• Journal of Aerospace System Engineering
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• v.18 no.2
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• pp.12-20
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• 2024

The application of reinforcement design to ensure the structural safety of electronics in small satellites is limited by the spatial constraints of the satellite structure during launch vibrations. Additionally, a reliable evaluation approach is needed for mounting highly integrated devices that are susceptible to fatigue failure. Although the Steinberg fatigue failure theory has been used to assess the structural integrity of electronic devices, recent studies have highlighted its theoretical limitations. In this paper, we propose a structural methodology based on the critical strain theory to design the digital control unit (DCU) of the X-band SAR payload component for the small SAR technology experimental project (S-STEP), a small satellite constellation. To validate the design, we conducted modal and random analyses using simplified modeling techniques. Based on our methodology, we ultimately demonstrated the structural safety of the electronics through analysis results, safety margin derivation, and functional tests conducted both before and after the launch test.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.38 no.3
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• pp.251-258
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• 2014

Sunroof tracks are manufactured by press-forming extruded aluminum sheets. During press forming, cracking occurs along the sharply bent edge. The final positions of the punch and die were measured on the section, and their relation to cracking was investigated. Finite element simulation of bending to the final position was done to find the critical strains. Three-point bending tests with different material orientations, hardnesses, bending edge lengths, and bending radii were carried out in the laboratory, and finite element simulation of the three-point bending tests was performed to find the critical strains.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.37 no.4
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• pp.491-496
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• 2013

Finite element simulations of tensile tests were performed to determine the equivalent stress - equivalent plastic strain curves, critical equivalent stresses, and critical equivalent plastic strains. Then, the curves were used as inputs to finite element simulations of fracture toughness tests to determine the plane strain fracture toughness. The critical COD was taken as the COD when the equivalent plastic strain at the crack tip reached a critical value, and it was used as a crack growth criterion. The relationship between the critical COD and the critical equivalent plastic strain or the reduction of area was found. The relationship between the plane strain fracture toughness and the product of the critical equivalent stress and the critical equivalent plastic strain was also found.

• Proceedings of the Korean Society of Broadcast Engineers Conference
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• 2019.06a
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• pp.118-119
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• 2019

본 논문에서는 비디오 제작 및 유통의 활성화에 따라 필요성이 높아지고 있는 장면 전환을 검출하는 방법을 제안한다. 유통 과정에서 해상도 변환, 자막 삽입, 압축, 영상 반전 등의 다양한 변형이 추가되더라도 동일하게 장면 전환을 검출해야 하므로 전처리 과정과 SIFT를 이용한 특징 추출, 변형을 고려한 매칭 방법을 이용하여 프레임 간의 매칭률을 계산한다. 또한 매칭률의 임계값을 기준으로 장면 전환 여부를 판단한다. 원본 비디오에서의 특징을 가지고 다양한 변형이 가해진 비디오에서의 특징과 매칭률을 계산하여 유효성을 판단한다.

• Proceedings of the Materials Research Society of Korea Conference
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• 2009.11a
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• pp.35.1-35.1
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• 2009

오스테나이트계 Fe-10Cr-10Ni-xC(x=0.2, 0.5, 0.6and 0.7wt.%)합금에서 변형유기마르텐사이트상변태가 Sliding 마모저항성에 미치는영향을 탄소 및 온도에 따라 조사하였다. 변형유기마르텐사이트상변태가 미치는 영향을 살펴보기 위해 석출물적고 grain의 크기가 비슷한 합금내에서 조사하였다. 변형유기마르텐사이트상변태가 일어나는데 필요한 에너지를 변형률-응력 곡선을 통해 구할 수 있으며, 이를 임계변형에너지라 규명했다. 그 결과, 상온에서 Carbon 함량에 따라 변형유기마르텐사이트상변태가 일어나는데 필요한 임계변형에너지는 증가하였으며, Sliding 마모저항성은 저하되었다. 이는 carbon이 오스테나이트 안정화원소(austenite stabilityelement)이므로 carbon 함량이 증가할수록 변형유기마르텐사이트상변태가 유발하기위해서는 많은 에너지가 필요하기 때문에 low C에 비해 high C의 마모저항성이 저하된 것으로 사료된다. 또한 변형유기마르텐사이트상변태가 고온 Sliding 마모저항성에 미치는 영향을 살펴보기 위해 Fe-Cr-Ni-xC(x=0.2, 0.5, 0.6 and 0.7wt.%)합금을 온도별(25, 100, $300^{\circ}C$)로 조사하였다.

