This study investigates changes in the mechanical behaviors, especially hardness and indentation load-displacement curves, of thermal barrier coatings (TBCs) brought about by thermal shock. The TBCs on the Nickel-based bondcoat/superalloy was prepared with diameters of 25.4 mm and 600 μm thickness. The results of thermal shock cycling test from 1100 oC of the highest temperature indicate that the thermal shock do not influence on the mechanical behavior, but a continuous decrease in porosity and increase in hardness were observed after 1200 thermal shock cycles; these changes are believed to be due to sintering of thermal barrier coating materials. The results that no degradation in the indentation load-displacement curves indicate that the coating shows good thermal shock resistance up to 1200 cycles at 1100 oC in air.

In this study, the effect of temperature effect of the rubber matrix filled with nano sized silica particles composites with silica volume fraction of 19–25% was investigated by the Charpy impact test. The Charpy impact test was conducted in the temperature range from –40°C to 0°C. The critical energy release rate GIC of the rubber matrix composites filled with nano sized silica particles was considerably affected by temperature and it was shown that the maximum value was appeared at higher temperature between temperature tested and it was shown that the value of GIC increases as temperature tested increases. The major fracture mechanisms were matrix deformation, silica particle debonding and delamination, microcrack between particles and matrix, and/or pull out between particles and matrix which is ascertained by SEM photographs of Charpy impact surfaces fracture.

The present study is undertaken to evaluate the effect of volume fraction on the results of Charpy impact test for the rubber matrix filled with nano sized silica particles composites. The Charpy impact tests are conducted in the temperature range 0°C and –10°C. The range of volume fraction of silica particles tested are between 11% to 25%. The critical energy release rate GIC of the rubber matrix composites filled with nano sized silica particles is affected by silica volume fraction and it is shown that the value of GIC decreases as volume fraction increases. In regions close to the initial crack tip, fracture processes such as matrix deformation, silica particle debonding and delamination, and/or pull out between particles and matrix which is ascertained by SEM photographs of Charpy impact fracture surfaces.

복합적층판은 다른 금속재료에 비해 높은 비강도, 비강성 등의 우수한 역학적 특성을 지니므로 최근 다양한 분야에서 사용하고 있다. 그러나 이러한 복합적층판은 일반 금속재료에 비해 충격에 약하다는 단점이 있다. 이 점을 해결하기 위한 연구는 많은 연구자들에 의해 다양하게 시도되고 있다. 본 연구는 복합적층판에 초기응력을 도입하여 충격거동 특성을 파악한다. 고전적인 이론식인 Hertz의 접촉법칙과 실험식인 Sun과 Tan의 압입법칙을 포함한 유한요소프로그램을 이용하여 복합적층판의 초기응력에 의한 충격거동 특성을 조사한다.

The fiber reinforced polymer (FRP) strengthening is significantly effective for enhancing the performances of concrete to the high strain rate loadings. However, the FRP retrofitted concrete members show different behaviors comparing to quasi-static cases. This study presents experimental observation on behaviors of meso-scale concrete members retrofitted with FRP sheets under low-velocity drop-weight impact loadings. Concrete specimens with the dimensions of 100×100×400 mm were fabricated and various FRP sheets were attached. The specimens with a reinforced bottom surface and the doubly reinforced specimens showed much higher energy absorptions. Also, reinforced concrete (RC) members were cast and reinforced with CFRP sheets. The FRP flexural and shear strengthening RC beams has weakness in the spalling failure because the impact load concentrated the concrete face which is not strengthened with FRP sheets.

복합적층판은 다른 금속재료에 비해 높은 비강도, 비강성 등의 우수한 역학적 특성을 지니므로, 최근 다양한 분야에서 사용하고 있다. 그러나 이러한 복합적층판은 충격에 약하다는 단점이 있다. 그리하여 복합적층판의 충격거동에 대한 많은 연구가 이루어지고 있다. 충격거동을 조사하기 위해서는 우선 충격체와 복합적층판사이의 접촉력을 계산하여야 한다. 접촉력을 알기 위해서는 운동방정식, 복합적층판의 운동방정식 그리고 압입량에 관한 관계식을 동시에 풀어야 한다. 본 연구에서는 고전적인 헤르츠식, 썬식, 썬&양식 그리고 썬&탄식을 포함한 유한요소프로그램을 이용하여 복합적층판의 저속충격거동을 조사한다.

