• 제목/요약/키워드: quasi-steady

검색결과 322건 처리시간 0.037초

PAD 모델링을 통한 분리메카니즘 시뮬레이션 기법 (Simulation of Separation Mechanism by Modeling a Propellant Actuated Device)

  • 오석진;이도형
    • 한국추진공학회지
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    • 제14권6호
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    • pp.45-52
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    • 2010
  • 본 논문에는 분리장치 종류 중 하나인 가스푸셔와 가스발생기의 수학적-물리적 모델이 기술되어있다. 준정상상태 모델이 가스푸셔와 가스발생기로 구성된 PAD의 성능해석을 위해 도입되었다. 실험적 상수인 열손실계수와 마찰계수는 시험에 의해 결정되었다. 그레인 형상설계에 기초한 가스발생기와 가스푸셔 내부의 연소과정, 유동과 피스톤 거동이 수치해석적 방법으로 시뮬레이션 되었다. 개발된 예측기법은 향후 유사한 분리메카니즘 시스템 설계시에 유용하게 사용될 수 있을 것이다.

단일 알루미늄 연료 입자의 점화 및 연소 모델링 (Modeling of the Ignition and Combustion of Single Aluminum Particle)

  • 양희성;임지환;김경무;이지형;윤웅섭
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2008년도 제30회 춘계학술대회논문집
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    • pp.187-192
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    • 2008
  • A simplified model for an isolated aluminum particle burning in air is presented. Burning process consists of two stages, ignition and quasi-steady combustion (QSC). In ignition stage, aluminum which is inside of oxide film melts owing to the self heating called heterogeneous surface reaction (HSR) as well as the convective and radiative heat transfer from ambient air until the particle temperature reaches melting point of oxide film. In combustion stage, gas phase reaction occurs, and quasi-steady diffusion flame is assumed. For simplicity, 1-dimesional spherical symmetric condition and flame sheet assumption are also used. Extended conserved scalar formulations and modified Shvab-Zeldovich functions are used that account for the deposition of metal oxide on the surface of the molten aluminum. Using developed model, time variation of particle temperature, masses of molten aluminum and deposited oxide are predicted. Burning rate, flame radius and temperature are also calculated, and compared with some experimental data.

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액체로켓용 터보펌프 성능예측에 대한 수치해석적 연구 (Numerical Studies on the Performance Prediction of a Turbopump System for Liquid Rocket Engines)

  • 최창호;이기수;김진한;양수석;이대성
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2001년도 유체기계 연구개발 발표회 논문집
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    • pp.264-270
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    • 2001
  • The hydraulic performance analysis of an entire pump system composed of an inducer, impeller, volute and seal for the application on turbopumps is performed using three-dimensional Wavier-Stokes equations. A quasi-steady mixing-plane method is used on the impeller/volute interface to simulate the unsteady interaction phenomena. From this wort the effects of each component on the pump performance are investigated at design and off-design conditions through the analysis of flow structures and loss mechanisms. The computational results are in a good agreement with experimental ones in terms of the headrise and efficiency even though very complex flow structures are present. It is found that the asymmetric pressure distribution along the volute wall constitutes the main reason of the difference between experimental and computational results due to the limitation of the applying the quasi-steady method. Since the volute was found to be over-designed according to the pressure distribution of the volute wall, redesign of the volute has been performed resulting in an improved performance characteristic.

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이원추진제 추진시스템의 배관망에 대한 비정상 마찰을 고려한 과도기유체 해석 (A FLUID TRANSIENT ANALYSIS ON THE PIPE NETWORK OF BIPROPELLANT PROPULSION SYSTEM WITH AN UNSTEADY FRICTION)

  • 채종원;한조영;김정훈;전형열
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2010년 춘계학술대회논문집
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    • pp.487-490
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    • 2010
  • A fluid transient analysis on the pipe network of bipropellant propulsion system is conducted through numerical parametric studies in which unsteady friction results are compared with quasi-steady friction results and also show the pressure drop results during the liquid apogee engine firing. The fluid transient analysis program has verified through comparing with the original Zielke model, the full and recursive convolution model and quasi-steady model as a reference. And the pressure drop program also has verified through comparing with results of the well-known program, EPANET2. The bipropellant propulsion system has two different fluids as fuel and oxidizer, and mostly they are hypergolic combination so that the valve opening and closing of the thrusters, that cause the pressure waves, shall take place simultaneously to get proper performance. The different physical properties of the fuel and oxidizer result in the different responsive to the same valve opening and closing. The response results may be helpful to know the characteristics of the bipropellant propulsion system and design it.

