• Journal of the Korea institute for structural maintenance and inspection
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• v.23 no.3
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• pp.150-159
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• 2019

The bond analysis model equation was proposed through the regression analysis of the experimental values of bond behavior for each rebar. In order to verify the appropriateness of the bond analysis model equation, the bond behaviors calculated by the proposed bond analysis model, BPE model and CMR model were compared with experimental values. The proposed bond model showed the closest behavior to the experimental values when compared to other analysis models. The former models can not consider the different properties of GFRP rebar according to composed materials, mixing and manufacturing method and the latter has limitation to express the relationships between bond behavior because of derived formula by numerical analysis. This study proposed the analytical model different considering bond mechanism according to surface type. In order to verity the appropriateness of the bond analytical model, the bond behaviors calculated by the proposed bond analytical model, BPE model and CMR model were compared with experimental values. The proposed bond model showed the closest behavior to the experimental values when compared to other analysis models.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2010.11a
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• pp.271-275
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• 2010

Forming tool design is carried out for a manufacturing a outer shell structure of the nozzle extension of regenerative cooling thrust chamber. The method which manufactures outer shell structure of nozzle extension is a metal forming process using thin plate. Because the configuration of outer shell structure is changed after forming process by springback effect, the outer shell structure can't be exactly formed with the same forming tool as configuration of the nozzle extension. Therefore forming tool design considering springback effect is necessary for manufacturing the outer shell structure of the nozzle extension. In this study, new designed forming tool configuration was generated to decrease the errors between nozzle contour and formed structure. The analysis results show that the errors between nozzle contour and formed structure is significantly decreased using the new designed forming tool.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.43 no.10
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• pp.896-901
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• 2015

The skin-frame type structure is designed to investigate the thermal deformation of the wing skin induced by the temperature gradient. In order to effectively simulate the temperature gradient on the wing specimen, a water cooling system is devised on the frame of the specimen. Out of surface skin deformation of the skin-frame type structure made of SUS304 material with respect to the temperature is successfully measured using the digital image correlation (DIC) technique including quantitative evaluation of the measurement uncertainty.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.44 no.7
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• pp.562-567
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• 2016

Morphing wing which has a configuration optimized to flight speed and condition is faced to a lot of barriers to be overcome such as actuator technique, structural mechanization technique, flexible skin material, control law, and so on. As the first step for developing a morphing wing with rapid response, we designed and fabricated the morphing airfoil using a SMA(shape memory alloy) wire actuator and torsional bias springs. The design concept of the morphing airfoil was verified through operation test. The measured results show that the flap deflects smoothly and fast.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.19 no.9
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• pp.333-340
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• 2018

Recently, free-form buildings have been designed with complex shapes due to digitization of the construction industry. Exterior and interior components of free-form buildings have free cross sections and curved shapes. Therefore, structural members with curvature are frequently seen. In the modeling and stability evaluation of these structures, commercial programs using classical finite element analysis are not able to perform rapid shape modeling, resulting in a decrease in productivity. Therefore, in this study, pre- and post-processing modules were developed using a prior study to rapidly model the surface of a free-form building and to automatically generate frame structures that make up the cladding. The developed modules use a subdivision algorithm with spline curves. This algorithm is used to automatically generate analytical elements from the configuration information of NURBS curves. In addition, the deformation after analysis can be viewed more realistically. The modules can quickly construct complex curved surfaces. An analysis model of the frame structure was also automatically generated. Therefore, the modules could contribute to the productivity improvement of free-form building design.

• Composites Research
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• v.18 no.1
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• pp.30-37
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• 2005

The bending strength characteristics and local deformation behaviors of honeycomb sandwich composites were investigated using three-point bending experiment and finite element simulation with a real model of honeycomb core. Two kinds of cell sizes of honeycomb core, two kinds of skin layer thicknesses, perfect bonding specimen as well as initial delamination specimen were used for analysis of stress and deformation behaviors of honeycomb sandwich beams. Various failure modes such as skin layer yielding, interfacial delamination, core shear deformation and local buckling were considered. Its simulation results were very comparable to the experimental ones. Consequently, cell size of honeycomb core and skin layer thickness had dominant effects on the bending strength and deformation behaviors of honeycomb sandwich composites. Specimens of large core cell size and thin skin layer showed that bending strength decreased by $30\~68\%$.

