• Journal of the Korea Concrete Institute
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• v.23 no.6
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• pp.723-730
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• 2011

It is very important to experimentally evaluate concrete behavior at elevated temperature because aggregates make up approximately 80 percent of volume in concrete. In this study, an experiment to evaluate mechanical properties of normal weight and light weight concrete of 60 MPa was conducted. Based on loading level of 0, 20 and 40 percent, the tests of 28 days compressive strength, elastic modulus, thermal strain, total strain, and transient creep using ${\phi}100{\times}200mm$ cylindrical specimens at elevated temperature were performed. Then, the results were compared with CEB (Committes Euro-international du Beton) model code. The results showed that thermal strain of light weight concrete was smaller than normal weight concrete. Also, the results showed that compressive strength of light concrete at $700^{\circ}C$ was higher than normal weight concrete and CEB code, similar to that obtained at ambient temperature. Transient creep developed from loading at a critical temperature of $500^{\circ}C$ caused the concrete strains to change from expansion to compression. The transient creep test result showed that internal force was high when the ratio of shrinkage between concrete and aggregate was more influential than thermal expansion.

• Aerospace Engineering and Technology
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• v.13 no.1
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• pp.76-85
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• 2014

In this paper, the equivalent coefficient of thermal expansion (CTE) of fiber reinforced plastic composite material is investigated with various CTE prediction schemes. Although there are several methods for predicting the equivalent CTEs, most of them have some limitations of are not much accurate when comparing prediction results with test results. In the framework of computational homogenization, a representative volume element is taken from the predefined fiber-volume ratio, and modelled with finite element mesh. Finally, the equivalent CTEs are obtained by applying periodic boundary condition. To verify the performance of the proposed method, the results obtained are compared with those by the existing methods and test results. Additionally, the thermal pointing error analysis for star tracker support structure is conducted and its accuracy is estimated according to CTE prediction schemes.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.42 no.10
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• pp.809-815
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• 2014

The co-bonded dissimilar composite under a wide range of temperature change shows thermal distortion due to the differences in thermal expansion characteristics of the composite materials. Analysis of the thermal expansion characteristics of each composite is required for the design of co-bonded dissimilar composite structure with considering the shape distortion during the manufacturing process. In this work, digital image correlation (DIC) technique is introduced for measuring the thermal distortion characteristics of co-bonded dissimilar composite specimen, carbon/epoxy and silica/phenolic. The thermal distortion of co-bonded dissimilar composite specimen is numerically estimated and compared with the experiments. The estimated results is successfully validated using the measured results.

• Journal of the Korean Ceramic Society
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• v.38 no.2
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• pp.193-198
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• 2001

유한요소법을 이용하여 STS VOD 래들에서 내장 내화물의 재질 및 back filler의 시공 위치에 따른 열응력을 수행하였다. 불소성 내화물의 경우 높은 열전도율에 의해 가동면과 배면(back face)간의 온도구배가 소성품에 비해 감소하였으며 탄성계수도 낮아 발생되는 열응력이 2~4배 낮았다. Back filler는 dolomite 내화물의 열간 팽창을 흡수하기 위해 시공하는 것으로, 상대적으로 낮은 열전도율을 가지고 있기 때문에 back filler의 내부와 외부에 급격한 온도구배가 발생된다. 결과적으로 래들의 내부는 고온을 유지하여 내화물이 팽창이 되고, 외부는 온도가 낮아지므로 수축되어 열응력이 증가하였다.

• Korean Journal of Optics and Photonics
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• v.4 no.4
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• pp.397-402
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• 1993

This paper presents a new computational algorithm of phase-shifting interferometry which can effectively eliminate the uncertainty errors of the reference phases encountered in obtaining multiple interferograms. The algorithm treats the reference phases as additional unknowns and determines their exact values by analyzing interferograms using numerical least square technique. A series of simulations prove that this algorithm can improve measuring accuracy being unaffected by the nonlinear and random errors of phase-shifters.