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Improvement and validation of a flow model for conical vortices

  • Ye, Jihong;Dong, Xin
    • Wind and Structures
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    • 제19권2호
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    • pp.113-144
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    • 2014
  • Separation bubble and conical vortices on a large-span flat roof were observed in this study through the use of flow visualization. The results indicated that separation bubble occurred when the flow was normal to the leading edge of the flat roof. Conical vortices that occur under the cornering flow were observed near the leading edge, and their appearance was influenced by the wind angle. When the wind changed from along the diagonal to deviating from the diagonal of the roof, the conical vortex close to the approaching flow changed from circular to be more oblong shaped. Based on the measured velocities in the conical vortices by flow visualization, a proposed two-dimensional vortex model was improved and validated by simplifying the velocity profile between the vortex and the potential flow region. Through measured velocities and parameters of vortices, the intensities of conical vortices and separation bubble on a large-span flat roof under different wind directions were provided. The quasi-steady theory was corrected by including the effect of vortices. With this improved two-dimensional vortex model and the corrected quasi-steady theory, the mean and peak suction beneath the cores of the conical vortices and separation bubble can be predicted, and these were verified by measured pressures on a larger-scale model of the flat roof.

Transient Groundwater Flow Modeling in Coastal Aquifer

  • 이은희;현윤정;이강근;박병원
    • 한국지하수토양환경학회:학술대회논문집
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    • 한국지하수토양환경학회 2006년도 총회 및 춘계학술발표회
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    • pp.293-297
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    • 2006
  • Submarine groundwater discharge (SGD) and the interface between seawater and freshwater in an unconfined coastal aquifer was evaluated by numerical modeling. A two-dimensional vertical cross section of the aquifer was constructed. Coupled flow and salinity transport modeling were peformed by using a numerical code FEFLOW In this study, we investigated the changes in groundwater flow and salinity transport in coastal aquifer with hydraulic condition such as the magnitude of recharge flux, hydraulic conductivity. Especially, transient simulation considering tidal effect and seasonal change of recharge rate was simulated to compare the difference between quasi-steady state and transient state. Results show that SGD flux is in proportion to the recharge rate and hydraulic conductivity, and the interface between the seawater and the freshwater shows somewhat retreat toward the seaside as recharge flux increases. Considered tidal effect, SGD flux and flow directions are affected by continuous change of the sea level and the interface shows more dispersed pattern affected by velocity variation. The cases which represent variable daily recharge rate instead of annual average value also shows remarkably different result from the quasi-steady case, implying the importance of transient state simulation.

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설마천 유역의 토양수분 장기 모니터링을 통한 토양수분 시공간 변화양상의 특성화 (Characterizing the Spatial-temporal Distribution of Soil Moisture for Sulmachun Watershed Through a Continuous Monitoring)

  • 이가영;김기훈;김상현
    • 한국수자원학회:학술대회논문집
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    • 한국수자원학회 2004년도 학술발표회
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    • pp.209-214
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    • 2004
  • 국내산지사면에서의 토양수분의 시공간적 분포를 파악하기 위하여 TDR(Time Domain Reflectometry)을 이용한 토양수분 장기 모니터링을 실시하였다. 대상사면을 측량하여 DEM(Digital Elevation Model)을 구축하고 흐름분배알고리즘에 적용하여 측정지점을 선정, 역 측량하여 효율적인 측정 체계를 구축하였다. DEM을 통하여 대상산지사면의 지형을 파악, 활용하여 정적 습윤지수(steady-state wetness index), 반동력학적 습윤지수(quasi-dynamic wetness index)를 구하였다. 장기 모니터링을 통한 토양수분 자료를 시공간적으로 분석하고 각각의 습윤 지수의 특징을 분석하고 습윤 지수와 토양수분 실측치와의 유의성과 제한점을 비교 분석하였다.

