• The Journal of Advanced Prosthodontics
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• 제3권4호
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• pp.196-203
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• 2011

PURPOSE. This study evaluated marginal fit of glass infiltrated alumina cores fabricated using two techniques and their marginal stability after firing cycles of veneering porcelain. MATERIALS AND METHODS. Fifteen standardized all-ceramic crowns were fabricated on a metal die using each technique: slip cast technique of VITA In-Ceram sprint Alumina (Group A as control) and plastic foil matrix technique of Turkom-Cera fused alumina core system (Group B). Copings were compared between groups and within groups at coping stage and after firing each layer of veneering porcelain. A device was used to standardize seating of copings on the metal die and positioning of the specimens under the microscope after each stage of fabrication. The specimens were not cemented and marginal gap was measured using an image analyzing software (Imagepro Express) on the photographs captured under an optical microscope. Two tailed unpaired 't test' was used to compare marginal gaps in two groups and one way ANOVA was used to analyze marginal distortion within each group at 95% confidence interval. RESULTS. The marginal gap was smaller at the coping stage in group B ($60+30{\mu}M$) than group A ($81+21{\mu}M$) with statistical significance. After firing of veneering porcelain the difference was insignificant. At the final stage, both groups exhibited lower mean marginal gaps than at the initial coping stage with the difference of $11.75{\mu}M$ for group A and $11.94{\mu}M$ for group B, but it was statistically insignificant due to high value of standard deviation. CONCLUSION. Within the limitations of this study, it was concluded that both techniques produced copings with comparable and acceptable marginal fit and marginal stability on firing veneering porcelain.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2006년도 추계학술대회논문집
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• pp.840-843
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• 2006

The determination of firing order is very significant procedure in initial stage of design for medium speed diesel engine. Generally, the selection of firing order has been accomplished in view of minimum excitation forces condition. In this paper all possible firing orders under the given number of cylinder were considered to decide the optimum. Meanwhile torsional vibration characteristics using the phase vector sum method and minimum excitation force concept were applied. From these results, some superior cases were selected. And then, the torsional vibration response analysis and the resonance characteristics of engine structure were investigated for the final decision.

• 한국군사과학기술학회지
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• 제19권2호
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• pp.227-235
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• 2016

Heavy-weight high speed underwater vehicle(HSUV) is launched from the submerged mother ship. For the safety point of view, it is important to confirm whether the HSUV would touch the launching mother ship. In this paper, the hydrodynamic force and moment were modeled by the polynomials of motion variables and the simple lift and drag acting on a plate and cylinder which consist of the HSUV's several parts. The mother ship was assumed as the Rankine half body to consider the flow field near the moving ship. Such hydrodynamic force and moment were included in the 6 DOF equations of motion of the HSUV and the dynamic simulations for the various conditions of the HSUV until the propeller activation were performed. Developed simulation program is expected to reduce the number of expensive sea trial test to develop safety logic of the HSUV at the initial firing stage.

• 항공우주기술
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• 제6권2호
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• pp.96-103
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• 2007

정지궤도 위성의 전이궤도 해석 과정의 중요한 부분인 LAE(Liquid Apogee Engine, 액체원지점엔진) 분사전략 수립을 위한 프로그램을 개발하였다. 본 프로그램에서 다루고 여는 LAE 분사전략 수립은 전이궤도 해석의 첫 단계로서, 초기 전이궤도 요소와 지상 TT&C 중계소의 위치, 위성체 성능 파라미터를 입력받아 여러 제한 조건을 만족하면서 선택 가능한 분사 전략들을 계산하는 과정이다. 본 연구에서 개발된 프로그램은 일반적인 LAE를 사용하는 정지궤도 위성을 대상으로 하였으며 최대 여섯 개의 예비 분사 전략과 최대 6회까지 LAE를 분사하는 상황을 가정하였다. 본 프로그램에서 입출력 부분에는 MS-엑셀이 사용되었으며 계산 과정은 MATLAB 함수를 사용하여 구현되었다.

