• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2003년도 춘계학술발표대회 논문집
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• pp.37-41
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• 2003

In this study the mechanical behaviors of fiber metal laminates (FML) such as ARALL, GLARE and CARE which are recently developed as new structural materials and known to have excellent fatigue resistant characteristics while with relatively low densities compared to the conventional aluminum materials, are considered through the classical lamination theory. The mechanical properties such as elastic moduli, thermal expansion coefficients and hygro-thermally induced residual stresses in the fiber metal laminates are obtained and compared each other. Also load carrying mechanism between metal sheets and composite layers in the FML are considered.

• 한국구조물진단유지관리공학회 논문집
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• 제11권5호
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• pp.89-98
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• 2007

본 연구에서는 RC구조물의 접착 보수 보강 재료의 박리와 연관한 변형 거동에 대하여 검토하였다. 응력-변형곡선에서 최대응력 이후 항복을 일으킬 수 있는 변형량은 바탕재인 시멘트 모르터의 경우 $2.0{\times}10^{-3}$, 콘크리트는 $1.3{\times}10^{-3}$ 전후이고, 접착제인 에폭시수지 $0.8{\times}10^{-3}$, 폴리머 시멘트 모르터 $2.5{\times}10^{-3}$이며, 보강재인 강판과 탄소봉은 2.5와 $9.1{\times}10^{-3}$정도인 것으로 밝혀졌다. 온도변화에 따른 선팽창계수는 바탕재인 시멘트 모르터 및 콘크리트의 경우 $10{\mu}{\varepsilon}/{^{\circ}C}$전후인데 비하여, 접착제인 에폭시 수지는 $41{\sim}54{\mu}{\varepsilon}/{^{\circ}C}$, 폴리머 시멘트 모르터는 $-0.5{\sim}0.7{\mu}{\varepsilon}/{^{\circ}C}$, 보강재인 강판은 바탕재료와 비슷하지만, 탄소섬유는 $-1.7{\mu}{\varepsilon}/{^{\circ}C}$로 제일 작은 값이었다. 특히 바탕재료인 콘크리트와 에폭시수지 접착제간에는 온도변화에 따른 선팽창계수 차이가 크게 발생하였는데, 에폭시 수지 종류에 따라 약간의 차이는 있지만, $20{\sim}35{^{\circ}C}$이상의 온도차가 발생하는 조건이면 에폭시수지 접착제는 콘크리트 접착면에서 자연적으로 박리 할 수도 있는 것으로 밝혀졌다.

• 한국결정성장학회지
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• 제7권3호
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• pp.359-365
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• 1997

$K_2CoCl_4$ 단결정을 Ar분위기에서 Czochralski법으로 육성하였다. 육성된 결정의 물리적 성질의 조사로서 먼저 유전적 특성을 조사하여 commensurate-incommensurate(C-INC) 상전이에서 유전율의 thermal hysteresis가 $5^{\circ}C$ 이하의 값을 가짐을 보였고, incommensurate(INC) 상에서 $K^+$ 이온에 의한 ionic hopping mechanism으로 전도도를 해석하였으며 이때 activation energy는 0.62 eV 이었다. 각각의 결정축으로 열팽창을 조사하여 c축으로 가장 큰 열팽창을 보였으며 열팽창계수를 계산하였다. 광학적 특성의 조사로서 200 nm~ 3000 nm 영역에서 흡수 스펙트럼을 측정하여 나타나는 흡수 peak을 결정장내의 에너지 준위의 분리에 따른 전이 에너지로 해석하였으며, 800 nm~ 1200 nm 영역의 투과특성으로 optical band filter로서의 가능성을 제시하였다.

