• Journal of the Korean Society of Propulsion Engineers
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• v.14 no.5
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• pp.101-110
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• 2010

Dual pulse rocket motor is a solid motor with two grains separated by a bulkhead and rupture disc. The elasto-plastic explicit dynamic analysis for the rupture disc was conducted by finite element method. The effect of the slit geometry of a rupture disc was parametrically analyzed in terms of rupture time and shape. The results can be used to control the rupture pressure by changing the slit geometry of rupture disc.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2010.05a
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• pp.105-112
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• 2010

Dual Pulse Rocket Motor is a solid rocket motor with two grains separated by a bulkhead and rupture disc. The elasto-plastic explicit dynamic analysis of rupture disc was conducted by finite element method. The effect of the slit geometry of a rupture disc was analyzed for rupture time and shape by the parametric study. The results can be used to control the rupture pressure by the change the slit geometry of a rupture disc.

• Proceedings of the KSME Conference
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• 2000.04b
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• pp.704-708
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• 2000

A new efficient numerical method for computing unsteady, incompressible flows, DRANS (Decoupled Reynolds-Averaged Navier-Stokes), is presented. To eliminate the restriction of CFL condition, a fully-implicit time advancement in which the Crank-Nicolson method is used fer both the diffusion and convection terms. is adopted. Based on decomposition method, the velocity-turbulent quantity decoupling is achieved. The additional decoupling of the intermediate velocity components in the convection term is made for the fully-implicit time advancement scheme. Since the iterative procedures for the momentum, ${\kappa}\;and\;{\varepsilon}$ equations are not required, the components decouplings bring fourth the reduction of computational cost. The second-order accuracy in time of the present numerical algorithm is ascertained by computing decaying vortices. The present decoupling method is applied to turbulent boundary layer with local forcing.

• Electronics and Telecommunications Trends
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• v.23 no.2 s.110
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• pp.46-55
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• 2008

융합환경 하에서 새로운 기술과 서비스의 제공이 가능해지고 차세대 네트워크의 투자가 확대되면서 미래 통신시장에서 유선부문 지배적 사업자의 시장지배력이 전이될 가능성이 높아지고 있다. 이러한 통신시장의 환경변화에 대응하여 영국, 이탈리아, 스웨덴, 아일랜드 등 유럽의 많은 국가가 구조분리를 추진하였거나 진행중에 있다. 또한 EU는 2007년 11월 통신법 개정안을 통해 EU 27개 회원국 규제기관에 영국식 기능분리 권고안을 제안하였고, 개별 회원국의 찬성을 전제로 2009년 구조분리가 현실화 될 예정이다. 특히 EU의 통신법 개정안은 기존 병목설비에 적용되던 필수성과 독점성의 원칙을 상당히 탄력적이고 포괄적으로 해석하고 있다. 또한 유선시장의 경쟁 상황이 점차 개선되고 있음에도 구조분리를 강력하게 추진하고 있다. 이처럼 컨버전스 환경에 대비한 EU 및 유럽 각국의 강력한 구조분리 추진현황은 유선시장의 경쟁이 활발하지 않고, 구조분리 논의가 필수설비의 필수성과 독점성의 원칙에서 진전되지 못하고 있는 우리나라의 유선시장에 많은 시사점을 제시하고 있다.

• Proceedings of the Membrane Society of Korea Conference
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• 1994.04a
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• pp.39-42
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• 1994

산소와 질소는 공업적으로 공기를 분리하여 생산하는데, 이 분리공정에는 심냉법 (cryogenic distillation), PSA법 (pressure swing adsorption) 그리고 분리막법 등이 사용되고 있다. 현재는 위의 세가지 공정중에서 PSA법이 가장 널리 채택되고 있는 공정이다. 그런데, 고분자막을 이용하는 분리공정은 설비투자면에서 뿐만 아니라 에너지 절약측면에서 큰 이점을 갖고 있기 때문에 최근 들어 점차 주목 받고 있다 [1]. 그러나, 고분자막에서의 기체의 투과도와 선택도는 서로 상반적인 관계 (trade-off)에 있기 때문에 공기중의 산소와 질소의 분리를 위해서는 기존의 고분자들에 비해 투과도와 선택도가 동시에 개선된 새로운 막 소재의 개발이 절실하므로 이에 대한 연구가 활발히 진행되고 있다 [2].

