• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.37 no.8
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• pp.780-788
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• 2009

AE technique was applied to the static structural test of the composite wing structure to evaluate the structural integrity and damage. During the test, strain and displacements measurement technique were used to figure out for static structural strength. AE parameter analysis and source location technique were used to evaluate the internal damage and find out damage source location. Design limit load test, the 1st and 2nd design ultimate load tests and fracture test were performed. Main AE source was detected by an sensor attached on skin near by front lug. Especially, at the 1st design ultimate test, strain and displacements results didn't show internal damage but AE signal presented a phenomenon that the internal damage was formed. At the fracture test, AE activities were very lively, and strain and displacements results showed a tendency that the load path was changed by severe damage. The internal damage initiation load and location were accurately evaluated during the static structural test using AE technique. It is certified from this paper that AE technique is useful technique for evaluation of internal damage at static structural strength test.

• Journal of the Korea institute for structural maintenance and inspection
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• v.21 no.3
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• pp.60-68
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• 2017

Since the bridge is the main facility of the road that is the core of the civil infrastructure, the bridge is constructed to ensure stability and serviceability during the traffic use. In order to secure the safety of bridges, evaluating the integrity of bridges at present is an important task in the maintenance work of bridges. In general, to evaluate the load carrying capacity of bridges, it is possible to confirm the superimposed behavior and symmetric behavior of bridges by estimating the lateral load distribution factor of the bridges through vehicle loading tests. However, in order to measure the lateral load distribution factor of a commonly used bridge, a static loading test is performed. There is a difficulty in traffic control. Therefore, in this study, the static displacement component of the bridge measured in the dynamic loading test and the ambient vibration test was extracted by using empirical mode decomposition technique. The lateral load distribution was estimated using the extracted static displacement component and compared with the lateral load distribution factor measured in the static loading test.

• Proceedings of the Korean Institute of Industrial Safety Conference
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• 1999.06a
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• pp.181-186
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• 1999

반복하중에 따른 P.C 구조물의 장착장치로 사용되는 Wedge 형상에 따른 거동특성을 파악하기 위하여 정적최대하중을 이용하여 피로시험을 수행하였다. 또한 피로시험 결과로부터 반복회수에 따른 시험 체의 균열양상, 하중-변위, 하중-변형율, 하중-중앙 최대 변위, 하중-영구 변형량, 반복횟수에 따른 S-N선도 등을 고찰하였다. (중략)

• Journal of the Korean Geotechnical Society
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• v.17 no.1
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• pp.25-34
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• 2001

송전철탑의 기초로써 락앵커는 바람에 의해 반복적인 하중을 받고 있다. 반복하중은 락앵커의 인발 지지력 감소와 누적변위의 증가를 유발할 수 있다. 그러므로 송전철탑의 락앵커 설계시 세심한 주의가 요구된다. 본 논문에서는 세 가지 암반형태에 시공된 모형 락앵커에 대하여 반복하중 시험을 수행한 결과들을 제시하였다. 시험결과에 의하면 정적 극한하중의 50%보다 작은 최대 반복하중(Q$_{max}$)이 락앵커에 작용할 경우, 락앵커의 지지력에 대하여 반복하중의 영향이 없다. 최대 반복하중이 정적 극한하중의 50%에서 75%로 작용할 경우 누적변위의 증가를 유발하고, 정적 극한하중의 75%이상인 경우 락앵커의 지지력에 심각한 영향을 미친다. 따라서 정적 극한하중의 50% 이상의 반복하중을 받는 락앵커는 불안정하다.

