• Title/Summary/Keyword: Wave-type Flow

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Flow Analysis of POSRV Subsystem of Standard Korean Nuclear Reactor (한국 표준형 원전의 POSRV 하부 배관 유동해석)

  • Kwon, Soon-Bum;Kim, In-Goo;Ahn, Hyung-Joon;Lee, Dong-Eum;Baek, Seung-Cheol;Lee, Byeong-Eun
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.27 no.10
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    • pp.1464-1471
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    • 2003
  • In order to investigate the flows with shock wave in branch, 108$^{\circ}$ elbow and T-junction of the IRWST system of standard Korean nuclear reactor, detail time dependent behaviors of unsteady flow with shock wave, vortex and so on are obtained by numerical method using compressible three-dimensional Navier-Stokes equations. At first, the complex flow including the incident and reflected shock waves, vortex and expansion waves which are generated at the corner of T-junction is calculated by the commercial code of FLUENT6 and is compared with the experimental result to obtain the validation of numerical method. Then the flow fields in above mentioned units are analyzed by numerical method of [mite volume method. In numerical analysis, the distributions of flow properties with the moving of shock wave and the forces acting on the wall of each unit which can be used to calculate the size of supporting structure in future are calculated specially. It is found that the initial shock wave of normal type is re-established its type from an oblique one having the same strength of the initial shock wave at the 4 times hydraulic diameters of downstream from the branch point of each unit. Finally, it is turned out that the maximum force acting on the pipe wall becomes in order of the T-junction, 108$^{\circ}$ elbow and branch in magnitude, respectively.

A Parametric Study of the Wave-Generation Performance of a Piston-Type Wave Maker (피스톤 타입 조파기의 형상 매개변수에 대한 조파성능 연구)

  • Kwon, Do-Soo;Kim, Sung-Jae;Koo, Weoncheol
    • Journal of Ocean Engineering and Technology
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    • v.33 no.6
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    • pp.504-509
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    • 2019
  • The wave-generation performance of a piston-type wave maker was analyzed using the numerical wave tank technique, and the numerical results were compared with theoretical solutions. A two-dimensional frequency domain analysis was conducted based on the Rankine panel method. Various parameters were used to examine the wave-generation performance, such as the width and gap of the wave board. The effects of the thickness of the wave board and of the gap from the bottom of the tank were evaluated. The difference in the amplitude of the generated wave between the analytical solution and the numerical result was examined, and its causes were addressed due to the gap flow between the bottom of the tank and the wave board. This parametric analysis can be utilized to design an optimum wave make parametric analysis to design an optimum wave maker that can generate waves with amplitudes that can be predicted accurately.

A study of the spatial amplification of the Type II instability for the Rotating-disk flow (회전원판 유동의 제2형 불안정성 공간증폭에 관한 이론적 연구)

  • Lee, Yun-Yong;Lee, Kwang-Won;Hwang, Young-Kyu
    • Proceedings of the KSME Conference
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    • 2001.11b
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    • pp.481-486
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    • 2001
  • The hydrodynamic instability of the three-dimensional boundary layer on a rotating disk introduces a periodic modulation of the mean flow in the form of stationary cross flow vortices. Detailed numerical values of the growth rates, neutral curves and other characteristics have been calculated for the Type II-instabilities. Presented are the neutral stability results concerning the two instability modes by solving new linear stability equations reformulated not only by considering whole convective terms but by correcting some errors in the previous stability equations. The present stability results are agree with the previously known ones within reasonable limit. The spatial amplification contours have been calculated for the moving disturbance wave, whose azimuth angle is between $\varepsilon=-10^{\circ}$ and $-20^{\circ}$. The transition flow of the moving disturbance wave will be developed at $\varepsilon=-15^{\circ}$ and Re=352 corresponding at the growth rates n = 5.8 from the spatial amplification contours.

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Analysis of Hydroelastic Response of a Pontoon-type Structure Considering Effect of Wave Breaker with Underwater Opening (해수순환 방파제를 고려한 폰툰형 구조물의 유탄성응답 해석)

  • 홍사영;최윤락;홍석원
    • Journal of the Society of Naval Architects of Korea
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    • v.40 no.5
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    • pp.53-59
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    • 2003
  • Ocean space utilization using VLFS(Very Large Floating Structures) can provide environmental impact free space by allowing sea water flow freely through the floating structure. Use of Pontoon type VLFS for that purpose needs employment of breakwaters for reduction of wave effects. Therefore, in order to maximize advantage of environmental impact free structure, the breakwater should be the one that can allow water flow freely through it, too. In this paper hydroelastic response of a pontoon type structure is analyzed considering breakwaters which allow water flow through its opening at bottom of the breakwaters. Mode superposition technique is used for solving equation of flexible body while interactions between the pontoon and breakwaters is considered based on generalized mode concept. Bi-quadratic nine node higher-order boundary element method is adopted for more accurate numerical treatment near sharp edged body shape. Performance of various combinations of breakwaters is investigated.