• Proceedings of the KIEE Conference
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• 2001.04a
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• pp.150-152
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• 2001

근래 들어 소용량의 디스크형 발전기(disk type generator)가 여러 분야에서 이용되면서 기존 모델보다 개선된 특성을 나타내는 새로운 구조에 대한 연구가 진행되고 있다. 본 논문에서는 분리형 슬롯 구조를 지니는 디스크형 발전기를 제안하였고 그 특성을 해석하여 기존 모델과 비교함으로써 우수성을 입증하였다. 제안된 모델의 3차원 자계 해석을 위해서 체적적분방정식법(VIEM)을 이용하였다. 전기자와 계자의 상대 위치에 따른 자속 밀도 분포와 직렬 코일 내부의 총 자속량을 체적적분방정식법을 통하여 정확하게 계산하고 여기서 구해진 자속량에 대한 몇 가지 후처리 과정을 통해서 발전기의 주요 특성들을 구했다. 이 결과를 동일한 설계 제한 사항을 고려한 기존 모델의 결과와 비교하여 제안된 구조를 지니는 디스크형 발전기의 우수성을 입증하였고 실제 설계에도 활용이 가능하도록 했다.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.27 no.4
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• pp.458-465
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• 2003

The main objective of the research is to develop a research code solving transient incompressible Navier-Stokes equation. In this research code, Adams-Bashforth method was applied to the convective terms of the navier stokes equation and the splitted equations were discretized spatially by finite element methods to solve the complex geometry problems easily. To reduce the divergence on the boundaries of pressure poisson equation due to the unsuitable pressure boundary conditions, multi step approximation pressure boundary conditions derived from the boundary linear momentum equations were used. Simulations of Lid Driven Flow and Flow over Cylinder were conducted to prove the accuracy by means of the comparison with results of the previous workers.

• Journal of the Korean Geotechnical Society
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• v.29 no.7
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• pp.57-74
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• 2013

In this study, the virtual fixed point analysis and 3D full-modeling analysis for pile bent structures are conducted by considering various influencing factors and the applicability of the virtual fixed point theory is discussed. Also, a discrete analysis calculating separately both the superstructure and substructure of pile bent structures is performed on the basis of an equivalent base spring model by taking into account the major influencing parameters such as soil conditions, combined loading and pile diameter. The results show that the settlement and lateral deflection of the virtual fixed point theory are smaller than those of 3D full-modeling analysis. On the other hand, the virtual fixed point analysis overestimates the axial force and bending moment compared with 3D full-modeling analysis. It is shown that the virtual fixed point analysis cannot adequately predict the real behavior of pile bent structures. It is also found that discrete analysis gives similar results of lateral deflection and bending moment to those of unified analysis. Based on this study, it is found that discrete analysis considering column-pile interaction conditions is capable of predicting reasonably well the behavior of pile bent structures. It can be effectively used to perform a more economical design of pile bent structures.

• Journal of the Korean Geotechnical Society
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• v.27 no.5
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• pp.33-43
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• 2011

In this study, simplified analysis (discrete analysis of column and pile) of pile bent structures was performed on the basis of the equivalent base spring model. And the minimum reinforcement ratio in pile bent structures was evaluated by taking into account various factors. To obtain the detailed information, simplified analysis was performed for column-pile interactions and the behavior of a column-pile was estimated and highlighted. Based on this study, it is shown that previous design method based on virtual fixed point theory cannot adequately predict the physical behavior of pile bent structures. It is found that the maximum bending moment is located within craking moment of the pile when material non-linearity is considered. It is also found that the minimum reinforcement ratio (=0.4%) is appropriately applicable for the optimal design of pile bent structure under ultimate lateral loading.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2010.11a
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• pp.261-264
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• 2010

Dual Pulse Rocket Motor is a solid rocket motor with two grains separated by a bulkhead and rupture disc. The elasto-plastic explicit dynamic analysis of rupture disc was conducted by the finite element method. The effect of the slit geometry of rupture disc with radial slit was parametrically analyzed in terms of rupture time and shape. The results can be used to control the rupture pressure by changing the slit geometry of rupture disc.