• Korean Journal of Materials Research
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• v.7 no.11
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• pp.974-980
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• 1997

SiC$_{p}$/AI 합금 복합재료에 있어서 동적 및 정적파괴인성시험을 실시하고 파괴거동에 미치는 부하조건의 영향을 검토하였다. 동적파괴인성시험은 CAI시스템을 이용하여 1.5m/sec의 부하속도로 실시하였고, 정적파괴인성시험은 만능시험기를 이용하여 0.3 mm/min의 부하속도로 실시하였다. 또한 파괴과정을 명확히 해석하기 위하여 동적부하조건에 대해서는 stop block법을, 정적부하조건에 대해서는 복수시험편법을 이용하였다. 균열의 발생 및 성장은 부하조건에 의해 크게 영향을 받으며, 변위량에 대한 균열의 발생은 정적부하조건에서 더 빨리 일어나고, 균열의 성장은 동적부하조건에서 더 급격하다. 또한 부하조건은 파괴의 형태에도 크게 영향을 미치며, 동적부하조건하에서는 정적부하조건하에 비하여 균열이 입자부분(입자의 파단 또는 박리)을통과해 가는 경향이 크고 비교적 많은 편향을 반복해서 진행해 가지 때문에 파괴인성치도 크다.다.

• Journal of the Korea institute for structural maintenance and inspection
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• v.23 no.4
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• pp.53-60
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• 2019

In this study, a method for updating the finite element model of bridges with genetic algorithm using static displacement were presented, and verified this method using field test data for PSC girder bridge. As a field test, static load test and pseudo-static load test were conducted, and updated the finite element model of test bridge using each test data. Finally, evaluated the bridge load carrying capacity with updated model using pseudo-static load test's displacement data. To evaluate the bridge load carrying capacity, KHBDC-LSD, KHBDC and AASHTO LRFD's live load model were used, and compared the each results.

• Composites Research
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• v.28 no.4
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• pp.191-196
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• 2015

In this study, the static analysis and experiment were carried out on DCB specimens manufactured with aluminum foam in order to investigate the fracture toughness at the adhesive joint of the structure bonded with adhesive. In case of static analysis, all specimen models were shown to have the maximum reaction force when the forced displacement proceeded as much as 5 mm. The maximum reaction forces became 0.25 kN, 0.28 kN and 0.5 kN respectively in cases of specimen thicknesses of 35 mm, 45 mm and 55 mm. Two specimens in case of static experiment were selected to verify these analysis results. The maximum reaction forces were shown when the forced displacement proceeded as much as 5 to 6 mm. The maximum reaction forces became 0.22 kN and 0.3 kN respectively in cases of specimen thicknesses of 35 mm and 45 mm. By comparing the derived results, it could be shown that there was not much difference between the data of analyses and experiments. Therefore, It is inferred that the study data can be secured with only analysis by no extra experimental procedure. It is thought that the mechanical properties at the structure bonded of DCB with the type of mode III can be analyzed systematically.

• Journal of Korean Association for Spatial Structures
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• v.12 no.3
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• pp.79-87
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• 2012

In this study, static displacement sensors using lead switches are bonded on concrete beams and RC beams, and monitoring systems to crack damages are studied using radio frequency. If load is received on the center of flexible specimens, bonded static displacement sensors will be destroyed, and these become to send signals of damages at radio frequency system connected with static displacement sensors. Study of these functional building elements will be protected from external factors by unusual weather, earthquake, etc, in RC buildings and structures.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.36 no.5
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• pp.420-427
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• 2008

For simulation of a fin unfolding motion for the various aerodynamic conditions, equations and moments applying to the unfolding fin were modelled. Aerodynamic roll moment consists of the static roll moment and the damping moment, which were obtained through wind tunnel tests and numerical analyses respectively. Panel method was used to compute the roll damping coefficient with deflected fin, whose angle was equivalent to angle of attack due to the deployment motion. Roll damping coefficient is a function of angle of attack, sideslip angle, and deployment angle but not of angular velocity of deployment. Simulation with aerodynamic damping model gave more similar deployment time compared to fin deployment test results.

• Aerospace Engineering and Technology
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• v.4 no.1
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• pp.129-142
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• 2005

A semi-monocoque truncated cone structure, which is a main structure for the payload adapter of KSLV-I, was designed. Static test was performed to confirm the reliability of the cone structure under the design loads. Strains and displacements are measured during four load cases; the compressive axial, pure bending, pure shear, and combined loading conditions. The results showed that the cone structure satisfies the design requirements. An equivalent axial load was applied to the cone structure so that the global buckling of the cone structure occurred. The measured buckling load was compared with the predicted one by finite element method. The results show a good agreement.