Passive Control of the Condensation Shock Wave Oscillation in a Supersonic Nozzle (초음속 노즐에서 발생하는 응축충격파 진동의 피동제어)

  • Baek, Seung-Cheol;Kwon, Soon-Bum;Kim, Heuy-Dong
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.26 no.7
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    • pp.951-958
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    • 2002
  • Rapid expansion of a moist air or a stream through a supersonic nozzle often leads to non-equilibrium condensation shock wave, causing a considerable energy loss in flow field. Depending on amount of latent heat released due to non-equilibrium condensation, the flow is highly unstable or a periodical oscillation accompanying the condensation shock wave in the nozzle. The unsteadiness of the condensation shock wave is always associated with several kinds of instabilities as well as noise and vibration of flow devices. In the current study, a passive control technique using a porous wall with a plenum cavity underneath is applied for the purpose of alleviation of the condensation shock oscillations in a transonic nozzle. A droplet growth equation is coupled with two-dimensional Navier-Stokes equation system. Computations are carried out using a third-order MUSCL type TVD finite-difference scheme with a second-order fractional time step. An experiment using an indraft wind tunnel is made to validate the present computational results. The results show that the oscillations of the condensation shock wave are completely suppressed by the current passive control method.

A Study on Muffler′s Transmission Loss and Backpressure Property (소음기의 투과손실 및 배압특성에 관한 연구)

  • 정경훈;황원걸;이유엽;김기세
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2001.11b
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    • pp.676-681
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    • 2001
  • We usually divide the noise of exhaust system into pulsation noise and flow noise. Pulsation noise is the shock wave to occur when the burning gas of low pressure emits and include harmonic having basic frequency as the exhaust cycle of engine. Flow noise is the noise that is produced when gas flow emits into the atmosphere through the pipe and has the character of frequency like pink noise which has the high level of high frequency component. A muffler is divided into reflective type and absorptive type. We usually use the muffler compounding the property of them. In this study, it is the case of transfer matrix method that a muffler is compounded to analyze the elements of each section according to sound wave's proceed direction. But we use simple model. So, we use finite element method that takes short time to analyze. Acoustic analysis gives us transfer matrix to use FEA of SYSNOISE and we use STAR-CD for fluid analysis. We made database that is based on analytical results about the muffler of expansion type, extended type, offset type, reverse type, and perforated type and developed the muffler design system to perform work efficiently.

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Nonlinear Irregular Waves-current Interaction on Flow Fields with Wave Breaking around Permeable Submerged Breakwater (투과성잠제 주변에서 쇄파를 동반한 불규칙파-흐름장의 상호작용)

  • Lee, Kwang-Ho;Bae, Ju-Hyun;An, Sung-Wook;Kim, Do-Sam
    • Journal of Korean Society of Coastal and Ocean Engineers
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    • v.30 no.2
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    • pp.39-50
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    • 2018
  • In this study, the nonlinear interaction of irregular waves with wave breaking and currents around permeable submerged breakwater was investigated with the aid of olaFlow model which is open source CFD software published under the GPL license. The irregular wave performance of olaFlow applied in this study was verified by comparing and evaluating the target frequency spectrum and the generated frequency spectrum for applicability to irregular waves. Based on the applicability of this numerical model to irregular wave fields, in the coexistence fields of irregular waves and currents, the characteristics of wave height, frequency spectrum, breaking waves, averaged velocity and turbulent kinetic energy around porous submerged breakwater with the respect to the beach type and current direction versus wave propagation were carefully investigated. The numerical results revealed that the shape of wave breaking on the crown of the submerged breakwater and the formation of the mean flow velocity around the structure depend greatly on the current directions and the type of the beach. In addition, it was found that the wave height fluctuation due to the current direction with respect to the wave propagation is closely related to the turbulent kinetic energy.

