• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.50 no.6
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• pp.377-384
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• 2022

In the design of composite aircraft structures, it is very important to set material allowables and design values, which take into account certification. And when determining the material allowable and design value of composite structures, the static strength, damage tolerance requirements, and environmental effects should be considered. The building block approach has been applied to the civil and military aviation industry for a long time and provides the principal certification methodology. This current certification methodology is based on extensive testing including coupon, element, sub-component, and full scale test. In this paper, some examples of composite allowable tests have been presented and the fundamental background and application methods of the building block approach have been presented.

• Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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• 2002.11a
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• pp.548-550
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• 2002

본 장치는 다층막 스퍼터링 증착장치로써 박막을 증착시키는데 용이하게 설계하는 것이 목적이며, 박막두께가 균일하게 증착되고 진공조 내부의 압력을 일정하게 제어가 가능하고 배기시스템은 스퍼터실과 증착실의 진공배기를 공용으로 구조를 설계하여 장치의 스퍼터링 증착조건에 적합하도록 연구실험용으로 설계되어졌다.

• Composites Research
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• v.26 no.4
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• pp.223-229
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• 2013

Hybrid composite strut tower was designed to prevent permanent deformation of upper mount by the impact from the uneven road. When exceeding energy absorption capacity of tire and suspension systems, residual impact is delivered to upper mount. Especially, in case of using high-rigidity suspension system for high driving performance, the conventional strut tower can be easily deformed due to reduction of energy absorption capacity of suspension systems. In this study, optimal design of hybrid composite strut tower which made of back-up metal and carbon fiber reinforced composite was suggested by using finite element analysis, and low velocity impact test was performed to investigate their dynamic characteristics. Also, 3D measuring and ultra c-scanning methods were carried out to diagnose damages in the strut towers.

• Composites Research
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• v.32 no.2
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• pp.108-112
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• 2019

There has been a continuous study on the weight reduction of structure by composites. Unlike isotropic materials, the physical properties of composites vary according to the direction of laminate and the order of lamination. Therefore, in the case of composite ladders, it is essential to perform structural analysis to verify the planned design. In this study, ladder was designed by applying fabric material. In addition, the effect of loading position on the ladder was analyzed through finite element analysis, and structural performance was analyzed by selecting the most problematic location. We analyzed the effect of stacking order on the structural strength of the ladder by analyzing the structure by applying various stacking sequence and measuring the failure value in each layer.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2000.06a
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• pp.1268-1272
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• 2000

본, 논문에서는 카본/에폭시, PZT 세라믹 박판, 글래스/에폭시 층으로 이루어진 곡면형 복합재료 작동기(LIPCA)의 설계, 제작 및 성능실험에 대한 연구 성과를 제시하고 있다. LIPCA의 큰 요점은 기존 THUNDER의 성능을 유지하면서 이를 경량화 하기 위하여 THUNDER의 금속 층을 상대적으로 가벼운 섬유 강화 복합재료로 대체하는 것이다. 이러한 경량화 작업으로 LIPCA는 기존 THUNDER 보다 약 $30{\sim}40%$ 정도의 무게를 감소시킬 수 있으며, 복합재료의 특성에 따라 설계의 유연성을 가질 수 있는 장점이 있다. 또한, 에폭시 수지를 사용함으로써 접착제 없이 평판 몰드에서 오토클레이브에서 $177^{\circ}C$로 경화되어, 탈형된 후 충분한 곡률을 형성하였다. 작동 성능 실험에서, LIPCA는 기존 THUNDER보다 작동변위가 향상됨을 보였다.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.30 no.4A
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• pp.383-389
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• 2010

The concrete structural design provisions in Korea are based on ultimate strength design. Up to service load stage, it is assumed a linear stress-strain relation, but there is no stress-strain relationship for a concrete material from service load stage to limat state. According to the current provisions, an independent method is provided for the each calculation of deflection and crack width. In EC2 provisions based on limit state design, however, a stress-strain relationship of concrete is provided. Thereby, it is able to calculate a strength as well as a deflection directly from concrete stress-strain relationship. In this paper the moment-curvature relationship is directly calculated from a material law using equilibrium and compatibility conditions. Then strength and deflection are formulated. These results are compared with the values from the current provisions in Korea. From the results, the deflection based on a moment-curvature relationship is well agreed with experimental results and it is appeared that the deflection after the yielding of steel is also possible.

