• Title/Summary/Keyword: 압력변동

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A Study on Turbulent Wall Pressure Fluctuations Using a Coherent Structure Model (응집구조 모델을 이용한 난류 벽면 압력변동에 대한 연구)

  • Ahn, Byoung-Kwon
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.17 no.5 s.122
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    • pp.405-414
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    • 2007
  • In recent years, experimental and theoretical studies show that turbulent flows looking disordered have a definite structure produced repetitively with visible order. As a core structure of turbulence, hairpin vertices are believed to play a major role in developing and sustaining the turbulence process in the near wall region of turbulent boundary layers and may be regarded as the simplest conceptual model that can account for the essential features of the wall pressure fluctuations. In this work, fully developed typical hairpin vortices are focused and the associated surface pressure distributions and their corresponding spectra are estimated. On the basis of the attached eddy model, the overall surface pressure spectra are represented in terms of the eddy size distribution. The model is validated by comparison of predicted wavenumber spectra with existing empirical models, the results of direct numerical simulation (DNS) and also spatial correlations with experimental measurements.

Effect of Reynolds Number, Leading Edge Roughness and Air Content on the Cavitation Performance of Model Propellers (Reynolds수, 표면거칠기 및 공기함유량이 모형프로펠러 캐비테이션 성능에 미치는 영향)

  • Ki-Sup Kim;Kyung-Yeul Kim;Jong-Woo Ahn;Jin-Tae Lee
    • Journal of the Society of Naval Architects of Korea
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    • v.37 no.1
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    • pp.10-25
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    • 2000
  • The effects of Reynolds number of model propeller leading edge roughness and air content resolved in tunnel water on cavitation inception, cavitation extent and pressure fluctuation were investigated experimentally by using two model propellers in a cavitation tunnel. Cavitation observation and propeller induced fluctuating pressure measured in the present model test were compared with the model test results of other research institutes and the full-scale data of a German container ship(Sydney Express). The comparison shows a reasonable agreement.

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Surface Elevation Recovery Methods from Pressure Gage for Irregular Waves (불규칙파(不規則波에) 대한 압력식(壓力式) 파고계(波高計)의 적용성(適用性)에 관한 연구(研究))

  • Kwon, Jung Gon;Kang, Ju Bok
    • KSCE Journal of Civil and Environmental Engineering Research
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    • v.12 no.4_1
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    • pp.129-136
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    • 1992
  • A precedure for recovering surface displacement from a time series of pressure measured by a pressure gage in a shallow water (that is, FFTM, LCM. IWM) is investigated with respect to a proper cut-off-frequency of a frequency response function for the accurate recovery of wave height and period. The authors examined the applicability of above mentioned three transformation procedures through field observations and laboratory experiments and the following results are obtained. i) The cut-off-frequency of the frequency response function used in FFTM is deeply depend on both the frequency response of the pressure sensor and the water depth at the sensor. In this study, a relatively accurate surface displacement can be recovered when the frequency response function is cut off at the frequency corresponding to kh=3.0 where k is a wave number at the depth of h. The frequency response function in the region higher than the cut-off-frequency is set constant to be the value at the cut-off-frequency. ii) The transformed surface displacements by LCM are affected by the small waves of short periods included in the measured pressure. It is found that pressure variation whose local frequency is higher than kh=1.5 has to be neglected to recover surface displacement sufficiently. iii) In IWM, the linear pressure response function is usually utilized by multiplying a coefficient N which is a function of the frequency (or kh) and takes a value around unity. However, in this study, a constant value of N(=1.0) gives a relatively accurate recovery of surface displacements.

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원전의 자동기동 운전을 위한 냉각재 만수상태에서의 압력제어기 개발

  • 박재창;오병주
    • Proceedings of the Korean Nuclear Society Conference
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    • 1996.05a
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    • pp.440-445
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    • 1996
  • 본 논문에서는 가압기에 기포가 형성되기전 원자로 냉각재계통의 압력을 자동으로 제어할 수 있는 원자로 냉각재 압력 제어기를 개발하여 원전 시뮬레이터를 통해 설계된 제어기의 성능시험을 수행하였다. 그 결과 냉각재의 압력변동을 주는 환경 요인 발생시에도 설정치에 안정된 압력제어 특성을 보여주었다. 원전 기동시 압력제어에 본 논문에서 제안한 제어기를 적용할 경우 운전원의 운전부하를 줄여줄 것으로 예측된다.

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Numerical Simulation of the Effect of Pressure Fluctuation on the Modulation of Equivalence Ratio at the Fuel Injection Hole (압력변동이 연료 분사구에서의 당량비 변동에 미치는 영향에 관한 수치 해석)

  • Kim, Hyeon-Jun;Hong, Jung-Goo;Shin, Hyun-Dong
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.31 no.3 s.258
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    • pp.292-299
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    • 2007
  • In gas turbine technology, the flame stability is inherently greater in conventional diffusion type combustion over a wider range fuel to oxidizer ratio. However, premixed type combustion which has narrow flame stability region, is widely used due to environmental reason. It has been observed in experiments that combustion instability of low frequency (${\sim}10Hz$) results from the modulation of equivalence ratio at fuel injection hole when a pressure fluctuation propagates upwards along the channel of the burner under an unchoked fuel flow condition. In this study, a commercial program was used to determine how the fuel flow rate changed with respect to the pressure, velocity of the fuel flow and the mass fraction in a choked and an unchoked condition. The calculation focuses on the upstream of the dump plane to know how the forced pressure with the fuel injection conditions affects the modulation of the equivalence ratio. Therefore, it is found that pressure fluctuation leads to oscillation of mass flow rate and then results in equivalence ratio modulation under the unchoked fuel flow condition.

