• 항공우주기술
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• 제13권1호
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• pp.96-107
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• 2014

한국항공우주연구원(이하, 항우연)은 2017년에 시험용 달 궤도선을 2020년에 달 궤도선 및 착륙선 발사를 계획하고 있다. 달 궤도선이 달 궤도 진입(LOI) 기동을 수행할 경우 온 보드에 탑재된 유한 분사 방식의 추력기를 이용하기 때문에 임무계획 단계에서 이러한 내용을 고려하여 LOI 기동 전략을 수립해야 한다. 유한 분사 모델을 이용한 LOI 기동 전략 및 요구되는 속도증분(${\Delta}V$)은 분사시점의 위성 자세, 추진체의 종류, 추력기의 추력 레벨 및 분사 시점에 따라서 달라진다. 본 논문은 해외 우주국 달 궤도선의 LOI 기동 사례를 기술하고, 이를 기반으로 한국형 달 궤도선의 LOI 기동 전략을 구체화 하였다. 또한 이와 관련된 시뮬레이션을 수행함으로써 한국형 달 궤도선에 적합한 추력 레벨 및 분사 시점 등을 도출하였다.

• 한국전산구조공학회논문집
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• 제25권3호
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• pp.211-217
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• 2012

본 연구에서는 유리단섬유로 보강된 분사식 섬유보강 복합재료의 인장거동 평가를 위한 실험 및 해석연구를 수행하였다. 이를 위해 다양한 변형율속도(strain rate)에 따른 에폭시수지 및 분사식 섬유보강 복합재료의 인장강도 실험을 수행하였다. 본 연구에 사용된 분사식 섬유보강 복합재료는 15mm 길이로 절단된 유리단섬유가 25% 부피비율로 혼입된 보수 보강용 재료이다. 에폭시수지의 점탄성 특성을 고려하기 위해 역산모델링(inverse simulation)을 수행하여 변형율속도에 따른 점성변화를 함수식으로 제안하였다. 역산모델링을 통해 제안된 함수식을 미세역학 기반의 점탄성 손상모델(micromechanics-based viscoelastic damage model; Yang et al., 2012)에 적용하여 분사식 섬유보강 복합재료의 인장거동을 수치적으로 해석하였다. 분사식 섬유보강 복합재료의 인장거동 해석결과와 실험결과를 비교하여 미세역학 기반의 점탄성 손상모델의 정확성을 검증하였다.

• 건축역사연구
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• 제19권5호
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• pp.81-98
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• 2010

In the middle of the 8th century, we met the new high-rise building, the 7th storied wooden pagodas in 'Kokubunji' in Japan. I tried to analyze and study this building to show how the wooden pagoda had changed itself because of appearance of new style. The conculusions are as follows; 1. The construction of the foundation was mainly composed namely 'Panchuk'. It was proceeded by two ways. One is the earthen-digging, laying foundations named 'Gulkwangpachuk' and the other is simply laying foundation named 'Jisangpanchuk'. In that period, due to the progress of the technique, we assumed that the main stream is 'Jisangpanchuk'. 2. The elevation of base was mostly the single foundation from archaeological study. The material was stone. The middle case of pagoda had the base of tile-roofed. We knew the just one pagoda had the base of brick, but that was not main stream. 3. The new device had appeared in the central base stone. It was the stone point. But in that period the existing method, a hole style and the new style was used in the central base stone. This fact is showed that the central government was not hold the reigon(it names 'Kook') in the respect of the technique. 4. The plan scale is classified of 3 group. As a result, the first body is larger, the main-unit and the sub-unit is a equal unit. But smaller, the length of main-unit is longer than the one of sub-unit. And the very small pagoda was build in that period.

