• Title/Summary/Keyword: Gas Dynamics

Search Result 784, Processing Time 0.024 seconds

Efficiency Prediction of the Particle Removal Efficiency of Multi Inner Stage(MIS) Cyclone by Computational Fluid Dynamics(CFD) Analysis and Experimental Verification (CFD 해석을 이용한 Multi Inner Stage Cyclone 내부의 미세입자제거 효율 예측 및 실험적 검증)

  • Kim, Hye-Min;Kwon, Sung-An;Lee, Sang-Jun
    • Proceedings of the Korean Society of Computer Information Conference
    • /
    • 2012.07a
    • /
    • pp.243-246
    • /
    • 2012
  • A new multi inner stage(MIS) cyclone was designed to remove the acidic gas and minute particles of harmful materials produced from electronic industry. To characterize gas flow in MIS cyclone, pressure and velocity distribution were calculated by means of computational fluid dynamics(CFD) commercial program. Also, the flow locus of particles and particle removal efficiency were analyzed by Lagrangian method. When outlet pressure condition was -1,000 Pa, the efficiency was the best in this study. Based on the CFD simulation result, the pressure loss and destruction removal efficiency was measured through MIS cyclone experiment.

  • PDF

Critical Speed Analysis of a Small Gas Turbine Rotor (소형 가스터빈 회전체의 위험속도 해석)

  • Kim, Young-Cheol;Ha, Jin-Woong;Myung, Ji-Ho
    • The KSFM Journal of Fluid Machinery
    • /
    • v.12 no.3
    • /
    • pp.26-30
    • /
    • 2009
  • This paper predicts the critical speeds of a 5MW industrial gas turbine by using commercial rotordynamic tool, DYNAMICS 4.3. The gas turbine is operated at 12,975 rpm on squeeze film dampers. The stiffness of the squeeze film dampers are estimated. The critical speeds of the gas turbine rotor are calculated to have a sufficient separation margin (2%) from the 1st bending mode and pass over 2 rigid body modes below 4,000 cpm. This paper discussed the coupling effects on the dynamic response of the gas turbine.

Design Study on the Flow Characteristics of a Gas Management System for a Vertical Launching System (함정 수직발사대 화염처리장치 형상에 따른 유동특성 연구)

  • Yang, Young-Rok
    • Journal of the Korea Institute of Military Science and Technology
    • /
    • v.16 no.5
    • /
    • pp.712-717
    • /
    • 2013
  • The gas management system for a vertical launching system must be safely managed within a ship. The plenum and uptake are capable of containing and surviving a full-burning restrained firing without loss of gas management integrity. To secure the safety, the pressure characteristics with a supersonic under-expanded jet on a gas management system are numerically investigated using computational fluid dynamics. The results of present analysis and the preliminary design of the gas management system are described in this paper.

Gas pulsation analysis of large reciprocating compressor in parallel operation (병렬 운전되는 대형 왕복동 압축기의 가스맥동 분석)

  • Kim, Seong-Jun;Kim, Hyun-Cheol;Kim, Hyun-Jin
    • Proceedings of the SAREK Conference
    • /
    • 2009.06a
    • /
    • pp.910-915
    • /
    • 2009
  • For large reciprocating compressors in parallel operation, an analytical study has been carried out on the gas pulsation in associated discharge piping lines. Since the pressure pulsation at a valve, valve dynamics, and the gas flow rate through the valve are interrelated, affecting one another, these need to be solved simultaneously. Acoustic transfer matrix method, which relates acoustic pressure and velocity at one location to those at another location, has been adopted to calculate the effect of the gas flow at one valve location on the gas pulsation at other valve locations.

  • PDF

Gas Pulsation Analysis of Large Reciprocating Compressors in Parallel Operation (병렬 운전되는 대형 왕복동 압축기의 가스맥동 분석)

  • Kim, Seong-Jun;Kim, Hyun-Jae;Kim, Hyun-Jin
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
    • /
    • v.22 no.2
    • /
    • pp.97-103
    • /
    • 2010
  • For large reciprocating compressors in parallel operation, an analytical study has been carried out on the gas pulsation in associated discharge piping lines. Since the pressure pulsation at a valve, valve dynamics, and the gas flow rate through the valve are interrelated, affecting one another, these need to be solved simultaneously. Acoustic transfer matrix method, which relates acoustic pressure and velocity at one location to those at another location, has been adopted to calculate the effect of the gas flow at one valve location on the gas pulsation at other valve locations.

A Study on Ventilation Characteristics of Industrial Windows (공장창호의 환기특성에 관한 연구)

  • Piao, Cheng-Xu;Kim, Tae-Hyeung;Ha, Hyun-Chul;Xu, Rong-Bin
    • Journal of Environmental Science International
    • /
    • v.20 no.5
    • /
    • pp.581-587
    • /
    • 2011
  • Industrial natural ventilation systems consist of gravity ventilator, the high/low windows and doors. Especially, the high windows play an important role in the industrial natural ventilation systems. Generally speaking, industrial high windows are divided into 3 types; louver type, $45^{\circ}$ open type and $90^{\circ}$ open type. This study was numerically and experimentally conducted. Three types of windows were tested to know the ventilation characteristics and estimate the ventilation efficiencies. Numerically, computational fluid dynamics software (AIR PAK Ver. 2.0) was used to observe the flow characteristics inside the industrial building and the concentration contours generated by the tracer gas method. Experimentally, the flow visualization technique and the tracer gas method were applied with the model building to characterize the flow pattern inside the model building and to estimate the ventilation efficiencies with the different windows. It was found that $90^{\circ}$ open type window was most effective for the discharge of pollutants from the industrial building. On the other hand, the louver type window was found to be less effective than any other windows.

