• 한국전산유체공학회:학술대회논문집
• /
• 한국전산유체공학회 2008년도 춘계학술대회논문집
• /
• pp.332-336
• /
• 2008

A pulsation damper is usually mounted on the fuel rail to diminish undesirable noise in the vehicle cabin room. However, pulsation dampers are quite expensive. Therefore, several studies have focused on reducing fuel pressure pulsations by increasing the self-damping characteristics of the fuel rail. This paper is a basic study in the development of a fuel rail that can reduce pulsations via a self-damping effect. In this study, the pressure pulsation characteristics were of investigated with respect to the aspect ratio of the cross section, wall thickness, and fuel rail material through oil hammer simulations. An oil hammer simulation was performed in advance to simulate the pressure pulsations at the resonant speed, which is a time-saving way. The pressure pulsation peak of fuel rail was observed to rise as the injection period increases. Increase of the aspect ratio and decrease of the wall thickness can reduce the pressure pulsation efficiently.

• 융합신호처리학회논문지
• /
• 제21권1호
• /
• pp.49-54
• /
• 2020

심혈관질환은 전 세계 주요 사망 원인으로 다양한 원인에 의해 발생한다. 심혈관질환의 가장 높은 위험인자는 고혈압으로 뚜렷한 증상이 없지만 방치할 경우 여러 합병증을 유발한다. 고혈압을 치료하기 위하여 약물치료와 규칙적 운동을 진행해야한다. 고혈압 환자의 경우 과도한 신체 활동 시 심장에 큰 무리가 발생해 심혈관질환으로 이어질 수 있다. 따라서 적정 강도로 운동을 진행할 수 있는 PTT 계측을 통한 운동 강도 모니터링 시스템이 요구된다. 본 연구에서는 심전도와 맥파 계측을 통해 PTT를 산출하여 운동 강도에 따른 PTT 변화 모니터링 시스템을 구현하였다. 구현된 시스템은 심전도의 R-peak와 맥파의 P-peak를 미분하여 peak간의 시간차를 이용하여 PTT를 산출한다. 운동 강도에 따른 PTT 변화 모니터링을 위하여 달리기 실험을 진행하였다. 실험결과 저강도는 0.313s, 중강도는 0.220s, 고강도는 0.188s의 PTT가 측정되었으며, 운동 강도가 증가함에 따라 PTT는 감소하는 것을 확인하였다.

• Wind and Structures
• /
• 제12권1호
• /
• pp.77-88
• /
• 2009

A pulsed impinging jet is used to simulate the gust front of a thunderstorm downburst. This work concentrates on investigating the peak transient loading conditions on a 30 mm cubic model submerged in the simulated downburst flow. The outflow induced pressures are recorded and compared to those from boundary layer and steady wall jet flow. Given that peak winds associated with downburst events are often located in the transient frontal region, the importance of using a non-stationary modelling technique for assessing peak downburst wind loads is highlighted with comparisons.

• 설비공학논문집
• /
• 제15권9호
• /
• pp.768-778
• /
• 2003

Numerical analysis has been carried out to investigate laminar convective heat transfer in a tube for supercritical water near the thermodynamic critical point. Fluid flow and heat transfer are strongly coupled due to large variations of thermodynamic and transport properties such as density, specific heat, viscosity, and thermal conductivity near the critical point. Heat transfer characteristics in the developing region of the tube show transition behavior between liquid-like and gas-like phases with a peak in heat transfer coefficient distribution near the pseudocritical point. The peak of the heat transfer coefficient depends on pressure and wall heat flux rather than inlet temperature and Reynolds number, Results of the modeling provide convective heat transfer characteristics including velocity vectors, temperature, and the properties as well as the heat transfer coefficient. The effect of proximity to the critical point is considered and a heat transfer correlation is suggested for the peak of Nusselt number in the tube.

• 한국정보전자통신기술학회논문지
• /
• 제7권1호
• /
• pp.50-54
• /
• 2014

본 연구에서는 혈압측정으로부터 얻어지는 오실레이션(Oscillation) 신호를 이용하여 심박주기를 검출하고, 심박주기의 정확성을 개선하는 알고리듬을 개발하였다. 이를 위한 혈압측정의 방법으로 오실로메트릭(Oscillometric) 측정법을 사용하였으며, 오실레이션 신호의 피크들로부터 전 후 기울기들의 평균이 교차하는 지점을 실제 피크로 인정하고 심박주기를 계산하였다. 제안된 방법은 그래프 상에서 심박주기의 극심한 편차와 오류를 줄이는 성능을 나타냈다.

