• Journal of Power System Engineering
• /
• v.13 no.6
• /
• pp.22-28
• /
• 2009

열역학 제 2법칙의 관점의 열역학적 가용에너지인 엑서지 해석법을 적용하여 가솔린, 메탄올, M90 연료를 사용한 전기점화 기관의 성능해석을 수행하였다. 열역학적 사이클 해석을 위하여 사이클을 구성하는 각 과정은 열역학적 모델로 단순화하였고, 크랭크 각도에 따른 실린더의 압력과 작동유체를 구성하는 연료, 공기 및 연소생성물의 열역학적 물성 값들을 이용하여 각 과정에서의 엑서지와 손실 일을 계산하였다. 실험데이터는 단기통 전기점화기관을 가솔린, 메탄올과 M90(메탄을 90%+부탄 10%의 혼합연료)을 연료로 WOT(Wide Open Throttle), MBT(Minimum advanced spark timing for Best Torque), 2500rpm 조건으로 운전하여 측정하였다. 계산에 이용한 자료는 실험으로 측정한 크랭크 각도에 따른 연소실의 압력, 흡입공기와 연료유량, 흡입공기 온도, 냉각수 온도와 배출가스 온도 등이다. 이를 이용하여 각 과정에서의 엑서지와 손실 일을 계산하였으며 각 과정에서의 손실 일은 연소과정에서 가장 크며 팽창과정, 배출과정, 압축과정 및 흡입과정 순으로 크게 나타났다.

• Proceedings of the Korea Water Resources Association Conference
• /
• 2007.05a
• /
• pp.810-814
• /
• 2007

최근 제방개수 혹은 하폭확장과 같은 기왕의 제방대책을 적용하기 힘든 도시지역의 홍수피해 저감방안의 일환으로 개수로 혹은 지하터널 형식의 방수로와 같은 구조적 대안이 제시되고 있다. 현재 국내에서 검토되고 있는 방수로의 형식은 주로 유입부와 유출부의 양 지점 수두차에 의한 만관 상태의 흐름형식이다. 본 연구에서는 수두차에 의한 만관 상태의 흐름을 가지고 있으며, 3개 지점이상의 유입부를 가진 지하터널 형식의 방수로 계획시 마찰손실, 유입손실, 만곡부손실 등을 고려하여 유입부, 유출부 지점 계획에 따른 터널의 연장, 직경 등 제원 결정을 위하여 기존에 제시되어 있는 2개 저수지 유입시 정상상태 만관 흐름해석방법을 확장하여 3개 이상 저수지 유입시 정상상태 만관 흐름해석을 할 수 있도록 하였다.

• Journal of Korea Water Resources Association
• /
• v.48 no.2
• /
• pp.127-136
• /
• 2015

In general, XP-SWMM regards manholes as nodes, so it can not consider local head loss in surcharged manhole depending on shape and size of the manhole. That might be a reason why XP-SWMM underestimates inundated-area compared with reality. Therefore, it is necessary to study how we put the local head loss in surcharged manhole in order to simulate storm drain system with XP-SWMM. In this study, average head loss coefficients at circular and square manhole were estimated as 0.61 and 0.68 respectively through hydraulic experiments with various discharges. The estimated average head loss coefficients were put into XP-SWMM as inflow and outflow energy loss of nodes to simulate inundation area of Gunja basin. Simulated results show that not only overflow discharge amount but inundated-area increased considering the head loss coefficients. Also, inundation area with considering head loss coefficients was matched as much as 58% on real inundation area. That was more than simulated results without considering head loss coefficients as much as 18 %. Considering energy loss in surcharged manholes increases an accuracy of simulation. Therefore, the averaged head loss coefficients of this study could be used to simulate storm drain system. It was expected that the study results will be utilized as basic data for establishing the identification of the inundation risk area.

• Journal of the Korea Academia-Industrial cooperation Society
• /
• v.13 no.12
• /
• pp.5696-5703
• /
• 2012

In this study, the characteristics of filter that make up the automotive airbag system were analyzed. The gas pressure change of airbag is directly impacted by the filter. However, it is uncertain how much the design factors of filter affect the pressure of airbag. And it is difficult to access the pressure loss coefficient in the respect of characteristics of the airbag filter in the simulation method. To solve this problem, this study suggests pressure loss coefficient of the filter using simulation analysis. But it is impossible to interpret a sudden increase of pressure such as airbag filter. To solve this problem, by applying interpolation and scale down method, analysis was processed. Also, through the simulation interpretation of airbag filter's pressure loss coefficient, the guidelines for the filter design could be suggested.

• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2008.05a
• /
• pp.263-267
• /
• 2008

In this work the realistic install performance analysis of a helicopter was performed together with power extraction enabling to operate auxiliary system as well as intake pressure loss, loss due to bleed air, etc. which must be considered in practical propulsion system's performance modelling to be installed to the airframe. The pressure loss occurring in intake was estimated from the intake performance map with relationships of Mach Number and pressure loss. In order to evaluate the proposed installed performance model, the experimental data for comparison must be needed when mounted in propulsion system. However because of lack of accessibility to such real data at the moment, the alternative way was made through comparison that the analysis results by the proposed model were compared with a wellknown commercial program GASTURB's analysis results. The validity of the proposed installed performance model was consequently confirmed because its average deferences from the GASTURB's results were within 0.5%.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.12 no.1
• /
• pp.51-56
• /
• 2008

In this work the realistic install performance analysis of a helicopter was performed together with power extraction enabling to operate auxiliary system as well as intake pressure loss, loss due to bleed air, etc. which must be considered in practical propulsion system's performance modelling to be installed to the airframe. The pressure loss occurring in intake was estimated from the intake performance map with relationships of Mach Number and pressure loss. In order to evaluate the proposed installed performance model, the experimental data for comparison must be needed when mounted in propulsion system. However because of lack of accessibility to such real data at the moment, the alternative way was made through comparison that the analysis results by the proposed model were compared with a wellknown commercial program GASTURB's analysis results. The validity of the proposed installed performance model was consequently confirmed because its average deferences from the GASTURB's results were within 0.5%.

• Proceedings of the Acoustical Society of Korea Conference
• /
• 1998.06c
• /
• pp.319.1-321
• /
• 1998

판 구조물의 전달 손실은 효과적인 차음 설계를 위한 필수적인 지표 중 하나이다. 특히, 흡/차음재 부착등 적층에 의한 차음 성능의 변화 예측이 중요하다. 실제의 차음 구조물은 유한한 크기를 갖게 마련인데, 현재까지는무한 판 이론에 제한각이나 경계 손실등을 적용하여 그 값을 산출함으로써 판의 유한효과를 고려하였지만, 해석의 임의성으로 인해 일반적인 적용이 어렵다. 이에 본 연구에서는 흡음재가 부착된 유한한 면적을 갖는 적층판의 음향 전달 손실을 임계 주파수 미만의 주파수 대역에 대해 예측하고 흡음재의 부착에 따른 전달 손실의 변화를 관찰하였다. 판은 무한한 강체 배플위에 있다고 가정하였고, 모드 전개법을 응용하여 개개의 판모드들의 거동을 고려하였다. 여기서 흡음재는 공극질 재료로 가정하여 Biot의 이론을 적용하였다. 해석 결과로부터, 흡음재등이 부착된 적층판에 대해서는 일반적인 제한각의 적용이 어렵고, 그 영향을 충분히 고려할 수 있는 새로운 예측 도구의 필요성을 확인하였다.

• Proceedings of the KIPE Conference
• /
• 2008.06a
• /
• pp.58-60
• /
• 2008

본 논문에서는 영전압 스위칭 풀브릿지 DC-DC 컨버터의 회로방식에 대한 전력변환 효율 특성을 빠르고 효과적으로 분석 할 수 있는 방법에 대해 보고한 것이다. 먼저 기존회로에서 내부손실이 없는 이상적인 등가회로를 유도하고 스위칭 동작 파형을 이용하여 주요부분에 대한 전류의 실효값을 유도하였다. 이상적인 등가회로에 내부손실 저항을 삽입하고 전류의 실효값으로부터 주요소자의 전도손실을 계산하여 컨버터의 전력변환손실과 효율을 예측할 수 있도록 하였다. 해석 방법의 타당성을 검토하기 위해서 입력전압 400V, 출력전압 12V, 최대전력 720W의 시험용 회로를 구성하여 해석 결과와 비교 하였다.

• The Magazine of the Society of Air-Conditioning and Refrigerating Engineers of Korea
• /
• v.7 no.3
• /
• pp.160-166
• /
• 1978

Heat loss to the ground in ondol heating system is analyzed mathematically using conformal mapping and variable transformations, Both two-and three-dimensional systems are analyzed. Heated house is assumed to be rectangular shape. Mean value of heat loss to the ground can be obtained using Figure 2. Effects of thermal parameters to heat loss are discussed. Numerical examples are also given.

• Composites Research
• /
• v.12 no.2
• /
• pp.26-35
• /
• 1999

This paper presents the vibration damping characteristic of a single lap joint beam with partial dampers analyzed using the model strain energy method and the harmonic response analysis which were based on a finite element model. The two finite element analysis methods exhibited very similar results of the resonant frequency and system loss factor which were comparable to those by the theoretical analysis. Effects of the location of partial dampers and elastic moduli and thickness of their layers on the system loss factor were studied. The damping effects due to changes of modules and loss factor of the viscoelastic layer in lap joint and partial dampers were also studied. Consequently, the geometrical and material conditions at maximizing the system loss factor were suggested.