Analysis of Normal Shock-Wave Oscillation in a Supersonic Diffuser (초음속 디퓨져에서 발생하는 수직충격파 진동의 이론해석)

  • 김희동
    • Journal of the Korean Society of Propulsion Engineers
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    • v.2 no.3
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    • pp.36-46
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    • 1998
  • Shock-wave in a supersonic diffuser flow cannot be stable even in the given pressure ratio which remains constant over time, and oscillates around a certain time-mean position. In the present study, oscillation of a normal shock-wave in a supersonic diffuser was analyzed by a small perturbation method. Upstream pressure perturbation was applied to a supersonic diffuser flow with a normal shock-wave. Stability of shock-wave was investigated by considering the diffuser pressure recovery and frequency of the pressure perturbation. The results obtained show that a stable oscillation of weak normal shock-wave is obtainable for the flow with the Mach number over 1.74. The ratio of sound pressures downstream to upstream of the shock wave increases with increase of the Mach number. The present results agree well with other analytical and experimental results.

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A Study on the Air Pressure Endurance Test Device for High Speed Train Windows (고속철도차량 객차창문의 공기압력내구성 시험장치 개발에 관한 연구)

  • Chang, Dae-Sung;Yi, Won
    • Journal of the Korean Society for Railway
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    • v.15 no.2
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    • pp.104-108
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    • 2012
  • All of the Korean high speed train windows have been imported from abroad up to now. In this paper, the air pressure endurance test device for high speed train windows was studied and developed. This test device can create air pressure variation similar to train running real condition and carry out pressure endurance test according to international standard. Henceforward, this test device will be useful for domestic production of high speed train windows.

Numerical Simulation on Equivalence Ratio Fluctuation at the Fuel Injection Hole with respect to Pressure Fluctuation in a Combustion Chamber (연소실내의 압력 변동에 따른 연료 분사구에서의 당량비 변동에 관한 수치해석)

  • Kim, Hyeon-Jun;Hong, Jung-Goo;Shin, Hyun-Dong
    • 한국연소학회:학술대회논문집
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    • 2006.10a
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    • pp.27-35
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    • 2006
  • It has been observed in experiments that combustion instability of low frequency (${\sim}$ 10Hz) results form the modulation of equivalence ratio at fuel injection hole when a pressure fluctuation propagates upwards along the channel of the burner under an unchoked fuel flow condition. In this study, a commercial program was used to determine how the fuel flow rate changed with respect to the pressure, velocity of the fuel flow and the mass fraction in a choked and an unchoked condition. The calculation focus on the upstream of the dump plane to know how the forced pressure with the fuel injection conditions affects the modulation of the equivalence ratio. Therefore, it is found that pressure fluctuation leads to oscillation of mass flow rate and then results in equivalence ratio modulation under the unchoked fuel flow condition.

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공공요금(公共料金)과 물가(物價)

  • Park, U-Gyu
    • KDI Journal of Economic Policy
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    • v.15 no.3
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    • pp.37-52
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    • 1993
  • 우리나라에서는 70년대 중반 여후 공공요금관리(公共料金管理)가 물가정책의 주요수단으로 인식되어 왔으나, 다른 나라의 경험을 살펴보면 물가상승압력(物價上昇壓力)의 근본적인 해소가 전제되지 않는 가격규제정책(價格規制政策)은 유효한 물가대책(物價對策)이 아니라는 것이 보편적으로 인정되고 있다. 본고(本稿)의 분석(分析)에 의하면, 공공요금(公共料金)의 변동과 기타물가지수(소비자물가지수에서 공공요금 및 농축수산물지수를 제외한 것)의 변동간에는 장기적으로 같이 움직이는 공적분관계(共積分關係)가 존재한다. 그러나 일반의 인식과는 달리 공공요금의 변동이 기지물가변동(其地物價變動)을 초래하는 것이 아니라, 기타물가상승(其他物價上昇)이 공공요금상승을 유발하였던 것으로 나타났다. 이는 과거의 공공요금관리정책(公共料金管理政策)이 물가대책으로서의 유효성은 높지 않았음을 의미한다. 따라서 향후의 물가안정(物價安定)은 공공요금 등에 대한 직접적인 가격억제(價格抑制)보다는 경제전체의 물가상승압력(物價上昇壓力)을 완화시킬 수 있는 안정위주의 거시정책기조(巨視政策基調)를 통하여 이뤄 나가야 할 것이다.

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가압경수로 가압기 안전밸브 보수후 압력설정치 시험

  • 신대수;류용호
    • Proceedings of the Korean Nuclear Society Conference
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    • 1998.05a
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    • pp.386-391
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    • 1998
  • 국내 가압경수로 가압기 안전밸브는 운영기술지침서에 따라 운전 중과 같은 환경조건에서 압력설정치(2,485 psig) 시험을 수행하도록 규정되어 있다. 가압기 안전 밸브는 일정한 주기로 압력설정치 시험이 수행되고 있으나, 시험시의 주변 온도, 사용 유체 등 그 시험 조건에 따라 압력설정 허용치 $\pm$1% 이상의 편차가 발생할 수 있음이 확인되고 있다. 본 연구에서는 압력설정치 시험시의 주변온도 상태에 따른 설정치 변동 사례를 조사하고, 보수 후 압력설정치 조정을 위한 대체 방안과 그 문제점을 고찰하였다.

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