• Title/Summary/Keyword: Pressure Loss Model

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A Study on Loss of Coolant Accident in Nuclear Power Plant Using DOE (실험계획법을 이용한 원자력 발전소에서의 냉각제 상실사고에 대한 연구)

  • Leem Young-Moon;Lee Sung-Mo
    • Journal of the Korea Safety Management & Science
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    • v.7 no.4
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    • pp.85-99
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    • 2005
  • The main objective of this paper is to search whether containment vessel's best pressure may increase until how long when loss of coolant accident (LOCA) happened in containment vessel of Ulchin nuclear power plant 1 and 2. Another goal of this research is to find the influential factors that increase containment vessel pressure. Model for this research is Ulchin nuclear power plant 1 with 10 cycles. Data were collected by simulator of Ulchin nuclear power plant 1 and design of experiment was used for data analysis. For the experiment, seven factors that are going to influence in containment vessel pressure were chosen. It was found that fatter which influences in early rise of containment vessel pressure after LOCA is only explosion size. Also, containment vessel's best pressure (3.74 bar.a) was much lower than limit (4.86 bar.a) of FSAR (Final Safety Analysis Report).

EVALUATION OF TURBULENCE MODELS IN A HIGH PRESSURE TURBINE CASCADE SIMULATION (고압터빈 익렬 주위 유동해석에서 난류모델의 영향 평가)

  • El-Gendi, M.M.;Lee, K.U.;Chung, W.J.;Joh, C.Y.;Son, C.H.
    • Journal of computational fluids engineering
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    • v.17 no.3
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    • pp.53-58
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    • 2012
  • Steady flow simulations through a high pressure turbine guide vanes were carried out. The main objective of the present work is to study the performance of turbulence models on the steady flow prediction from aerodynamic and aerothermal points of view. Three turbulence models were compared, namely SST, k-${\omega}$ and ${\omega}$-Reynolds stress models. The laminar results were also compared. The comparison was done with emphasis on the isentropic Mach number and heat transfer coefficient along the blade, and total pressure loss in the wake region. The calculated isentropic Mach number showed reasonable agreement with experimental data along the blade surface for all three turbulent models. For the total pressure loss in the wake region, ${\omega}$-Reynolds stress model showed the best agreement with the experimental data. However, unless using an appropriate transition model, the heat transfer coefficients of all three turbulent models showed poor agreement with experimental data.

Numerical Investigation on Frictional Pressure Loss in a Perfect Square Micro Channel with Roughness and Particles

  • Han Dong-Hyouck;Lee Kyu-Jung
    • Journal of Mechanical Science and Technology
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    • v.20 no.8
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    • pp.1266-1274
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    • 2006
  • A numerical study is performed to investigate the effect of inner surface roughness and micro-particles on adiabatic single phase frictional pressure drop in a perfect square micro channel. With the variation of particles sizes (0.1 to $1{\mu}m$) and occupied volume ratio (0.01 to 10%) by particles, the Eulerian multi-phase model is applied to a $100{\mu}m$ hydraulic diameter perfect square micro channel in laminar flow region. Frictional pressure loss is affected significantly by particle size than occupied volume ratio by particles. The particle properties like density and coefficient of restitution are investigated with various particle materials and the density of particle is found as an influential factor. Roughness effect on pressure drop in the micro channel is investigated with the consideration of roughness height, pitch, and distribution. Additionally, the combination effect by particles and surface roughness are simulated. The pressure loss in microchannel with 2.5% relative roughness surface can be increased more than 20% by the addition of $0.5{\mu}m$ diameter particles.

Modeling of Engine Intake Pressure for Predicting Braking Performance Affected by Altitude (고도에 따른 제동 성능 예측을 위한 엔진 흡기압 모델링)

  • An, Kwangman;Lee, Jisuk;Park, Jinil;Lee, Jonghwa
    • Transactions of the Korean Society of Automotive Engineers
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    • v.22 no.3
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    • pp.228-233
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    • 2014
  • Reduction of the atmospheric pressure in high altitude affects brake booster system which was operated by the difference between the intake pressure and the atmospheric pressure. So, braking system can not stably perform due to decrease of brake boost pressure. In this study, effects of altitude change on engine intake pressure was analyzed by prediction model of engine intake pressure which was studied previously. And engine intake pressure was simulated by simulation model in various driving conditions and environmental conditions.

