• Composites Research
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• v.23 no.6
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• pp.47-54
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• 2010

Thermal vibration characteristics of a thin walled composite beam attached on spacecraft are investigated in this paper. The composite beam is assumed to have a thin CUS(circumferentially uniform stiffness) wall and modeled with several composite materials which are already space qualified such as T300/Epoxy, YS90AEpoxy. Steady state angle and peak to peak error in spacecraft attitude angle and tip displacement of composite beams are evaluated as a performance index for thermal vibration characteristics. Evaluation results shows that composite beam made out of YS90A has nearly 2 times better than T300 in terms of peak to peak attitude error angle.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.33 no.7
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• pp.26-32
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• 2005

In this paper, the vibration response of the spacecraft solar array is investigated. The solar array model consists of composite thin walled beam and solar blanket, spreader bar. The composite thin walled beam incorporates a number of nonclassical effects of transverse shear, primary and secondary warping, rotary inertia and anisotropy of constituent materials. The solar blanket is a membrane subjected to uniform tension in the z direction. The spreader bar is a rigid member. A coupled thermal structure analysis that includes the effects of structural deformations on heating and temperature gradient is investigated. A stability criterion given in parameters for establishes the conditions for thermal flutter.

• Journal of Korean Society of Steel Construction
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• v.18 no.4
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• pp.457-468
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• 2006

An experimental study was performed to investigate the maximum energy dissipation and the ductility capacity of shear-dominated steel plate walls with thin web plates. Three specimens of three-story plate walls with thin web plates were tested. The parameters for the test specimens were the aspect ratio of the web plate and the shear strength of the column. A concentrically braced frame and a moment-resisting frme were a also tested for comparison. The steel plate walls exhibited much better ductility and energy dissipation capacity than the concentrically braced frame and the moment-resisting frame. The results showed that unlike other structural systems, the sh as well as strength, and can therefore be used as an effective earthquake-resisting system. A method of predicting the energy dissipation capacity of a steel plate wall was proposed.

• Aerospace Engineering and Technology
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• v.8 no.2
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• pp.149-159
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• 2009

This paper deals with an analytical study on the aileron reversal characteristics of anisotropic composite aircraft wings modelled as thin-walled beam and having extension-twist structural couplings caused by Circumferentially Uniform Stiffness (CUS) layup scheme. For a study on the aileron reversal of CUS composite wings, it is essential to consider the following effects such as extension-twist structural coupling, wing aspect ratio, and ratio of span-wise and chord-wise length of aileron to wing, initial angle of attack, and sweep angle, etc. The results on the aileron reversal could have a significant role in more efficient designs of thin-walled composite wing aircraft for which this aeroelastic instability is one of the most critical ones.

• Journal of the Korean Society of Manufacturing Process Engineers
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• v.20 no.11
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• pp.52-59
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• 2021

Titanium alloy (Ti-alloy) is widely used as a material for core parts of aircraft structures and engines that require both lightweight and heat-resistant properties owing to their high specific stiffness. Most parts used in aircraft have I-, L-, and H-shaped thin-walled structures for weight reduction. It is difficult to machine thin-walled structures owing to vibrations and deformations during machining. In particular, cutting tool damage occurs in the corners of thin-walled structures owing to the rapid increase in cutting force and vibration, and machining quality deteriorates because of deep tool marks on machined surfaces. In this study, milling experiments were performed to derive an effective method for machining a L-shaped thin-walled structure with Ti-alloy (Ti-6Al-4V). Three types of machining experiment were performed. The surface quality, tool wear, cutting force, and vibration were analyzed comprehensively, and an effective machining method in terms of tool life and machining quality was derived.

• Journal of Biomedical Engineering Research
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• v.20 no.5
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• pp.593-599
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• 1999

수축절정기에 0.2mm, 0.4mm 두께의 소구경 인조혈관의 내경3.2mm의 동맥에 문합한 단단문합 주위의 유동과 구조해석을 동시에 수행하였다. 유동해석 결과 속도분포 및 벽단전률은 타 연구결과와 매우 유사하며 이론해와 매우 유사함을 보였다. 유동에 의해서 문합부 주위에 작용하는 응력은 문합부에 집중되며 이는 수십만 pa에 달했다. 또한 인조혈관과 동맥에 작용하는 원주방향의 응력을 이론해와 비교한 결과 서로 유사함을 보였으며 두께가 얇은 인조혈관을 사용하는 경우 문합부의 compliance mismatch 는 개선되나 반대로 응력은 더 많이 받음을 알 수 있었다. 본 연구를 통해서 유체에 의하여 혈관이 영향을 받는 심혈관계 현상을 연구하는데 있어서 이와 같은 유체-구조 상호작용을 고려하여 동시에 해결 하는 방법은 매우 유용할 것으로 생각된다.