• Korean Journal of Crystallography
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• v.14 no.1
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• pp.7-12
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• 2003

The compound SrA1₂(BO₃)₂O is a good host lattice for negative thermal expansion. We have measured thermal expansion over the limited temperature range by X-ray diffraction and ceramic dilatometry. In the aluminum borate compound, a thermal contraction is observed with a coefficient -1.64×10/sup -4/ Å/℃ on the c axis in the temperature range 23∼215℃ and with a maximum change -1.75㎛ in length of a ceramic bar of 20㎜ in the temperature range 110∼170℃, respectively.

• Proceedings of the Korean Institute of Surface Engineering Conference
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• 2012.05a
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• pp.137-138
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• 2012

박막태양전지의 경우 기판재와 태양전지를 구성하는 반도체 층간의 열팽창 거동 차이가 태양전지의 변형을 야기한다. 이러한 열변형은 태양전지의 효율에 영향을 주는 것으로 알려져 있다. 그러므로 태양전지를 구성하는 반도체 층과 열팽창 거동이 유사한 기판재의 적용이 필요하다. 본 연구에서는 연성 CIGS 태양전지를 구성하는 기판과 박막층의 두께변화가 열공정 중 발생하는 잔류응력에 미치는 영향을 전산해석 하고자 하였다. 전산해석 결과 Fe-52wt%Ni 기판재의 두께가 증가함에 따라 CIGS 박막층 내부의 잔류응력은 감소하였다. SiO2 절연층의 두께가 증가하면 CIGS 박막층의 잔류응력이 증가하였다. Mo 후면전극층이 얇아지면 잔류응력이 감소하였으나 CIGS층의 두께변화는 CIGS층의 잔류응력에 큰 영향을 미치지 않았다.

• Proceedings of the Optical Society of Korea Conference
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• 2003.07a
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• pp.138-139
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• 2003

반사경을 지지하는 데에 있어서의 기계적, 열적 변형이 광학 부품에 미치는 영향을 최소화 하도록 광학 요소를 이러한 영향으로부터 차단하는 기계 장치를 플렉셔(flexure)라고 한다. 기계적 영향은 중력, 관성, 진동에 의한 하중 및 조립 시의 오차에 의한 응력 등에 의해 발생하는 변형을 말한다. 또한 열적 영향은 열적 평형 상태와 과도 상태 하에서 주위 환경의 온도변화에 의한 변형을 말한다. 예를 들어 작은 열팽창 계수를 가진 반사경 또는 렌즈와 큰 열팽창 계수를 갖는 지지구조가 어떤 온도 하에서 조립된 후 처음 온도와 다른 온도에 놓이는 경우를 생각해 보자. (중략)

• Proceedings of the Korea Society for Energy Engineering kosee Conference
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• 1999.05a
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• pp.207-212
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• 1999

화학반응이 일어나는 고정층 반응기의 성능을 모사하고 해석하기 위해서는 반응베드의 열 및 물질전달 특성을 정확히 아는 것이 중요하다. 본 연구에서는 화학열펌프에 사용되는 금속염-팽창흑연 다공성 반응매체의 유효열전도도와 기체투과도를 측정하였다. 유효열전도도는 전이 일차원 열류기법을 이용하여 측정하였고, 기체투과도는 Darcy's law를 이용하여 측정하였다. 팽창흑연이 함유된 반응베드의 유효열전도도와 기체투과도는 흑연을 기준으로 한 겉보기밀도에 따라 각각 14.1-36.5 W/mK, 8.0x$10^{-15}$-$10^{-12}$ $m^2$의 범위에 있었다.

• Aerospace Engineering and Technology
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• v.8 no.2
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• pp.113-121
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• 2009

Shaker system is used to simulate the vibration from the launch environment. The vibration tests are performed in the vertical and lateral direction. For the lateral vibration test, the slip table system is used with shaker system. For the latest large satellite, vibration test adaptor is made of the steel. But slip table of lateral vibration is made of magnesium, so there is big difference of thermal expansion ratio between slip table and vibration test adaptor. This paper encompasses the following items; verification process of thermal characteristics and overturning moment and a solution for lateral vibration test with steel vibration test adaptor.