• Korean Journal of Air-Conditioning and Refrigeration Engineering
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• v.8 no.4
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• pp.497-509
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• 1996

Evacuated powder insulations have long been known to have better thermal performance than existing commercially available insulators, such as fiber glass and CFC-blown foam. To make a composite powder panel, a series of individually evacuated panels was encapsulated in a rigid closed cell foam matrix. The panels were encapsulated in a thin glass sheet barrier to preserve the vacuum. The thermal conductivity of the individual panel was found to be $0.0062W/m^{\circ}K$ by experiment and the polyurethane foam above had a thermal conductivity of $0.024W/m^{\circ}K$. In this study, numerical analysis using finite element method was carried out to investigate insulation performance of rigid foam/evacuated powder composite panel with respect to panel geometries such as panel pitch, panel aspect ratio and panel area ratio. Numerical analysis has indicated that more optimal vacuum panel geometries, much lower overall thermal conductivities can be achieved.

• Proceedings of the IEEK Conference
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• 2001.09a
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• pp.705-708
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• 2001

여러 장의 입력 영상으로부터 3차원 형상 정보를 복원하는 기법은 크게 스테레오(stereo) 기법과 각선 기반 방법으로 나누어져 있다. 특히 복셀 기반 방법은 스테레오 기법에서의 대응점 문제를 극복하고 가리어짐 현상이나 컬러의 변화가 적은 영역에서의 현상 복원 능력이 우수한 것으로 알려져 있지만 광학적 외피(photo hull) 이라는 근본적인 복원 한계성을 가진다. Photo hull은 바라보는 카메라의 위치에 크게 의존하는 성질을 보인다. 조건에 맞는 최적의 카메라 위치를 결정하는 것을 시점 계획(view planning)이라 고 하고 거리 영상(range images)로부터 형상을 복원하는 기법에 활발히 연구되어져 왔다. 본 논문에서는 복셀 기반 방법에서의 단점인 photo hull을 줄이기 위해 최적의 시점을 선택하는 시점 계획(view planning)에 대한 알고리듬을 제안하고 photo hull의 효과를 최소로 하여 형상이 복원되는 것을 실험을 통해 검증한다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2000.04a
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• pp.36-36
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• 2000

액체로켓엔진에 사용되는 2000psi이상의 고압 연소실(Combustion Chamber)의 냉각은 내피(Inner Shell)에 기계 가공된 냉각통로(Cooling Channel)로 냉각제를 흘려보내는 재생냉각방식이 널리 사용되며 기계 가공된 냉각 통로는 외피(Outer Shell)에 의해서 지지 밀봉된다. 일반적으로 내피 재료는 순수한 구리보다 강도가 우수하고 열전도도는 유사한 구리합금을 사용하고, 외피는 강도가 우수한 스테인레스 강을 사용하여 브레이징 접합된 구조를 형성한다. 브레이징 공정은 조립품을 약 $450^{\cire}C$ 이상의 액상선을 갖는 삽입금속(Filler Metal)을 사용하여 적당한 온도($450^{\cire}C$ ~ 모재의 고상선)에서 가열하여 접합시키는 방법으로, 용융 금속의 젖음 현상(Wetting Phenomena), 접합 틈새(Joint Clearance)로의 용융 삽입금속의 유입(Capillary Phenomena)과 접합 계면의 반응을 통해서 접합이 이루어진다. 이는 일반적인 접합 공정과 비교하여 모재의 변형이 적고, 이종 금속 간의 접합이 용이하며, 복잡한 부품을 정밀하게 접합할 수 있는 장점이 있으나, 접합될 제품의 표면 상태 및 분위기(Atmosphere), 접합될 부품간의 조립 틈새, 가열 싸이클(Heating Cycle) 등에 대한 공정 확립 및 관리가 매우 중요하다. 재생냉각 구조를 갖는 연소실은 우선 접합면의 형상이 매우 복잡하여 균일한 접합 틈새를 유지하면서 접합시키기가 매우 어려우며, 고온, 고압의 환경에서 작동하므로 일부 접합면이 접합되지 않을 경우 내피의 변형 및 파괴가 발생하고, 브레이징 시 용융된 삽입금속이 냉각통로 내로 유입될 경우 연소 시 이부근에서 재료의 용융이 발생될 수 있다. 따라서, 이러한 현상을 방지하기 위해서는 진공 분위기 하에서 적절한 접합 틈새를 유지할 수 있는 공정 및 장비의 개발이 필요하다.

• 한국태양에너지학회:학술대회논문집
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• 2009.11a
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• pp.142-147
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• 2009

In order to achieve performance assessment and optimal control of a double-skin system, an accurate simulation model is required. In the previous study, a lumped simulation model of such system was developed. As a follow-up of the previous research, the first objective of this paper is to investigate how the mathematical model should be calibrated according to system configuration(cavity width, depth, height, airflow pattern, local environment, etc.). And the second objective of this study is to discuss the effect of local weather information. In conclusion, this paper describes that the model should be recalibrated according to configuration. And it is necessary to have local weather information for accurate prediction and optimal control of the system.