• Journal of the Korean Society of Manufacturing Process Engineers
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• v.21 no.6
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• pp.81-88
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• 2022

Titanium alloy (Ti-6Al-4V) has excellent mechanical properties and high specific strength; therefore, it is widely used in aerospace, automobile, defense, engine parts, and bio fields. Particularly in the aerospace field, as it has a low specific gravity and rigidity, it is used for the purpose of increasing energy efficiency through weight reduction of parts, and most have a thin-walled structure. However, it is extremely difficult to machine thin-walled shapes owing to vibration and deformation. In the case of thin-walled structures, the cutting forces and vibrations rapidly increase depending on the cutting conditions, significantly affecting the surface integrity and tool life. In this study, machining experiments on thin-wall milling of a titanium alloy (Ti-6Al-4V) were conducted for each experimental condition with different axial depths of cut, radial depth of cut, and machining sequence. The machining characteristics were analyzed, and an effective machining method was derived by a comprehensive analysis of the machined surface conditions and cutting signals.

• Journal of Aerospace System Engineering
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• v.3 no.2
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• pp.1-11
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• 2009

A structural modelling for study on dynamic characteristics of tapered composite aircraft wings in the form of thin-walled beam is presented. The proposed structural model includes effects of transverse shear flexibility exhibited by the advanced composite materials and warping restraint characterizing elastic anisotropy and induced structural couplings. The complex effects of these factors could have a role in more efficient analysis on those structural models.

• Journal of Korean Society of Steel Construction
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• v.16 no.6 s.73
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• pp.781-792
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• 2004

Experiments were performed to study the cyclic behavior of framed steel walls with thin web plates. Five specimens of single-bay and three-story steel plate walls were tested for cyclic lateral load. The parameters for the test specimens included the plate thickness and the column strength. Based on the test results, the strength, deformability, and energy dissipation capacity of the framed steel walls were studied. The test results showed that the behavioral characteristics of the framed steel walls with thin web plates were different in many aspects from those of the conventional braced frame, and the steel wall with a stiffened web plate exhibited cantilever action, high strength, and low ductility. With the framed steel plate walls, local plate buckling and tension-field action developed in the thin web plates, and plastic deformation was uniformly distributed along the wall's height. As a result, the framed steel plate walls exhibited combined flexural and shear deformation, but they also showed high strength and energy dissipation capacity. Moreover, such walls have high deformability, which was equivalent to that of the conventional moment frame. Frame members such as columns and beams, however, must be designed to resist the tension-field action of the thin web plates. If the column does not have sufficient strength, and if its sections are not compact enough, the overall strength of the framed steel wall might be significantly decreased by the development of the soft-story mechanism. The framed steel walls with thin web plates have advantages, such as high deformability and high strength. Therefore, they can be used as ductile elements in earthquake-resistant systems.

• The Korean Journal of Malacology
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• v.8 no.1
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• pp.61-71
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• 1992

동양달팽이 (Nesiohelix samarangae)는 동양달팽이속(Nesiohelix)에 속하는 종으로 한국에서 동양？팽이속으로는 유일하게 발견되는 종이다. 본 실험에서는 동양달팽이의 웅성생식기관의 각 부분 즉, 난정소(ovotestis), 양성관(hermaphrodite duct), 수정실(fertilization chamber), 전립선(prostate), 수정관(vas deferens), 상음경(epiphallus), 음경(penis)등의 배열 상태를 관찰하고 이들에 대한 광학현미경적 관찰을 위해 Hematoxylin- Eosin염색과 Mallory 염색을 실시하였다. 난정소(ovotestis)는 많은 수의 선포(acini)로 이루어져 있으며 각 선포는 배상피세포층(germinal epithelial cell layer)과 영양세포(nurse cell), 생식세포(gamete cell)들로 이루어져 있었다. 선포(acini)는 원주상피로 덮여있었다. 양성관(hermaphrodite duct)은 가늘고 긴 관으로 내벽은 섬모입방상피세포와 얇은 결합조직층으로 이루어져 있었으며 내강은 농축된 정자로 가득 차 있었다 . 수정관(fertilization chamber)은 3개의 도관이 결합조직에 의해 둘러싸인 형태로 이루어져 있었다. 도관의 상피세포는 뚜렷한 위중층섬모원주세포로 되어 있었다. 전립선(prostaoe)은 분비기능을 가진 것으로 사료되는 세포들과 실제 분비가 일어나는 실(chamber)로 이루어져 있었으나 다른 염색법 또는 전자현미경적 관찰에 의해 다른 구조들의 존재유무를 확인 해야할 것으로 사료된다. 실(chamber)은 분비포로 보이는 세포들과 접해 있었다. 수정관(vas deferens)은 결합조직으로 이루어진 근육질의 두꺼운 벽을 가지고 있었으며 내강은 돌출부위에 의해 4부분으로 갈라져 있었다. 내강에 연한 상피는 원주세포로 되어 있었다. 상음경(epiphallus)의 벽은 근섬유 다발은 벽의 외곽으로 갈수록 밀도가 높아졌다. 상부에 내강과 연결되는 함입구조(groove)를 가지며, 내강에 연한 상피는 섬모가 없는 원주세포로 이루어져 있었다. 음경(penis)은 근섬유가 산재된 두꺼운 벽을 가졌으며 상음경보다 굵은 원통형이었다. 내강은 많은 돌출부에 의해 복잡하게 나뉘어 있으며 상피세포는 원주 세포로 이루어져 있었고 섬모는 관찰되지 않았다. 내강 내의 분비물과 세포의 형태로 보아 내강상피세포는 분비기능을 가진 것으로 사료된다.