• Journal of the Korea Convergence Society
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• v.9 no.1
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• pp.283-289
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• 2018

In automotive disc brake systems, frictional heat is not uniformly dispersed for reasons such as heat flux and thermal deformation. The thermoelastic deformation due to the frictional heat affects the contact pressure distribution and the contact load may be concentrated on the contact portion on the the disc brake surface, resulting in thermoelastic instability. In this study, thermal analysis and thermal deformation analysis considering the contact between disk and pad occurred during braking through 3D axial symmetry model with reference to the experimental equation and Kao's analysis method of contact pressure of disk and pad. ANSYS is used to analyze the thermal and elastic instability problems occurring at the contact surface between the disk and the pad, considering both the thermal and mechanical loads. A 3D axisymmetric model with direct contact between the disk and the pad was constructed to more accurately observe the thermal behavior of the disk by observing the frictional surface temperature, thermal deformation and contact thermal stress of the disk.

• Transactions of the Korean Society of Automotive Engineers
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• v.11 no.6
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• pp.93-100
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• 2003

This paper describes the thermoelastic instability arising from friction heat generation in braking and proposes the finite element methods to predict the variation of temperature and thermal deformation. In a conventional disc brake analysis, heat generation is only related with wheel speed and friction material and the interface pressure between disc and pad is assumed constant. But under dynamic braking conditions, the frictional heat causes the thermoelastic distortion that leads to more concentrated contact pressure distribution and hence more and more non-uniform temperature. In this paper, to complete the solution of the thermomechanically coupled problem, the linear relation model between pressure and temperature is proposed and demonstrated in examples of a simple two dimensional contact problem. And the two dimensional model has been extended to an annular three dimensional disc model in order to consider more realistic geometry and to provide a more accurate critical speed for automotive brake systems.

• Journal of the Korean Institute of Telematics and Electronics A
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• v.33A no.11
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• pp.105-111
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• 1996

We have invetigated the characteristics of thermal instability of Co-silicides annealed at 850$^{\circ}$C ~ 1000$^{\circ}$C for 10~90 minutes in a furance with N$_{2}$ ambient. In our experiments, Co-silicides and Co/Ti bilayer silicides were formed by depositing (Co, Ti) films on the clean Si substrates in an E-beam evaporator and performing the RTA annelaing. The sheet resistances of Co-silicides formed form Co exhibited the nearly constant value under the post-annealing time above 900$^{\circ}$C showing the increase of 30% and 60% under the conditions annealed at 900$^{\circ}$C and 1000$^{\circ}$C for 30minutes. On the other hand, there were no remarkable changes in the sheet resistance sof Co-silicides formed form Co/Ti bilayer under the post-annealing conditons below 1000$^{\circ}$C.

• The Magazine of the Society of Air-Conditioning and Refrigerating Engineers of Korea
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• v.17 no.4
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• pp.489-498
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• 1988

An analysis has been given for the effect of viscous dissipation on the thermal instability of plane Couette flow between two parallel plates maintained at different constant temperatures. Under the assumption that the principle of the exchange of stabilities holds, stationary disturbance quantities in the form of longitudinal vortices are considered. The magnitudes of disturbance quantities are then represented as fast convergent power series so that the eigenvalue problem for determining the onset conditions of the thermal instability may be reduced to a simplified problem of finding the roots of a $4{\times}4$ determinant. It is shown that as the magnitude of the visucous dissipation increases the flow becomes more susceptible to instabilities, which is in very good agreement with previous results obtained in some related researches.

• Journal of the Korean Institute of Gas
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• v.8 no.3 s.24
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• pp.8-15
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• 2004

This paper presents von Mises stress, deformation, and rotating distortion moment characteristics of inner tank bottom plate as a function of a cryogenic temperature difference along the radial distance from the center area to the corner one. The calculated results show that the filling level of LNG at the beginning of the cool-down process is very important for the design safety analysis of the inner tank. Obviously the thermal loading by a temperature difference between the LNG vapor gas of $-80^{\circ}C$ and a LNG temperature of $-162^{\circ}C$ affects to the thermal related characteristics of the bottom plates and annular one. From the computed results, the temperature difference by a vapor gas and liquid of LNG may lead to the thermal instability of the bottom plate. This phenomenon may cause the system failure of an inner tank.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.47 no.10
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• pp.695-704
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• 2019

In hypersonic regime, the complicated interaction between the air and surface of aircraft results in intensive aerodynamic heating on body. Provided this phenomenon occurs on a hypersonic vehicle, the temperature of the body extremely increases. And consequently, thermal deformation is produced and material properties are degraded. Furthermore, those affect both the aerothermoelastic stability and thermal safety of structures significantly. With the background, thermal safety and dynamic stability are studied according to the altitude, flight time and Mach number. Based on the investigation, design guideline is suggested to guarantees the structural integrity of hypersonic vehicles in terms of both of thermal safety and dynamic stability.

• Journal of the Korean earth science society
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• v.29 no.7
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• pp.579-585
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• 2008

The time-dependent evolution of disk mass for outburst limit cycle in a black hole microquasar is calculated based on the non-linear hydrodynamic model of thermally unstable accretion disk. The physical parameters such as black hole mass, disk size and mass transfer rate are adopted to reproduce the historical 1975 outburst observed in a prototype black hole X-ray nova A0620-00. The time-dependent effect of irradiation from the central hot region to the disk is considered in two ways: direct irradiation and indirect irradiation reflected from hot accretion flow above the disk. The accretion disk thermal instability model can account for the bolometric luminosity appropriate to typical characteristics of system luminosity observed in X-ray transients during the whole cycle of the outburst evolution. The maximum mass of the accretion disk, ${\sim}4.03{\times}10^{24}g$, is achieved at the ignition of an outburst, and the minimum value, ${\sim}8.54{\times}10^{23}g$, is reached during the cooling decay to quiescence. The disk mass varies ${\sim}5$ times during outburst limit cycle.