A PRESSURE DROP MODEL FOR PWR GRIDS

  • Oh, Dong-Seok;In, Wang-Ki;Bang, Je-Geon;Jung, Youn-Ho;Chun, Tae-Hyun
    • Proceedings of the Korean Nuclear Society Conference
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    • 1998.05a
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    • pp.483-488
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    • 1998
  • A pressure drop model for the PWR grids with and without mixing device is proposed at single phase based on the fluid mechanistic approach. Total pressure loss is expressed in additive way for form and frictional losses. The general friction factor correlations and form drag coefficients available in the open literatures are used to the model. As the results, the model shows better predictions than the existing ones for the non-mixing grids, and reasonable agreements with the available experimental data for mixing grids. Therefore it is concluded that the proposed model for pressure drop can provide sufficiently good approximation for grid optimization and design calculation in advanced grid development.

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A Study on the Flow Characteristics and Pressure Loss of a Muffler for the Variation of Volumetric Rate and Offset (체적비와 오프셋 변화에 의한 소음기내의 유동특성과 압력손실에 관한 연구)

  • 김민호;정우인;천인범
    • Transactions of the Korean Society of Automotive Engineers
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    • v.8 no.4
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    • pp.93-99
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    • 2000
  • It is well known that an automotive muffle strongly influences engine efficiency and noise reduction. The performance of a muffler system is determined by the geometrical parameters such as the relative location of an inlet and outlet pipe size and cross sectional geometry of a chamber. In this study numerical analysis was performed to examine the flow characteristics in the simple automotive muffler for the variation of volumetric rate and offset. The computational grid generation was carried out. The RNG k-$\varepsilon$ turbulence model was applied. To provide the boundary condition for numerical analysis the experimental measurement wes carried out. As a result of this study we could understand that there was a recirculation flow inside muffler and pressure loss depends on the variation of volumetric rate and offset.

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Shallow Water Low-frequency Reverberation Model (천해 저주파 잔향음 예측모델)

  • 김남수;오선택;나정열
    • The Journal of the Acoustical Society of Korea
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    • v.21 no.8
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    • pp.679-685
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    • 2002
  • Low-frequency mono-static reverberation model for shallow-water environment is presented. It is necessary to develop the transmission loss model to calculate the sub-bottom interaction because the ray-based transmission loss model is difficult to compute the pressure accurately which penetrates the bottom medium. In this paper reverberation level is calculated using the RAM (Range dependent Acoustic Model) to augment the multi-path expansion model because it does not estimate transmission loss accurately in shallow water. The signals generated by the L-HYREV and the GSM are compared with the observed signals and it is showed that the L-HYREV model provides a closer fit to the observed signals than those obtained using the GSM.

Pressure Characteristics According to the Duct Shapes of Turbo Blowers Connected in Serial (다단 블로어 덕트형상에 따른 압력특성 연구)

  • Park, Young-Bin;Jang, Choon-Man;Yang, Sang-Ho
    • The KSFM Journal of Fluid Machinery
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    • v.13 no.2
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    • pp.30-35
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    • 2010
  • Pressure characteristics according to the duct shapes of turbo blowers connected in serial have been performed to reduce pressure loss in the piping system. To analyze three-dimensional flow field in the turbo blower system, general analysis code, CFX, is introduced in the present work. SST turbulence model is applied to estimate the eddy viscosity. Throughout the numerical simulation for the turbo blower system having a various shape of a inlet guide, optimal inlet guide can be selected. It is found that the pressure loss in the piping system having the optimal inlet guide can be reduced by minimizing the inflow distortion at the upstream of the impeller. Detailed flow analysis of the blower system serially connected is also performed and analyzed.

Physical model test of Jintan underground gas storage cavern group

  • Chen, Yulong;Wei, Jiong
    • Geomechanics and Engineering
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    • v.30 no.1
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    • pp.45-49
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    • 2022
  • In the present study, a physical model was built for the Jintan underground gas storage cavern group according to the similarity theory. In this regard, four ellipsoid caverns were built with scaled in-situ stresses and internal pressure. Then the stability of underground caverns was analyzed. The obtained results demonstrate that loss of internal pressure adversely affects the safety of caverns and attention should be paid during the operation of gas storage.