• 한국자동차공학회논문집
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• 제18권1호
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• pp.131-138
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• 2010

Because real flow of engine exhaust is very hot and highly transient, it may cause thermal and inertial loads on catalyzed filters in DPF. Transient and detailed flow and thermal simulations are necessary in this field. To assess the importance of time dependent phenomena, typical cone-type configuration such as an underbody DPF is selected for steady and transient analysis. User defined functions of FLUENT by sinusoidal inlet velocities are written and integrated with main solver for realistic simulation. Also, 4-cylinder and 6-cylinder engines for 3,000 L class are considered for the dynamic exhaust effect of engine type. Key parameters to understanding of catalyst performance and durability issues such as flow uniformity index and peak velocity are investigated. Also, pressure drop for engine power are considered. From the simulation results for three different cases, proper approach is recommended.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2007년도 춘계학술대회논문집
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• pp.97-102
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• 2007

As environmental vibration requirements on precision equipments get more stringent, use of pneumatic vibration isolators becomes more crucial and, hence, their dynamic performance needs to be further improved. Dynamic behavior of those pneumatic vibration isolation tables is very important to both manufacturer and customer as performance specifications. Together with conventional transmissibility, transient response characteristics are another critical performance index especially when movements of components, e.g., x-y tables, of the precision equipments are very dynamic. In this paper, analysis on transient response of a pneumatic vibration isolation table loaded by a mass moving on it is presented. This is a conventional dynamics problem on a rigid body with 6 degree of freedom and a mass with another degree of freedom. How to obtain transient responses of the isolation table is described when the movements of the mass are prescribed relative to the table.

• 한국소음진동공학회논문집
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• 제16권9호
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• pp.926-936
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• 2006

In this study, structural vibration analyses of a smart unmanned aerial vehicle (UAV) have been conducted considering dynamic loads generated by rotating rotor and wakes. The present UAV (TR-S5-03) finite element model is constructed as a full three-dimensional configuration with different fuel conditions and tilting angles for helicopter, transition and airplane flight modes. Practical computational procedure for modal transient response analysis (MTRA) is established using general purpose finite element method (FEM) and computational fluid dynamics (CFD) technique. The dynamic loads generated by rotating blades in the transient and forward flight conditions are calculated by unsteady CFD technique with sliding mesh concept. As the results of present study, transient structural displacements and accelerations are presented in detail. In addition, vibration characteristics of structural parts and installed equipments are investigated for different fuel conditions and tilting angles.

• 대한기계학회논문집B
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• 제21권4호
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• pp.486-493
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• 1997

Experimental investigations on the comparison of developments between transient jets and evolving jet diffusion flames have been made in initial injection period. To achieve this experiment, an ignition technique using a residual flame as the ignition source is devised. High speed Schlieren visualizations, and measurements including jet tip penetration velocities and jet widths of the primary vortex are employed to examine the developing processes for several flow conditions. It is seen that the developing behaviors in the presence of flame are greatly different from those in transient jet, and thus the flow characteristics in the transient part are also modified. The discernible differences are shown to consist of the delay of the rollup of the primary vortex, the faster spreading after the rollup due to exothermic expansion, and the survival of only a primary vortex. The growth of primary vortex in the transient jet is properly explained through an impulsively started laminar vortex prior to the interaction. It is also found that the jet tip penetration velocity varies with elapsed time and an increase in Res gives rise to a higher tip penetration velocity.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2006년도 춘계학술대회논문집
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• pp.367-375
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• 2006

In this study, structural vibration analyses of a smart unmanned aerial vehicle (UAV) have been conducted considering dynamic loads generated by rotating rotor and wakes. The present UAV (TR-S5-03) finite element model is constructed as a full three-dimensional configuration with different fuel conditions and tilting angles for helicopter, transition and airplane flight modes. Practical computational procedure for modal transient response analysis (MTRA) is established. using general purpose finite element method (FEM) and computational fluid dynamics (CFD) technique. The dynamic loads generated by rotating blades in the transient and forward flight conditions are calculated by unsteady CFD technique with sliding mesh concept. As the results of present study, transient structural displacements and accelerations are presented in detail. In addition, vibration characteristics of structural parts and installed equipments are investigated for different fuel conditions and tilting angles.

