• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.46 no.12
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• pp.1004-1011
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• 2018

Recently, pyrotechnic separation nut has attracted a considerable attention because of its shock reduction effect among various pyrotechnic mechanical devices. However, its bolt loosening behavior under transverse vibration has not been studied sufficiently, since segmented nuts are utilized instead of conventional nut in pyrotechnic separation nut. With the background, bolt loosening analyses are carried out referring to Junker vibration test. The analysis procedure consists of two steps. The first step is the bolt fastening step, screwing the bolt by fastening torque. The second step is the bolt loosening step under transverse vibration. Through the procedure, bolt loosening behaviors are obtained, and the effect of clearance on loosening behavior is closely investigated for reliable design of pyrotechnic separation nut.

• Korean Journal of Plant Tissue Culture
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• v.22 no.1
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• pp.19-23
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• 1995

Carrot cultured cells are able to respond to a temperature increase by inducing a set of new proteins, heat shock proteins (HSP). Such an induction of the HS gene was known to be achieved mainly at the level of transcription. However there has been an increasing number of evidences showing that a translational control was involved in the regulation of the HS gene expression. A comparison of HSP synthesized in vivo to in vivo (represent for mRNA level since the amount of the proteins produced by in vivo translation system will be proportional to an amount of the corresponding mRNA)showed no correlation between the amount of HS mRNA and the amount of the corresponding HSP at $30^{\circ}C$, It appears that a translational control may exert a major role in the expression of HS gene in carrot callus cells at $30^{\circ}C$.

• Proceedings of the Korean Society For Composite Materials Conference
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• 2005.04a
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• pp.64-66
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• 2005

In order to evaluate impact characteristics for the laminates with or without delaminations, carbon fiber/epoxy laminated composite were fabricated. After trying several ways to develop delaminations within the laminates, an insertion of teflon-tape was found to be most effective. The locations for delamination was determined after several trial-and-error experiments. The low impact energy did not produce measurable difference for composites with or without delamination, which indicated the presence of impact energy threshold. The impact chacteristics for composites with the delamination were found to be different from those for composites with other type of defect including fiber failures.

• Journal of Ocean Engineering and Technology
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• v.16 no.6
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• pp.55-59
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• 2002

Delamination means that cracking occurs on the interface layer between composite laminates. In this paper, to predict the delamination growth in composite laminates subjected to low-velocity impact, the unit load method was introduced, and an eighteen-node 3-D finite element analysis, based on assumed strain mixed formulation, was conducted. Strain energy release rate, necessary to determine the delamination growth, was calculated by using the virtual crack closure technique. The unit load method saves the computation time more than the re-meshing method. The virtual crack closure technique enables the strain energy release rate to be easily calculated, because information of the singular stress field near the crack tip is not required. Hence, the delamination growth in composite laminates that are subjected to low-velocity impact can be efficiently predicted using the above-mentioned methods.

• 한국전산유체공학회:학술대회논문집
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• 2004.10a
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• pp.155-160
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• 2004

This paper describes a supersonic separation of air-launching rocket from the mother plane. Three dimensional Euler equations were numerically solved to analyze steady/unsteady state fluid flows. To solve the Euler equations, named CFD-FASTRAN that is commercial computation code. The results of simulation clearly demonstrate effect of shock-expansion wave interaction between the rocket and the mother plane. Moreover, important influential factors at separating stage of the rocket were extracted with a comprehensive analysis. Finally, from the consideration of supersonic-separation, a guideline to safety-separation is given to the design of supersonic air-launching rocket.

• Proceedings of the KIPE Conference
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• 2018.07a
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• pp.243-245
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• 2018

발사체 및 인공위성에서 발사시부터 우주까지 도달하는데 다양한 환경이 주어진다. 본 논문에서는 발사체의 단분리 및 페어링 분리시 생기는 충격 환경과 대기가 발사체 표면에 충돌하여 생기는 진동 환경에 대한 배터리 내부 변화를 분석한다. 환경시험을 반영한 전기적 모델링을 설계하고 전기적 파라미터를 기반으로 배터리 열해석과 실제 배터리팩 내부 열을 측정하여 비교 및 분석한다.

• Computational Structural Engineering
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• v.11 no.4
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• pp.331-340
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• 1998

본 연구에서는 이동제한장치가 있는 연속교의 지진응답특성을 고찰하였다. 일점고정연속교에 있어서 이동제한장치는 교각이 탄성거동을 하는 경우 교축방법 수평력 분산기능이 있으며 교각하부에 소성힌지가 발생하거나 내진분리베어링이 있는 경우에는 최대변위 및 비탄성거동에 따른 잔류변위제한에 매우 효과적이다. 상부구조와 이동제한장치의 충돌시 발생하는 충격력은 완충재의 사용으로 상당히 감소시킬 수 있다. 이동제한장치의 설치위치 및 이격거리는 이동제한장치가 설치될 하부구조의 강성 및 강도와 온도변화, 급제동력, 작은 지진발생시 충돌여부, 신축이음장치유간 등을 고려하여 결정되어야 한다.

• Bulletin of the Korean Space Science Society
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• 2006.04a
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• pp.86-86
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• 2006

• Proceedings of the KOR-KST Conference
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• 2007.11a
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• pp.418-426
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• 2007

• Journal of KSNVE
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• v.27 no.1
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• pp.7-11
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• 2017