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액체로켓용 터보펌프 성능예측에 대한 수치해석적 연구 (Numerical Studies on the Performance Prediction of a Turbopump System for Liquid Rocket Engines)

  • 최창호;이기수;김진한;양수석;이대성
    • 한국유체기계학회 논문집
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    • 제5권2호
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    • pp.15-21
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    • 2002
  • The hydraulic performance analysis of an entire pump system composed of inducer, impeller, volute and seal for the application of turbopumps is numerically performed using three-dimensional Navier-Stokes equations. A quasi-steady mixing-plane method is used on the impeller/volute interface to simulate the unsteady interaction phenomena. From this work, the effects of each component on the pump performance are investigated at design and off-design conditions through the analysis of flow structures and loss mechanisms. The computational results are in a good agreement with experimental ones in terms of the headrise and efficiency even though very complex flow structures are present. It is found that the asymmetric pressure distribution along the volute wall constitutes the main reason of the difference between experimental and computational results, due to the limitation of the quasi-steady method. Since the volute was found to be over-designed by the pressure distribution of the volute wall, re-design of the volute has been performed, resulting in an improved performance characteristic.

알루미늄 입자 연소 지배인자의 민감도 해석 (Parametric Studies on the Sensitivity of Single Isolated Aluminum Particle Combustion Modeling)

  • 이상협;고태호;양희성;윤웅섭
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2010년도 제35회 추계학술대회논문집
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    • pp.321-327
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    • 2010
  • 마이크로 크기의 단일 알루미늄 해석을 위한 간단한 모델을 작성하고, 현상의 주요 파라메터를 도출하는 연구를 수행하였다. 금속 입자의 연소는 점화와 준정상상태의 연소 단계로 구성하였고, 각 단계는 액적 연소의 경우와 유사하게 보존 및 이송 방정식들을 사용하여 모사되었다. 모델은 기존의 실험 데이터와의 엄격한 비교를 통해 신뢰성을 검증하였고, 이 과정에서 현상의 주요 변수를 도출하여 그 영향을 평가하였다. 주요 변수로는 초기 입자크기, 산화 피막 두께, 대류 열전달의 유무, 외기온도, 압력 등이 선정되었고, 간단한 열역학적 모델임에도 불구하고 정량적으로 실험 데이터와 유사하게 각각의 파라메터의 영향을 평가할 수 있음을 확인하였다.

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비정상 유동의 메탄/공기 혼합기 반응안정성 효과 연구 (Combustion Stability and the Properties of Methane/Air Mixture Subjected to Unsteady Flow Fluctuations)

  • 이의주;오창보
    • 한국안전학회지
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    • 제26권5호
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    • pp.1-6
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    • 2011
  • Flame extinction and the chemistry of stoichiometric methane/air mixture were investigated numerically in the PSR(perfectly stirred reactor). For the study, PSR code was modified to be possible to unsteady calculation, and the sinusoidal fluctuation was subjected to the residence time. In the region of residence time far from the extinction limit, combustion mode was strongly dependent on the frequency. The low frequency excitation provided the quasi-steady behavior on the temperature and the concentrations of related species, but small variation of temperature was observed under high frequency. In the region of residence time near the extinction limit, the mixture subjected above 1 KHz was still reacting even though extinction had to be occurred under quasi-steady concept. The attenuation of extinction limit resulted from that chemical time was comparable to the flow time. The mean mole fractions of both NO and CO were almost same regardless of imposed frequency. However, the average mole fraction of $C_2H_2$ was decreased as increasing frequency, which implies that soot yield might be reduced at the higher frequency of flow excitation. The result provides the basic concept for flame stabilization, and it will be used to design a mild combustor.