• Defense and Technology
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• no.10 s.260
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• pp.54-65
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• 2000

무기체계에 소요되는 재료개발은 고도로 경험적이고 그와 관련된 재료 시험은 적용 무기 체계와는 무관하게 독립적으로 이뤄져야 하며, 또한 기존의 재료 모델과 서로 연관성을 짓는다는 것이 어렵다. 반면, 재료가 적용될 체계의 설계는 고도의 계산에 의해 이뤄지며, 그 시험 과정도 아주 잘 확립되어 있다. 이러한 이유로 신 재료개발은 시급히 요구되는 체계 개발에 앞서 이루어지지 않으면 안된다.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.13 no.4
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• pp.15-25
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• 1993

In order to promote the efficient use of composite materials, effort is currently being directed at the development of design criteria for composite structures. Insofar as design against buckling is concerned, it is well known that, for metal shells, a key step is the definition of 'knockdown' factors on the elastic critical buckling stress accounting mainly for the influence of initial geometric imperfections. At present, the imperfection sensitivity of composite shells has not been explored in detail. Due to the large number of parameters influencing buckling response (considerably larger than for isotropic shells), a very large number of tests would be needed to quantify imperfection sensitivity experimentally. An alternative approach is to use validated numerical models for this task. Thus, the objective of this paper is to outline the underlying theory used in developing a composite shell element and to present results from a validation exercise and subsequently from a parametric study on axially loaded glass fibre-reinforced plastic (GFRP) curved panels using finite element modelling. Both eigenvalue and incremental analyses are performed, the latter including the effect of initial geometric imperfection shape and amplitude, and the results are used to estimate 'knockdown' factors for such panels.

• Journal of the KSME
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• v.18 no.1
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• pp.34-41
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• 1978

일반적으로 피로파괴의 사고원인으로는 무적합한 설계재질의 불량, 공작 및 기계조작의 미스등이 있다. 어떤 기계에 대한 파괴원인규명이 확실할 경우에는 그 대책도 쉽게 강구되지만, 원인규명이 불확실한 경우에는 매우 어렵게 된다. 만일 어떤 기계에 대하여 사고의 원인이 될만한 제인자들 에 대한 보완이 잘되어 있다고 하더라도 파괴가 일어 났다고 하자, 그러면 설계자는 안전설계를 하였는가또는 파괴에 대한 대책을 어떻게 강구하는게 좋을 것인가 하는 문제로서 고심하게 된다. 이러한 경우, 먼저 생각할 수 있는 것은 사용재료의 선택 및 가공 또는 열처리가 제대로 되었다 고 하더라도 피로강도에는 Scattering현상이 발생한다는 것을 고려하는 것이 좋겠다. 이러한 경우 설계자는 Scattering을 충분히 고려하여 파괴가 일어나지 않는 설계를 할 필요가 있고, 설계개선 에 따라서 미지의 Scattering을 보완할 수 있는 문제를 생각할 수 있어야 할 것이다. 그렇기 때 문에 설계자는 특히 피로강도에 관한 충분한 지식을 가지고 강도에 대한 Scattering에 대해서도 경험을 쌓고 새로운 자료 에 관심을 기울려 피로파괴방지에 노력하는 것이 좋을 것이다. 따라서 본 원고에서는 독자 제현께서 이미 알고 있으리라 믿어지는 내용을 간추려 보기로 하였고, 내용 별로 는 (1) 설계의 본찰, (2) 재료의 선택과 열처리, (3) 피로지동에 영향을 주는 열처리의 제인 지, (4) 피로파괴와 설계, (5) 안전설계, (6) 신뢰성과 안전성등에 대하여 기술하여 보겠다.

• The Journal of Korean Institute of Electromagnetic Engineering and Science
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• v.12 no.6
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• pp.1002-1008
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• 2001

The absorbing structure composed of multi-layered fiber reinforced composite materials was designed and microwave absorbing properties are investigated. On the basis of transmission line theory, the theoretical equations to predict the reflection loss and the appropriate composite material for each functional layer are suggested. The most significant result of this study is the successful design and fabrication of triple-layered composite laminates which has the superior microwave absorbing porperties (more than 10 dB in 4∼12 GHz range), without using the ferrite filler in the impedance transforming layer. In the two-layered composite laminate (absorber/substrate), however, the use of ferrite filler (about 40 wt %) in the absorbing layer is necessary to obtain the certain level of microwave absorbance. By combining the glass-fiber composite with ferrite filler and carbon-fiber composite substrate, the microwave absorbing properties more than 10 dB in 4∼12 GHz frequencies than be obtained.