• International Journal of Air-Conditioning and Refrigeration
• /
• 제13권4호
• /
• pp.206-216
• /
• 2005

Numerical analysis has been carried out to investigate laminar convective heat transfer at zero gravity in a tube for supercritical water near the thermodynamic critical point. Fluid flow and heat transfer are strongly coupled due to large variation of thermodynamic and transport properties such as density, specific heat, viscosity, and thermal conductivity near the critical point. Heat transfer characteristics in the developing region of the tube show transition behavior between liquid-like and gas-like phases with a peak in heat transfer coefficient distribution near the pseudo critical point. The peak of the heat transfer coefficient depends on pressure and wall heat flux rather than inlet temperature and Reynolds number. Results of the modeling provide convective heat transfer characteristics including velocity vectors, temperature, and the properties as well as the heat transfer coefficient. The effect of proximity on the critical point is considered and a heat transfer correlation is suggested for the peak of Nusselt number in the tube.

• 화약ㆍ발파
• /
• 제35권1호
• /
• pp.1-17
• /
• 2017

공기를 통해 이동하는 폭발파에 의한 압력 및 압력에 의해 지표 및 지하구조물에 미치는 영향을 이해하는 것은 매우 중요하다. 폭발의 충격이 구조물에 미치는 영향을 컴퓨터 시뮬레이션하기 위해서는 시간과 거리에 따른 압력의 변화를 결정하여야 한다. 기존의 연구를 통해 압력의 변화와 관련되는 인자들을 추정하기 위한 여러 경험식들이 개발되었다. 본 연구에서는 최대압력, 양압지속기간, 임펄스, 최소음압, 음압지속기간, 폭발파 도착시간과 감쇠상수를 예측하는 경험식들을 조사 분석하였으며 가장 널리 사용되고 있는 Kingery 경험식과 다른 경험식에 의한 압력 변화를 비교하였다.

• 한국분무공학회지
• /
• 제16권1호
• /
• pp.7-14
• /
• 2011

High pressure LPG fuel spray with a conventional swirl injector was visualized and the impact of the injection pressure was also investigated using a DISI (direct injection spark ignition) LPG single cylinder engine. Engine performance and emission characteristics were evaluated over three different injection pressure and engine loads at an engine speed of 1500 rpm. The fuel spray pattern appeared to notably have longer penetration length and narrower spray angle than those of gasoline due to its lower angular momentum and rapid vaporization. Fuel injection pressure did not affect combustion behaviors but for high injection pressure and low load condition ($P_{inj}$=120 bar and 2 bar IMEP), which was expected weak flow field configuration and low pressure inside the cylinder. In terms of nano particle formation the positions of peak values in particle size distributions were not also changed regardless of the injection pressure, and its number densities were dramatically reduced compared to those of gasoline.

• 한국연소학회지
• /
• 제16권3호
• /
• pp.33-40
• /
• 2011

Combustion experiments were conducted at three different fuels ($CH_4$, $C_2H_4$ and $C_3H_8$) to investigate the effects of combustor pressure (30 ~ -30 kPa) on combustion charateristics and reaction zone structure. Regardless of the fuels, emission index of CO (EICO) increased with decreasing combustor pressure, and EICO of $C_2H_4$ was mostly affected by changing combustor pressure at subatmospheric pressure. In order to observe reaction zone, $OH^*$, $CH^*$ and ${C_2}^*$ chemiluminescence intensity were measured. The sequence of the chemiluminescence intensity peak position was affected by chemical characteristics of fuels rather than changing combustor pressure. The emission zone thickness of $C_2H_4$ and $C_3H_8$, defined by the full width at half maximum (FWHM) of $CH^*$ intensity profile, were increased with decreasing combustor pressure. however, the thickness of $C_2H_4$ exhibited the opposite tendency due to the characteristics of the fuel as the bond structure.

• 대한조선학회논문집
• /
• 제44권3호
• /
• pp.279-284
• /
• 2007

As a container vessel becomes larger, the bow flare becomes larger. The large bow flare structures are often subjected to dynamic pressure loads due to bow flare slamming occurring in rough seas. The aim of this paper is to investigate the characteristics of bow flare slamming pressure measured in a real voyage through the North Pacific Ocean. The characteristics of impact pressure load caused by slamming is addressed in terms of the pressure pulse-time history which involves rising time, peak pressure, decaying time and type of pressure decay. The values were presented using non-dimensional parameters.