A Numerical Study on Temperature Prediction Bias using FDS in Simulated Thermal Environments of Fire (모사된 화재의 열적환경에서 FDS를 이용한 온도 예측오차에 관한 수치해석 연구)

  • Han, Ho-Sik;Kim, Bong-Jun;Hwang, Cheol-Hong
    • Journal of the Korean Society of Safety
    • /
    • v.32 no.2
    • /
    • pp.14-20
    • /
    • 2017
  • A numerical study was conducted to identify the predictive performance for the bare-bead thermocouple (TC) using FDS (Fire Dynamics Simulator) in simulated thermal environments of fire. A relative prediction bias of TC temperature calculated from reverse-radiation correction by FDS was evaluated with the comparison of previous experimental data. As a result, it was identified that the TC temperatures predicted by FDS were lower than the temperatures measured by bare-bead TC for the ranges of heat flux and gas temperature considered. The relative prediction bias of TC temperature by FDS was gradually increased with the increase in radiative heat flux and also significantly increased with the decrease in the gas temperature. Quantitatively, at the gas temperature of $20^{\circ}C$, the TC temperature predicted by FDS had the relative bias of approximately -20% with the radiative heat flux of $20kW/m^2$ corresponding to thermal radiation level of the flashover. It is predicted from the present study that more accurate validation of fire modeling will be possible with the quantitative prediction bias occurred in the process of reverse-radiation correction of temperature predicted by FDS.

Evaluation of Turbulent Models on the Swirling Flow of a Gun-Type Gas Burner According to the Mesh Size (격자크기에 따른 Gun식 가스버너의 스월유동에 대한 난류모델평가)

  • Kim, Jang-Kweon;Oh, Seok-Hyung
    • Journal of Power System Engineering
    • /
    • v.18 no.3
    • /
    • pp.59-65
    • /
    • 2014
  • The computational fluid dynamics was carried out to evaluate turbulent models on the swirling flow of a gun-type gas burner(GTGB) according to the mesh size. The commercial SC/Tetra software was used for a steady-state, incompressible and three-dimensional numerical analysis. In consequence, the velocity magnitude from the exit of a GTGB and the flowrate predicted by the turbulent models of MP k-${\varepsilon}$, Realizable k-${\varepsilon}$ and RNG k-${\varepsilon}$ agree with the results measured by an experiment very well. Moreover, the turbulent kinetic energy predicted by the turbulent model of standard k-${\varepsilon}$ with mesh type C only agrees with the experimental result very well along the radial distance. On the other hand, the detailed prediction of the information of swirling flow field near the exit of a GTGB at least needs a CFD analysis using a fairly large-sized mesh such as a mesh type C.

Modelling cavitating flow around underwater missiles

  • Petitpas, Fabien;Saurel, Richard;Ahn, Byoung-Kwon;Ko, Sung-Ho
    • International Journal of Naval Architecture and Ocean Engineering
    • /
    • v.3 no.4
    • /
    • pp.263-273
    • /
    • 2011
  • The diffuse interface model of Saurel et al. (2008) is used for the computation of compressible cavitating flows around underwater missiles. Such systems use gas injection and natural cavitation to reduce drag effects. Consequently material interfaces appear separating liquid and gas. These interfaces may have a really complex dynamics such that only a few formulations are able to predict their evolution. Contrarily to front tracking or interface reconstruction method the interfaces are computed as diffused numerical zones, that are captured in a routinely manner, as is done usually with gas dynamics solvers for shocks and contact discontinuity. With the present approach, a single set of partial differential equations is solved everywhere, with a single numerical scheme. This leads to very efficient solvers. The algorithm derived in Saurel et al. (2009) is used to compute cavitation pockets around solid bodies. It is first validated against experiments done in cavitation tunnel at CNU. Then it is used to compute flows around high speed underwater systems (Shkval-like missile). Performance data are then computed showing method ability to predict forces acting on the system.

Reactions of Gas-Phase Atomic Hydrogen with Chemisorbed Hydrogen on a Graphite Surface

  • Ree, Jong-Baik;Kim, Yoo-Hang;Shin, Hyung-Kyu
    • Bulletin of the Korean Chemical Society
    • /
    • v.28 no.4
    • /
    • pp.635-646
    • /
    • 2007
  • The reaction of gas-phase hydrogen atoms H with H atoms chemisorbed on a graphite surface has been studied by the classical dynamics. The graphite surface is composed of the surface and 10 inner layers at various gas and surface temperatures (Tg, Ts). Three chains in the surface layer and 13 chains through the inner layers are considered to surround the adatom site. Four reaction pathways are found: H2 formation, H-H exchange, H desorption, and H adsorption. At (1500 K, 300 K), the probabilities of H2 formation and H desorption are 0.28 and 0.24, respectively, whereas those of the other two pathways are in the order of 10-2. Half the reaction energy deposits in the vibrational motion of H2, thus leading to a highly excited state. The majority of the H2 formation results from the chemisorption-type H(g)-surface interaction. Vibrational excitation is found to be strong for H2 formed on a cold surface (~10 K), exhibiting a pronounced vibrational population inversion. Over the temperature range (10-100 K, 10 K), the probabilities of H2 formation and H-H exchange vary from 0 to ~0.1, but the other two probabilities are in the order of 10-3.