• Proceedings of the Korean Vacuum Society Conference
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• 2016.02a
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• pp.283.2-283.2
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• 2016

최근 ZnO는 무독성, 저가격, 수소 플라즈마에 대한 내구성 및 열적 안정성 등의 활발히 연구되고 있으며, III족 원소(Al, Ga, In) 불순물을 도핑하여 전기적 성질의 열적 불안정성을 해결하고 전기적 성질을 향상 시키고 또한 밴드갭 에너지가 3.3 eV 이상으로 증가하여 가시광선 영역에서 광투과율이 높은 투명도 전성 재료를 제공할 수 있다. 본 연구에서는 RF Magnetron Sputtering을 이용하여 내열성과 광학적 측면에서 우수한 성능을 가지는 PES 기판에 표면 에너지를 높이고 치밀한 구조의 박막을 증착하기 위해서 $O_2$ 플라즈마 처리를 하여 ZnO계 투명 전도막을 제작함으로써 투명전극에서 요구하는 $10^{-3}{\Omega}{\cdot}cm$ 이하의 낮은 비저항과 80% 이상의 광투과율을 가지는 방안에 대하여 연구하였다. PES 기판 위에 고밀도 $O_2$ 플라즈마를 이용하여 전 처리를 실시한 후 4인치의 Al-doped ZnO(ZnO 98 wt% : $Al_2O_3$ 2 wt%), AZO의 타겟을 이용하여 상온에서 RF Magnetron Sputtering 법으로 AZO 박막을 증착하였다. PES 기판상의 AZO 박막 두께가(100~400nm) 증가함에 따라 캐리어 농도와 홀 이동도가 점차 증가하는 경향을 보였다. 이는 박막 두께가 증가할수록 면저항과 비저항은 감소하며 결정립 크기가 커지고 결정입계에서 산란이 줄어들기 때문에 전기적 특성이 개선된 것으로 판단된다. 고밀도 $O_2$ 플라즈마 표면처리 시간이 증가함에 따라 플라스틱 기판의 결합에너지와 부착력이 증가하여 AZO 박막의 결정립 크기를 증가시키며, 접촉각은 감소하였다. 또한 급속열처리 온도가 증가함에 따라 전기적 특성과 광학적 특성이 향상됨을 확인할 수 있었다. 제작된 AZO 박막은 급속열처리 시간 10분에서 온도 $200^{\circ}C$일 때, 캐리어 농도 $2.32{\times}10^{21}cm^{-3}$, 홀 이동도 $4.3cm^{-2}/V$로 가장 높은 것을 확인할 수 있었고, 가장 낮은 비저항 $1.07{\times}10^{-3}{\Omega}{\cdot}cm$과 가시광 영역(300 nm ~ 1100 nm)에서의 AZO 박막의 광 투과율은 약 86%를 얻을 수 있었다.

• Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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• 2007.11a
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• pp.336-337
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• 2007

현재 투명전극의 재료로 ITO, ZnO, $SnO_2$등의 재료가 주로 이용되며, 낮은 저항률을 장점으로 가지는 ITO 박막이 가장 널리 이용되고 있으나, 가격이 비싸다는 단점을 가지고 있다. 이 밖에도 ITO 박막보다 가격이 저렴한 ZnO박막에 대한 연구가 많이 진행되고 있으나, 고온에서의 열적 불안정성 등의 문제로 상용화되지는 못하고 있다. 그러나 $SnO_2$ 박막은 ITO와 ZnO 박막보다 저항률이 다소 높지만, 우수한 열적, 화학적 안정성과 저렴한 가격으로 ITO 박막을 대체할 투명전도막 재료로 주목받고 있다. 본 연구에서는 $SnO_2$박막의 저항률 향상을 위하여 ATO(Antimony doped Tin Oxide) 박막을 RF Magnetron Sputtering 법으로 Coming glass위에 증착하였으며, 박막 증착시 산소 유량의 변화가 ATO 박막의 구조적, 전기적 그리고 광학적 특성에 미치는 효과를 연구하였다. 본 실험에서는 동작압력을 10 mTorr, RF power를 250W로 고정하고 $O_2$ 유량을 부분적으로 변화시키면서 증착되어진 ATO 박막을 분석한 결과 Ar:$O_2$의 비가 90:10일 때 최적의 가스비율로써 우수한 구조적, 전기적 그리고 광학적 특성을 보임을 확인하였다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2003.10a
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• pp.83-88
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• 2003

An analytical study was carried out to evaluate the regenerative cooling characteristics in the liquid rocket engine of a 10tf-thrust level using kerosene as a fuel. As a supplementary cooling method, a radiative cooling was applied to the nozzle extension. It was found out from this work that the cooling system with the regenerative and radiation cooling only is not adaptable as a cooling method for the liquid rocket engine of a 10tf-thrust level using kerosene as a fuel for the 2nd stage of the space launch vehicle. So, additional cooling method, curtain cooling was introduced and analyzed. Curtain cooling was very effective to reduce the thermal and thermo-structural instability.