• 한국세라믹학회지
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• 제21권3호
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• pp.245-252
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• 1984

Willemite phosphor is a good one having excellent luminescence efficiency that it;s emission wavelength is in the range of about 525 nm. The energy band gap of this willemite phosphor is about 4.1 eV. When the ratio of ZnO/SiO is 1.8 and Mncl in used as activator source the phosphor has the value of maximum luminescence efficiency. The characteristic of willemite phosphor is tendency of the dependence of temperature. The willemite which was fired with activator after being synthesized at initial firing without activator shows higher value of luminescence efficiency than willemite which was fired with activator in initial stage, When the concentration of activator is 1-1.5mol% it has its most favorite condition and the value of luminescence efficiency decreases according to increasement of activator concentration.

• 한국소음진동공학회논문집
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• 제16권4호
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• pp.319-328
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• 2006

4-실린더 엔진의 작동 시 크랭크샤프트의 기계적 거동을 해석하는 방법에 관한 연구 논문이다 이 해석의 목적은 모드 해석을 단순화 하기위해 Pin 과 Arm을 일정하게 가정하고, 이를 통해 단순화된 크랭크샤프트의 특성을 연구하는 것이며, 해석을 통하여 얻어진 전달 함수에서의 고유진동수와 모드 형상을 실험을 통한 모드 해석과 비교하였다. 시뮬레이션을 통한 결과와 실험을 비교한 결과 해석치와 실험치의 값이 일치함을 확인할 수 있었고 이를 통하여 해석 모델을 검증하였다. 또한 검증된 모델을 통하여 엔진 작동 시 크랭크샤프트의 특성을 해석하고자 하였다. 초기 연소 조건에 기초하여 주파수 영역에서 크랭크샤프트의 동적 거동을 해석하기 위한 새로운 방법을 기술하였다. 새로운 기법은 엔진의 작동 조건에서 저널 베어링과 밸런서의 형상 변경을 통하여 얻어진 에너지 값을 계산하기 위해서 RMS값을 이용하였다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2003년도 추계학술대회
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• pp.1121-1126
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• 2003

Strength evaluation was carried out for the fillet and oil hole of crankshaft of medium speed diesel HiMSEN engine to verify initial concept design. Alternating torque obtained from torsional vibration analysis and radial force due to firing pressure were applied. It was assumed that the maximum alternating torque and radial force occur simultaneously. Weak points in view of fatigue are proceeding fillet and crank pin fillet area and the minimum normalized fatigue safety factor is 1.17 at crank pin fillet. The fatigue strength of the oil hole was evaluated to verify the effect of the surface roughness of the oil hole. As results, the specific level of the inner surface roughness and the polishing depth of the oil hole for sufficient fatigue strength was suggested. The maximum stress value and stress distribution at the inner surface of the oil hole can be easily estimated at initial design stage by the newly developed method.

• 한국콘텐츠학회논문지
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• 제18권8호
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• pp.118-126
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• 2018

교전 초기에 높은 위협도를 가진 다수의 표적에 대해 적을 신속하게 제압하기 위해서는 단 시간 내에 가능한 많은 무장을 발사할 수 있도록 적시에 효과적인 무장 할당을 수립하여 교전 효과를 극대화하는 것이 중요하다. 본 논문에서는 다표적 다무장 환경에서 신속 대응 무기 체계를 위한 무장 할당 알고리즘을 제안한다. 제안하는 알고리즘에서는 무장군 별 방위각 크기 기준으로 표적을 정렬하여 방위각 기준으로 표적군-무장군 간 집단 할당을 수행한 후, 산출된 표적의 위협도 기준으로 표적-무장 간 개별 할당을 수행하여 복잡도 낮은 연산으로 신속 대응이 가능한 사격 계획을 수립하여 교전 효과를 극대화한다. 본 논문에서는 제안하는 알고리즘의 시뮬레이션 및 가시화를 통해 성능 평가 및 검증을 수행하였다. 성능 평가 결과, 제안하는 알고리즘은 대규모의 전장 환경에서도 빠른 시간 내에 높은 표적 할당률을 보이는 효과적인 무장할당을 수행함으로써 신속 발사 무기 체계에 적용할 시에 높은 효용성 및 효과가 기대된다.