• Proceedings of the KAIS Fall Conference
• /
• 2012.05b
• /
• pp.671-673
• /
• 2012

본 연구에서는 상용 엔진 해석프로그램인 GT-Power를 이용하여 디젤엔진의 성능을 개선 개발을 위한 일차원 성능해석 모델을 개발하였다. 개발된 일차원 엔진 성능모델을 통하여 엔진의 출력, 토크 및 연비등을 검토하였다. 향후 터보챠져를 장착한 엔진개발에 사용이 가능하도록 터보매칭을 할 수 있는 모델을 추가하였으며, 향후 디젤엔진의 실험결과와 비교를 통하여 엔진 모델을 지속적으로 보완할 예정이다.

• Nuclear Engineering and Technology
• /
• v.18 no.2
• /
• pp.71-77
• /
• 1986

A one dimensional neutron kinetics program, BIK which is applicable to the safety analyses of PWR's is developed to analyze the reactor core in axial dimension. The BIK employs the finite difference technique in space and $\theta$-time integration method in time. Detailed models for the Doppler and moderator feedbacks and control rod motion are included. The benchmark of the nuclear model is carried out through the ANL benchmark problem and the time dependent nuclear power change in the rod ejection accident of KNU1 is calculated by BIK code. The results indicate that the BIK can predict the neutron dynamics with fair accuracy within the limits of one dimensional analysis and it is useful for the safety analyses of PWR's.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.10 no.4
• /
• pp.11-18
• /
• 2006

Compound flow by confluence of two parallel flows through a convergent channel and its choking phenomenon are calculated by one-dimensional isentropic model and completely mixing model. Optical observations and pressure measurements for subsonic/subsonic compound flows are carried out and compared with the results of one-dimensional calculations. As a result, it is found that inlet conditions of one flow influence the behavior of the other flow as well as the choking condition and present experimental data agree well with the results of one-dimensional calculations.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.24 no.6
• /
• pp.69-77
• /
• 2020

A quasi one-dimensional multi-phase reaction flow analysis code is developed for the performance analysis of liquid pintle thrusters. Unsteady flow field, droplet evaporation, finite reaction and film cooling models are composed as the major models of the performance analysis. The droplet vaporization takes account of Abramzon's vaporization model, and the combustion employs a flamelet model based on detail chemical reactions. Shine's model is applied for the film cooling calculation. To verify each model, the Sod shock tube, single droplet vaporization, kerosene droplets combustion, and film length are evaluated.

• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2010.11a
• /
• pp.213-216
• /
• 2010

A typical unsteady internal ballistic analysis model was proposed to take account of the erosive burning for a solid rocket motor. The variance of local velocity and pressure along grain surface are analyzed by using the continuity and momentum equation. The model introduced in this study showed good agreements with the results of previous internal ballistics program. It was investigated that the change of combustion pressure, gas velocity and regrestion rate along the grain axis.

• Journal of Energy Engineering
• /
• v.15 no.1 s.45
• /
• pp.1-7
• /
• 2006

The multi-dimensional two-phase flow models were developed for analyze the multi-dimensional behaviors or nuclear systems. To verify the simple turbulence model, The single phase mixing problem in a rectangular slab was calculated and compared with the commercial CFD code results. That result shows a good agreement with the CFD result. And the RPI Air-water experiments were simulated to assess the two-phase turbulence model in the multi-dimensional component. The first calculated distribution or void-fraction is highly dispersed and diffusive. It was revealed that the main reason is undesirable stratification force in a horizontal stratified flow regimes. Therefore the horizontally stratified flow regime is deleted because the stratified flow regime is not expected in multi-dimensional flow. With the modification of the flow regime, the predicted flow patterns and void fraction profiles are in good agreement with the measured data.

• The Korean Journal of Rheology
• /
• v.7 no.3
• /
• pp.192-202
• /
• 1995

이연구에서는 유변학 구성방정식이 나타내는 일차원 불안정성의 몇가지 예를 보였 다. 안정성 해석을 위하여 맥스웰형 미분구성방정식 Giesekus, Leonov, Larson 모델을 선택 하였다. 나타난 불안정성은 단순전단유동에서의 정상유동곡석이 무제한적 단수증가성을 위 배할 때 발생한다. 단순전단유동에 부과된 섭동하에서 Giesekus와 Larson 모델이 일정영역 의 무델계수와 전단율속도값에서 불안정 거동은 관성력을 고려하지 않은 경우에도 발생함이 증명되었다. 끝으로 이러한 불안정 거동을 개선하는 몇가지 방법을 Leonv와 Giesekus 모델 에 대하여 제시하였다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2005.11a
• /
• pp.136-140
• /
• 2005

By extending one-dimensional ZND detonation structure analysis model, a simple model for two-dimensional oblique detonation wave structure analysis is presented by coupling Rankine-Hugoniot relation and chemical kinetics for oblique shock wave and oblique detonation wave. Base on this study, two-dimensional fluid dynamics analysis is carried out to investigate the detailed unsteady structure of oblique detonation waves involving triple point, transverse waves and cellular structures. CFD results provide a deeper insight into the detailed structure of oblique detonation waves, and the simple model could be used as a unified design tool for hypersonic propulsion systems employing oblique detonation wave as combustion mechanism.

• Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
• /
• 2006.11a
• /
• pp.99-100
• /
• 2006

$BF_2$ molecule 이온주입은 ULSI기술에 있어서 ultra shallow 정합형성을 위해고 P-MOS를 제작하는데 매우 유용한 기술이다. 주입된 boron 이온의 분포를 위해서 $0.05{\mu}m$ 나노스케일의 마스크사이즈의 패턴에 이온 주입한 결과를 일차원적인 분포해석을 위해서 UT-Marlowe tool을 사용하여 gauss 및 pearson 모델의 도핑분포를 나타내었다. 또한 이 데이터를 TSUPREM4에 적용하여 이차원적인 도핑분포와 열처리 후에 boron의 gauss 및 pearson의 모델의 도핑분포를 본 논문에 나타내었다.

• Nuclear Engineering and Technology
• /
• v.24 no.2
• /
• pp.130-140
• /
• 1992

The physical benchmark problem on the direct-contact condensation under the horizontal occurrent stratified flow was analyzed using the RELAP5/MOD2 and /MOD3 one-dimensional model. Analysis was peformed for the Northwestern experiments, which involved condensing steam/water flow in a rectangular channel. The study showed that the RELAP5 interfacial heat transfer model, under the horizontal stratified flow regime, predicted the condensation rate well though the interfacial heat transfer area was underpredicted. However, some discrepancies in water layer thickness and local heat transfer coefficient with experimental results were found especially when there is a wavy interface, and those were satisfied only within the range.