Analysis of the Cold Gas Flow in Puffer Type Circuit Breaker (Puffer식 차단기 내의 냉가스 유동 해석)

  • Kim, Hong-Gyu;Sin, Seung-Rok;Jeong, Hyeon-Gyo;Kim, Du-Seong;Gwon, Gi-Yeong
    • The Transactions of the Korean Institute of Electrical Engineers B
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    • v.49 no.4
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    • pp.233-239
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    • 2000
  • There are many difficult problems in analyzing the gas flow in puffer type circuit breaker such as complex geometry, moving boundary, shock wave and so on. To predict the interruption performance accurately, these should be considered in the simulation. In this paper, the analysis procedure of the cold gas flow in the circuit breaker is presented. Euler equation is solved by FVFLIC method which is an explicit time difference scheme for an unsteady flow computation. Moving boundaries are treated with a cell elimination-addition technique. The pressure and density in front of piston are calculated from the rate of the cell volume change. The presented method is applied to the real circuit breaker model and the pressure in front of the piston is good agreement with the experimental one.

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Experimental Study on Flow Change at Downstream of Stepped Drop Structure (계단형 낙차공 하류 흐름변화에 대한 실험연구)

  • Yeo, Hong-Koo;Kang, Joon-Gu;Choi, Nam-Jeong;Kim, Sung-Jung
    • Proceedings of the Korea Water Resources Association Conference
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    • 2008.05a
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    • pp.1889-1893
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    • 2008
  • 본 연구에서는 완경사 계단형 낙차공에서 하류수심 변화에 따른 도수 형태의 변화와 WTF 흐름 특성에 대한 분석을 수행하였다. 일정한 유량에서 하류수위를 증가시키면 도수 형태가 달라지는데 특히 계단 끝단에서 완전도수, 잠김도수(B점프), downward curved jet, upward curved jet, wave type flow(WTF)가 차례로 나타났다. 잠김도수에서는 표면 롤러 현상이 관찰되었고 curved jet에서는 큰 유속 감세 없이 파가 하류까지 전달되었다. WTF에서는 사류흐름이 바닥 recirculation 구역의 영향으로 변형되면서 wave 형태의 도수를 발생시켰다. 하류수위를 점점 증가 시키면 도수의 발생 위치가 계단 위쪽으로 이동하며 잠김도수와 WTF가 번갈아가며 발생하였다. 하류수위가 높아질수록 도수의 규모는 작아졌으며 표면 롤러도 미약해지는 경향을 보였다. 세 가지 유량조건에 따른 WTF의 규모를 비교한 결과 유량이 증가할수록 WTF의 크기가 증가하였으며 무차원화한 WTF의 형상은 거의 비슷한 것으로 나타났다. 계단형 낙차공은 기존낙차공에서 발생하는 도수와 달리 WTF가 발생되므로 이에 대한 분석이 필요하다. WTF가 발생하는 구간의 수위는 하류수위보다 높아지기 때문에 하천 설계 시 하천 접합부의 조건(구수부지설치, 제방설치 등)에 따라 wave의 높이가 설계의 중요 인자로 고려되어야 할 것이다. WTF는 지금까지의 계단형 낙차공 설계 시 고려되지 못한 부분으로서 차후에 계단형 구조물 또는 계단식 변형 구조물 설계 시 주요 자료로 활용 될 것이다.

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Distributions of the velocity and pressure of the pulsatile laminar flow in a pipe with the various frequencies (주파수의 변화에 따른 원형관로내 층류맥동유동의 속도와 압력의 분포)

  • Bae, S.C.;Mo, Y.W.
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.9 no.4
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    • pp.561-571
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    • 1997
  • In this paper, the fundamental equations are developed for the pulsatile laminar flow generated by changing the oscillatory flow with $0{\leq}f{\leq}48Hz$ into a steady one with $0{\leq}Re{\leq}2500$ in a rigid circular pipe. Analytical solutions for the wave propagation factor k, the axial distributions of cross-sectional mean velocity $u_m$ and pressure p are schematically derived and confirmed experimentally. The axial distributions of centerline velocity and pressure were measured by using Pitot-static tubes and strain gauge type pressure transducers, respectively. The cross-sectional mean velocity was calculated from the centerline velocity by applying the parabolic distribution of the laminar flow and it was confirmed by using the ultrasonic flowmeter. It was found that the axial distributions of cross-sectional mean velocity and pressure agree well with theoretical ones and depend only on the Reynolds number Re and angular velocity $\omega$.

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