• 한국방사성폐기물학회:학술대회논문집
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• 한국방사성폐기물학회 2008년도 학술논문요약집
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• pp.137-138
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• 2008

• 세라미스트
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• 제12권4호
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• pp.78-88
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• 2009

• 대한기계학회논문집B
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• 제35권10호
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• pp.1061-1066
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• 2011

본 연구에서는 절삭가공 시 생산성 향상을 위해 사용되는 고압분사 홀더(hp holder)에 들어가는 노즐의 유동특성을 파악하였다. 집중형의 노즐 분사형태를 유지하면서 분사되는 유동에 영향을 주는 설계인자로 입구 유입속도, 노즐 유입각도, 노즐 출구직경을 설정하여 이에 대한 수치해석을 수행하였다. 그 결과 입구 유입속도가 높을수록, 노즐 출구직경이 작을수록 분사되는 유체의 압력과 속도가 높은 것으로 나타났다. 노즐 유입각도의 경우에는 각도변화에 따른 유동특성의 차이가 크지 않았지만 약 $15^{\circ}$일 때가 가장 높은 유동특성을 보였다. 또한 결과값을 이용하여 분사되는 유체의 힘에 의해 가공 시 발생하는 칩의 제거 가능 여부를 확인해 보았다.

• 대한기계학회논문집B
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• 제22권9호
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• pp.1255-1266
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• 1998

Effects of a length-to-diameter ratio, L/D, on the three-dimensional flow and aerodynamic loss within an injection hole, which is normally oriented to the mainflow, have been investigated by using a straight five-hole probe. The length-to-diameter ratio of the injection hole is varied to be 0.5 and 2.0 for blowing ratios of 0.5, 1.0 and 2.0. Regardless of the blowing ratio, flows within the hole and at the jet exit are strongly affected by the length-to-diameter ratio. In the case of L/D=0.5, the inside flow is considerably influenced by the mainflow, and the exit flow variation is found to be the greatest. The aerodynamic loss in this case is usually attributed to jet -mainflow interactions. In the case of L/D=2.0, the flow separation and reattachment in the inlet region are completely separated from the complicated exit flow, and the aerodynamic-loss production is mainly due to the inlet flow separation.

• 한국전산유체공학회지
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• 제4권3호
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• pp.21-27
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• 1999

In this paper, tile characteristics of flow resulting from the configurations of piston head and intake-port of the cylinder in a gasoline-direct-injection engine are investigated numerically. Calculations are carried out from intake process to the end of compression. GTT code which includes the third order upwind Chakravarthy-Osher TVD scheme and κ-ε turbulence model with the law of wall as a boundary condition. As a result, a piston head with a smaller radius of curvature and larger radius gives stronger reverse tumble. It is also shown that as the maximum tumble ratio increases by the configuration of the intake-port the tumble ratio at the end of compression stroke increases. It is concluded that flows at the end of compression stroke can be controlled by the optimum design of intake-port and piston head.

• 한국분무공학회지
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• 제6권4호
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• pp.39-48
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• 2001

The Gasoline Direct Injection(GDI) system has been highlighted due to the improvement of fuel consumption and the control of exhaust emission from gasoline engines. Main purpose of the present study is to measure spray characteristics of GDSI for real engine application. We have investigated experimentally spray tip penetration, spray angle, tip velocity and spatial spray distribution. Counter-rotating vortex grown on the spray surface plays an important role in the spray characteristics. Accordingly the spray tip penetration and tip velocity do not excess 50mm, 20m/s respectively, under 0.6MPa ambient pressure. the spray cone angle of GDSI have a same tendency to a simplex swirl atomizer.

• 한국생산제조학회지
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• 제20권6호
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• pp.793-798
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• 2011

In this study, it was grasped to the flow characteristics of cutting fluid injected by nozzle installed in high pressure holder for avoiding chip curling occurred during machining process. And for avoiding chip curling, the possibility of elimination under various chip conditions was checked. Consequently, the highest discharging pressure and velocity was shown in 150 of nozzle inflow angle. Also as nozzle outlet diameter is small, the pressure and velocity of injected flow are high. Moreover, It could be confirmed that width and thickness of chip have no direct effect on chip elimination and it is achieved by torque generated by injected cutting fluid.