• Steel and Composite Structures
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• 제18권6호
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• pp.1493-1515
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• 2015

A new refined hyperbolic shear deformation theory (RHSDT), which involves only four unknown functions as against five in case of other shear deformation theories, is presented for the thermoelastic bending analysis of functionally graded sandwich plates. Unlike any other theory, the number of unknown functions involved is only four, as against five in case of other shear deformation theories. The theory presented is variationally consistent, does not require shear correction factor, and gives rise to transverse shear stress variation such that the transverse shear stresses vary parabolically across the thickness satisfying shear stress free surface conditions. The sandwich plate faces are assumed to have isotropic, two-constituent material distribution through the thickness, and the modulus of elasticity, Poisson's ratio of the faces, and thermal expansion coefficients are assumed to vary according to a power law distribution in terms of the volume fractions of the constituents. The core layer is still homogeneous and made of an isotropic ceramic material. Several kinds of sandwich plates are used taking into account the symmetry of the plate and the thickness of each layer. The influences played by the transverse shear deformation, thermal load, plate aspect ratio and volume fraction distribution are studied. Numerical results for deflections and stresses of functionally graded metal-ceramic plates are investigated. It can be concluded that the proposed theory is accurate and simple in solving the thermoelastic bending behavior of functionally graded plates.

• Composites Research
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• 제20권3호
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• pp.37-42
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• 2007

금속복합재료에서는 강화재와 기지재 사이의 열팽창계수 차이에 의해 복합재료 내부에 잔류응력이 남아있어 복합재료 전체의 강도저하를 가져온다. 본 연구에서는 TiNi 형상기억합금을 강화재료로써 이러한 잔류응력 문제를 해결하기 위하여 이용하였다. TiNi 형상기억합금은 형상기억효과를 이용하여 복합재료의 잔류응력문제를 해결할 뿐만 아니라 복합재료의 인장강도를 증가시키는 역할을 한다. 핫프레스 방법에 의해 제작된 형상기억복합재료의 강도증가를 위하여 냉간압연을 실시하여 실험을 실시하였다. 이와 같이 제작된 형상기억복합재료의 저온에서의 미시적 손상거동을 평가하기 위하여 음향방출기법을 이용하였다. 또한 열충격을 받은 시험편의 손상에 대한 연구도 이루어졌다.

• 한국세라믹학회지
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• 제31권5호
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• pp.572-580
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• 1994

With low thermal expansion coefficients, eucryptite (Li2O.Al2O3.2SiO2) and spodumene (Li2O.Al2O3.4SiO2) in LAS ceramic system show good thermal shock resistance. In this study, sillimanite or kaolin group silicate minerals and Li2CO3 were used as starting materials, and if necessary SiO2 or Al2O3 were added for making stoichiometrically formed specimens. By this process, eucryptite powders were synthesized and characterized. The powder mixtures of lithiumcabonate and silicate minerals calcined at 80$0^{\circ}C$ for 2 hrs were made into powder compacts. $\beta$-Eucryptite single phase was formed via intermediate phases of Li2SiO3 and LiAlO2 et al, by heating at 110$0^{\circ}C$ or 120$0^{\circ}C$ for 10 hrs from those powder compacts. When using the sillimanite group minerals, Virginia kyanite or andalusite was reacted to form eucryptite at 120$0^{\circ}C$and CMK International kyanite were completed at 110$0^{\circ}C$. When kaolin group minerals were used, it was found that the synthesizing temperature (100$0^{\circ}C$) of $\beta$-eucryptite from the mixture of New Zealand white kaolin was lower than that from Hadong pink kaolin (110$0^{\circ}C$). The Microstructure of systhesized powder showed the irregular lump shape such as densed crystallines.

• Nuclear Engineering and Technology
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• 제51권4호
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• pp.987-995
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• 2019

Steam jet condensation is of great importance to pressure suppression containment and automatic depressurization system in nuclear power plant. In this paper, the condensation processes of sonic steam jet in a quiescent subcooled pool are recorded and analyzed, more precise understanding are got in direct contact condensation. Experiments are conducted at atmospheric pressure, and the steam is injected into the subcooled water pool through a vertical nozzle with the inner diameter of 10 mm, water temperature in the range of $25-60^{\circ}C$ and mass velocity in the range of $320-1080kg/m^2s$. Richardson number is calculated based on the conservation of momentum for single water jet and its values are in the range of 0.16-2.67. There is no thermal stratification observed in the water pool. Four condensation regimes are observed, including condensation oscillation, contraction, expansion-contraction and double expansion-contraction shapes. A condensation regime map is present based on steam mass velocity and water temperature. The dimensionless steam plume length increase with the increase of steam mass velocity and water temperature, and its values are in the range of 1.4-9.0. Condensation heat transfer coefficient decreases with the increase of steam mass velocity and water temperature, and its values are in the range of $1.44-3.65MW/m^2^{\circ}C$. New more accurate semi-empirical correlations for prediction of the dimensionless steam plume length and condensation heat transfer coefficient are proposed respectively. The discrepancy of predicted plume length is within ${\pm}10%$ for present experimental results and ${\pm}25%$ for previous researchers. The discrepancy of predicted condensation heat transfer coefficient is with ${\pm}12%$.