• 한국소음진동공학회논문집
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• 제17권6호
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• pp.515-523
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• 2007

As environmental vibration requirements on precision equipments get more stringent, use of pneumatic vibration isolators becomes more crucial and, hence, their dynamic performance needs to be further improved. Dynamic behavior of those pneumatic vibration Isolation tables is very important to both manufacturer and customer as performance specifications. Together with conventional transmissibility, transient response characteristics are another critical performance index especially when movements of components, e.g., x-y tables, of the precision equipments are very dynamic. In this paper, analysis on transient response of a pneumatic vibration isolation table loaded by a mass moving on it is presented. This is a conventional dynamics problem on a rigid body with 6 degree of freedom and a mass with another degree of freedom. How to obtain transient responses of the isolation table is described when the movements of the mass are prescribed relative to the table.

• 조명전기설비학회논문지
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• 제24권5호
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• pp.62-69
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• 2010

본 논문은 매설지선의 과도접지임피던스의 임펄스전류의 인가위치와 대지구조에 대한 의존성에 관한것으로 다른 저항률을 가지는 토양에 매설된 길이 25, 50[m]인 매설지선의 과도접지임피던스와 규약접지 임피던스를 임펄스전류의 상승시간에 따라 측정하고 분석하였다. 그 결과, 매설지선의 과도접지임피던스는 유도성을 나타냈으며, 규약접지임피던스는 과도접지임피던스와 비슷한 경향성을 보였다. 매설지선의 접지저항은 임펄스전류의 인가위치에 관계없지만 특히 과도접지임피던스와 규약접지임피던스는 짧은 시간영역에서 임펄스전류의 인가위치와 대지저항률에 의존적이었다.

• 대한토목학회논문집
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• 제26권6B호
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• pp.623-631
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• 2006

본 연구에서는 하상변화가 존재하는 자연하천에서의 물질거동을 해석하기 위한 주기적저장대모형을 개발하였다. 저장대 구조에 따른 저장효과를 살펴보기 위하여 자연하천의 특성을 고려한 4개의 주기적 여울-소 구조를 갖는 와 흐름에서 소금물과 염료를 이용하여 실험한 모형실험결과를 이용하였다. 염료실험 결과, 물질이동 및 혼합거동은 하상 및 하안의 구조에 영향을 받는 것으로 나타났다. 기존의 저장대분산모형이 주기적으로 변화하는 저장대 구조에 의한 이동 및 질량교환 효과를 정확히 재현하지 못하는 것에 비해서 경계변화에 따른 질량교환 효과를 보다 효과적으로 재현할 수 있는 주기적저장대모형은 모형 실험 결과를 잘 재현하는 것으로 나타났다. 새로운 저장대모형을 미국 텍사스주의 Sabin River에 적용하였으며, 그 결과는 실험을 통해서 수집된 농도분포를 잘 재현하는 것으로 나타났다.

• Tribology and Lubricants
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• 제22권6호
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• pp.342-349
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• 2006

In this study, a dynamic behavior of rotor-bearing system used in CNG compressor has been investigated using the combined methodologies of finite elements and transfer matrices. The finite element is formulated including the field element for a shaft section and the point element for roller bearings. The Houbolt method is used to consider the time march for the integration of the system equations. The transient whirl response of rotating shaft supported on roller bearings is obtained, considering compression forces and unbalance forces at eccentric crank-pin part. And, the steady state displacements of the rotor are compared with a variation in stiffness coefficient of roller bearings. Results show that the loci of crankshaft considering unbalance forces and external compression forces are more severe in whirl motion than with only unbalance forces.

• 한국조명전기설비학회:학술대회논문집
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• 한국조명전기설비학회 2009년도 추계학술대회 논문집
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• pp.311-314
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• 2009

This paper presents the characteristics of grounding impedance of counterpoises buried at various soil structures. Grounding impedance measurements were made by the Fall-of-Potential method. The experiments were carried out in 50 m counterpoise of 25 $mm^2$ buried at a depth of 0.5 m. The test current was injected by the impulse generator having the front time of $1{\sim}60{\mu}s$. As a result, the soil structures greatly influences on the grounding impedance characteristics of counterpoise. The transient grounding impedances strongly depend on the injection mint and the front time of impulse current.