (GFRP) face sheets, GFRP lattice webs, polyurethane (PU) foam and ceramsite filler. Quasi-static compression experiments on the LRCSC manufactured by a vacuum assisted resin infusion process (VARIP) were performed to demonstrate the feasibility of the proposed cylinders. Compared with the cylinders without lattice webs, a maximum increase in the ultimate elastic load of the lattice-web reinforced cylinders of approximately 928% can be obtained. Moreover, due to the use of ceramsite filler, the energy absorption was increased by 662%. Several numerical simulations using ANSYS/LS-DYNA were conducted to parametrically investigate the effects of the number of longitudinal lattice webs, the number of transverse lattice webs, and the thickness of the transverse lattice web and GFRP face sheet. The effectiveness and feasibility of the numerical model were verified by a series of experimental results. The numerical results demonstrated that a larger number of thicker transverse lattice webs can significantly enhance the ultimate elastic load and initial stiffness. Moreover, the ultimate elastic load and initial stiffness were hardly affected by the number of longitudinal lattice webs.

• 한국항공우주학회지
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• 제47권5호
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• pp.319-325
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• 2019

본 논문의 목적은 항공기에 장착되는 복합재 라미네이트 및 샌드위치구조를 가지는 레이돔에 대한 조류충돌해석을 수행하고 해석결과와 시험결과를 비교 및 분석하기 위함이다. 먼저 SPH(Smoothed Particle Hydrodynamics)법을 통해 물의 특성을 가지는 조류를 모델링하였으며, 조류충돌시험을 통해 조류가 충돌할 때의 속도를 입력하여 조류충돌해석을 수행하였다. 해석결과를 통해 레이돔의 파손 여부를 조사하고 최대 변형량을 시험결과와 비교하였으며 충돌과정에서의 압력변화추이가 기 연구되었던 결과와 일치함을 확인하였고, 이를 통해 수치해석모델의 신뢰성을 확보하였다. 또한 조류모델을 이루는 입자의 밀도가 레이돔의 파손 형상에 영향을 미친다는 사실을 확인하였다.

• Composites Research
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• 제22권3호
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• pp.55-59
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• 2009

마이크로스트림 안테나는 가볍고 부피가 작을 뿐만 아니라 집적화가 가능하고, 표면 부착력이 탁월하여 많은 통신 시스템 안테나로 응용되고 있다. 안테나의 구조는 12.5GHz의 중심주파수를 갖는 사각 패치 마이크로 스트립 안테나로 설계하였고 곡률 방향으로 패치를 확장시켜 총 4개의 패치를 배열시켰다. 양쪽의 복합재료 사이에 허니컴을 삽입한 샌드위치 구조물이 되도록 설계한 다음 충격 실험을 실시하였다. 충격실험 후 안테나 성능변화를 측정한 결과 영향을 받지 않는다는 것을 확인하였다.

• Advances in aircraft and spacecraft science
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• 제10권4호
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• pp.347-368
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• 2023

In the first part of this study, a numerical simulation model was developed using the mechanical APDL software to validate the results of the 3D-elastisity theory on the laminated sandwich plate developed by Panago. The numerical simulation model showed a good agreement to the results of Pagano's theory in terms of deflection, normal stresses, and shear stresses. In the second part of this study, the developed numerical simulation model was used to define different plates dimensions and fibers layup orientations to examine the load response in terms of deflection and stresses. Further analysis was implemented on the natural frequencies of laminated xxx plates of the plates. The layup configurations include Unidirectional (UD), Cross-Ply (CP), Quasi-Isotropic (QI), the linear bio-inspired known as Linear-Helicoidal (LH), and the nonlinear bio-inspired known as Fibonacci-Helicoidal (FH). The following numerical simulation model can be used for the design and study of novel, sophisticated bio-inspired composite structures in a variety of configurations subjected to sinusoidal or constant loads.