• 대한기계학회논문집B
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• 제38권2호
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• pp.155-163
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• 2014

주유소에서 거래되는 액체 연료인 석유류는 온도 변화에 따라 팽창과 수축하게 된다. 석유류의 체적팽창계수는 약 $0.1%/^{\circ}C$이고, 우리나라의 기온은 겨울철에는 $-15^{\circ}C$, 여름철에는 $35^{\circ}C$까지 변한다. 온도 변화에 따른 체적의 변화가 석유류 거래에 미치는 영향을 조사하기 위해 주유소에 저장된 연료와 주유되는 연료의 온도 변화를 측정하였다. 또 우리나라의 지난 50 년간의 일간, 월간, 년간 온도 변화를 고찰하였다. 지하 저장탱크의 유류 온도는 계절에 관계없이 하루 중 안정되게 유지되었다. 주유소 주위의 환경 조건과 위치, 주유 빈도등이 주유되는 유류의 온도에 영향을 미치는 것을 알 수 있었다. 이러한 연구 결과는 건전한 석유류의 거래와 관련 법령의 제정에 활용될 것이다.

• 대한치과보철학회지
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• 제41권1호
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• pp.89-98
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• 2003

Titanium requires special ceramic system for veneering. Low fusing dental ceramics with coefficients of thermal expansion matching that of titanium have been developed. The purpose of this study was determine the bond strengths between cast and noncast pure titanium and two commercial titanium porcelains, and to compare the results with a conventional nickel-chromium alloy-ceramic system. The bond strengths were determined using a 3-point flexure test. Three-point flexure specimens $25{\times}3{\times}0.5mm$ were prepared After removal of ${\alpha}-case$ layer, they were veneered with $8{\times}3{\times}1mm$ of ceramics at the center of the bar. Specimens were tested in a universal testing machine. Within the limits of this study, the following conclusions were drawn: 1. The bond strengths between pure titanium and two commercial porcelains exceeded th lower limit of the bonding strength value in ISO 9693(25MPa). 2. There was no significant difference between cast and noncast titanium-porcelain bonds. 3. There was no significant difference between two commercial titanium porcelains. 4. The bond strengths of the titanium-porcelain systems ranged from 73% to 79% of that of the Ni-Cr-conventional porcelain system.

• 한국재료학회지
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• 제23권3호
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• pp.199-205
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• 2013

The mechanical properties and microstructures of aluminum-matrix composites fabricated by the dispersion of fine alumina particles less than $20{\mu}m$ in size into 6061 aluminum alloys are investigated in this study. In the as-quenched state, the yield stress of the composite is 40~85 MPa higher than that of the 6061 alloy. This difference is attributed to the high density of dislocations within the matrix introduced due to the difference in the thermal expansion coefficients between the matrix and the reinforcement. The difference in the yield stress between the composite and the 6061 alloy decreases with the aging time and the age-hardening curves of both materials show a similar trend. At room temperature, the strain-hardening rate of the composite is higher than that of the 6061 alloy, most likely because the distribution of reinforcements enhances the dislocation density during deformation. Both the yield stress and the strain-hardening rate of the T6-treated composite decrease as the testing temperature increases, and the rate of decrease is faster in the composite than in the 6061 alloy. Under creep conditions, the stress exponents of the T6-treated composite vary from 8.3 at 473 K to 4.8 at 623 K. These exponents are larger than those of the 6061 matrix alloy.