The present study was undertaken to evaluate the effect of temperature on the results of Charpy impact test for glass fiber reinforced polyurethane(GF/PUR) composites. The Charpy impact test were conducted in the temperature range from -50˚ to 50˚. The impact fracture toughness of GF/PUR composites was considerably affected by temperature and it was shown that the maximum value was appeared at room temperature. It is believed that sensitivity of notch on impact fracture energy were increased with decrease in temperature of specimen. As the GF/PUR composites exposed in low temperature, impact fracture toughness of composites decreased gradually owing to the decrease of interface bonding strength caused by difference of thermal expansion coefficient between the glass fiber/polyurethane resin. And decrease of interface bonding strength of composites with decrease in specimen temperature was ascertained by SEM photographs of Charpy impact fracture surface.

충격흡수시설의 충돌거동은 보통 0.4초 미만의 짧은 순간에 일어나므로 삼차원의 매우 복잡한 거동을 수치적으로 계산한다는 것은 쉽지 않다. 따라서 새로운 충격흡수시설을 개발할 때 특별한 설계단계를 거치지 않고 실물차량 충돌시험에만 의존하고 있는 실정이다. 충돌시험에서 탑승자 안전도를 평가하기 위해서 계측기를 통해 가속도와 각속도를 추출하여 계산하고 있으며 고속카메라를 이용해 차량과 충격흡수시설의 충돌거동을 촬영한다. 하지만 고속카메라 영상의 활용범위는 제한적으로 사용되고 있으며, 탑승자 안전도 분석이나 충격흡수시설의 에너지소산 메커니즘을 분석하기위해 활용된 사례가 없다. 본 연구에서는 계측기로부터 획득한 데이타와 고속카메라 영상분석을 통해 추출된 데이타를 비교해 적합성 여부를 판단하고 탑승자 안전도 해석이나 충돌거동을 분석 에 활용할 수 있는 방안을 모색하였다.

The main goal of this work is to study the effects of temperature and volume fraction of fiber on the Charpy impact test with GF/PP composites. The critical fracture energy and failure mechanisms of GF/PP composites are investigated in the temperature range of 60℃ to -50℃ by impact test. The critical fracture energy increased as the fiber volume fraction ratio increased. The critical fracture energy shows a maximum at ambient temperature and it tends to decreases as temperature goes up or goes down. Major failure mechanisms can be classified such as fiber matrix debonding, fiber pull-out and/or delamination and matrix deformation.

Many of researches regarding mechanical properties of composite materials are associated with humid environment and temperature. Especially the temperature is a very important factor influencing the design of thermoplastic composites. However, the effect of temperature on impact behavior of reinforced composites have not yet been fully explored. An approach which predicts critical fracture toughness GIC was performed by the impact test in this work. The main goal of this work is to study the effect of temperature and span of specimen supports on the results of Charpy impact test for GF/PE composite. The critical fracture energy and failure mechanism of GF/PE composites were investigated in the temperature range of 60℃;to;-50℃ by the Charpy impact test. The critical fracture energy showed the maximum at the ambient temperature, and it tended to decrease as the temperature increased or decreased from the ambient temperature. The major failure mechanisms are the fiber matrix debonding, the fiber pull-out and/or delamination and the matrix deformation.n.

장섬유 CF/에폭시 복합재료를 사용하여-50℃에서 60℃ 사이의 범위에서 스팬길이를 변화시켜 충격시험으로 얻어진 임계파괴에너지의 거동을 고찰한 결과는 다음과 같다. 1. CF/에폭시 복합재료의 온도 변화에 따른 임계파괴에너지 GIC는 동일한 스팬길에서는 실온의 경우가 가장 높고, 60℃, -15℃ 그리고 -50℃의 순으로 낮게 나타났다. 2. CF/에폭시 복합재료의 스팬길이의 변화에 대한 임계 파괴에너지 GIC는 동일한 온도조건하에서는 스팬길이가 20mm인 경우가 가장 높게 나타났으나 불안정하며, 스팬길이는 40mm인 경우 임계파괴에너지 GIC는 가장 낮게 나타났으나 실험치의 흩어짐을 고려할 때 40mm인 경우의 시험편이 더 적절한 조건이라 생각된다. 3. 본 실험에 사용한 재료의 파괴기구는 섬유의 풀아웃, 섬유와 매트릭스 사이의 디본딩 그리고 매트릭스의 변형을 관찰할 수 있었으며, 이와 같은 파괴기가구 종합적으로 상호작용한다고 생각된다.

The critical fracture energy and failure mechanisms of GF/PP composites are investigated in the temperatures range of the ambient temperature to -50℃ The critical fracture energy increase as fiber volume fraction ratio increased The critical fracture energy shows a maximum at ambient temperature and it tends to decrease as temperature goes up. Major failure mechanisms can be classfied such as fiber matrix debonding, fiber pull-out and/or delamination and matrix deformation.