• Tunnel and Underground Space
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• v.19 no.2
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• pp.158-166
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• 2009

As a basic study for investigating the development of the stress-induced crack in Hoek-Brown rock, a homogenization technique of elastic cracks is proposed. The onset of crack is monitored by Hoek-Brown empirical criterion, while the orientation of the crack is determined by the critical plane approach. The concept of volume averaging in stress and strain component was invoked to homogenize the representative rock volume which consists of intact rock and cracks. The formulation results in the constitutive relations for the homogenized equivalent anisotropic material. The homogenization model was implemented in the standard FEM code COSMOSM. The numerical uniaxial tests were performed under plane strain condition to check the validity of the propose numerical model. The effect of friction between the loading plate and the rock sample on the mode of deformation and fracturing was examined by assuming two different contact conditions. The numerical simulation revealed that the homogenized model is able to capture the salient features of deformation and fracturing which are observed commonly in the uniaxial compression test.

• Journal of the Korean Geosynthetics Society
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• v.6 no.4
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• pp.1-6
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• 2007

New procedure for evaluation of creep reduction factor by the limit creep strain concept was introduced through the analysis of creep test results. To determine the limit creep strain of the geogrids, the Sherby-Dorm Plots were applied and the results of this procedure were compared and interpreted, respectively. From this, it is seen that the creep reduction factors were 1.45 for the geogrid samples used in this study. Through the comparison of creep reduction factors in 10% creep strain criteria, it was confirmed that the range of creep reduction factor is about 0.06~0.14 for the geogrid samples in this study.

• Composites Research
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• v.12 no.4
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• pp.8-16
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• 1999

In this study, when the applied directions of tensile loading is changed fatigue damage of quasi-isotropic composite laminates was discussed. Low cycle fatigue tests of $[0/-60/+60]_s$ laminates and $[+30/-30/90]_s$ laminates were carried out. Material systems used were AS4/Epoxy and AS4/PEEK. The fatigue damage of $[+30/-30/90]_s$ laminates differed from that of $[0/-60/+60]_s$ laminates. The position of delamination generated at AS4/Epoxy and AS4/PEEK $[+30/-30/90]_s$ laminates appeared differently according to the kind of matrix. Critical values of strain energy release rate were obtained by using the strain measured at the initiation of delamination. The experimental results agreed well with the results obtained by the proposed method for determining strain energy release rate.

• Proceedings of the Korean Society of Precision Engineering Conference
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• 2012.10a
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• pp.703-704
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• 2012

• Fire Science and Engineering
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• v.17 no.3
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• pp.20-25
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• 2003

Measurements with filaments and thermocouples and computations with Oppdif and FDS were carried out to investigate the impact of flame strain, agent addition, and buoyancy on the structure and extinction of nonpremixed counterflow flames. Measurements through 2.2 s drop tests in microgravity conditions and experiments in normal gravity conditions were compared with the results of computations. For the global strain rates 7 s$^{-1}$ through 100 s$^{-1}$ , the turning point behavior in the critical nitrogen concentration at O-g was confirmed. The effects of buoyancy, that is, changes in the flame curvature and thickness were also confirmed by the computations with FDS. There was agreement in the peak flame temperature and its position between the computations and the measurements in the near extinction methane/air diffusion flames in microgravity.