• Title/Summary/Keyword: Cavitation Phenomenon

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KRISO 대형 캐비테이션터널 시험조건의 함정 모형선 반류에 대한 수치해석적 연구 (Numerical Analysis of the Wake of a Surface Ship Model Mounted in KRISO Large Cavitation Tunnel)

  • 박일룡;김제인;김기섭;안종우;박영하;김명수
    • 대한조선학회논문집
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    • 제53권6호
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    • pp.494-502
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    • 2016
  • The accurate assessment of hull-appendage interaction in the early design stage is important to control the inflow to the propeller plane, which can cause undesirable hydrodynamic effects in terms of cavitation phenomenon. This paper describes a numerical analysis for the flow around a fully appended surface ship model for which KRISO has carried out a model test in the Large Cavitation Tunnel(LCT). This numerical study was performed with the LCT model test in a complementary manner for a good reproduction of the wake distribution of surface ships. A second order accurate finite volume method provided by a commercial computational fluid dynamics(CFD) program was used to solve the governing Reynolds Averaged Navier-Stokes(RANS) equations, where the SST $k-{\omega}$ model was used for turbulence closure. The numerical results were compared to available LCT experimental data for validation. The calculations gave good predictions for the boundary layer profiles on the walls of the empty cavitation tunnel and the wake at the propeller plane of the fully appended hull model in the LCT.

공구자세의 연속제어를 통한 선박용 프로펠러의 5축 가공 표면조도의 개선 (The Improvement of Surface Roughness of Marine Propeller by Continuous Control of Cutter Posture in 5-Axis Machining)

  • 손황진;임은성;정윤교
    • 한국기계가공학회지
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    • 제11권2호
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    • pp.27-33
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    • 2012
  • A marine propeller is designed for preventing cavitation priority. Cavitation is a phenomenon which is defined as the vibration or noise by dropping the pressure on the high-speed rotation of the propeller. There has to be a enough thrust on the low-speed rotation for preventing cavitation. Thus, it has to be considered in the increasing of the number of blade and the angle of wing to design the propeller. In addition, flow resistance will be increasing by narrowing the width between blades. So high quality surface roughness of the hub to minimize flow resistance is required. Interference problems with tool and neighboring surfaces often take place from this kind of characteristics of the propeller. During 5-Axis machining of these propellers, the excessive local interference avoidance, necessary to avoid interference, leads to inconsistency of cutter posture, low quality of machined surface. Therefore, in order to increase the surface quality, it is necessary to minimize the cutter posture changes and create a continuous tool path while avoiding interference. This study, by using a MC-space algorithm for interference avoidance and a MB-spline algorithm for continuous control, is intended to create a 5-Axis machining tool path with excellent surface quality. Also, an effectiveness is confirmed through a verification manufacturing.

수중 프로펠러 명음 현상의 규명에 관한 연구 (A study on the identification of underwater propeller singing phenomenon)

  • 김태형;이형석
    • 한국음향학회지
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    • 제37권2호
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    • pp.92-98
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    • 2018
  • 본 논문은 모형 프로펠러를 대상으로 공동수조 시험, 수중 충격시험, 유한요소해석 및 전산유체해석에 기반하여 수행한 명음 발생 메커니즘 연구이다. 선미 유동을 모사하기 위해 반류망, 프로펠러 및 방향타를 설치하고 수중청음기와 가속도계로 프로펠러 명음 현상의 발생과 소멸을 계측하였다. 유한요소해석을 통해 프로펠러 날개의 고유진동수를 예측하고 접촉 및 비접촉식 충격시험으로 이를 검증하였다. RANS(Reynolds Averaged Navier-Stokes) 방정식 기반 전산유체해석을 통하여 프로펠러 날개 각 단면의 유속과 유효 받음각을 계산하였으며, DES(Detached Eddy Simulation) 기반 고해상도 해석을 통해 명음 발생 위치에서 2-D 날개 단면 뒷전의 와류흘림주파수(vortex shedding frequency) 계산을 수행하였다. 수치적으로 예측된 와류흘림주파수는 모형시험으로 계측한 명음 발생 주파수 및 날개 고유진동수와 일치함을 확인하였다.

인젝터 노즐 형상이 노즐 내부 유동 및 출구 특성에 미치는 영향 (Influences of Injector Nozzle Shape on Nozzle Internal Flow and Outlet Characteristics)

  • 김창현;이강수;박재인;백제현
    • 한국자동차공학회논문집
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    • 제21권6호
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    • pp.108-116
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    • 2013
  • Diesel engine injector is used for spraying the fuel into the cylinder chamber. Complex phenomenon like cavitation occurs from small scale domain, highly pressurized condition and rapid injection. Flow inside the nozzle affects the whole engine performance including combustion and exhaust, therefore understanding the flow inside the injector nozzle is very important. In this paper, cylindrical and convergent-divergent nozzles are suggested for nozzle types and their influences on nozzle internal flow and nozzle outlet characteristics will be analyzed by changing their outlet diameters.

An Outlook on the Draft-Tube-Surge Study

  • Nishi, Michihiro;Liu, Shuhong
    • International Journal of Fluid Machinery and Systems
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    • 제6권1호
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    • pp.33-48
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    • 2013
  • If large pressure fluctuation is observed in the draft tube of a Francis turbine at part-load operation, we have generally called it draft-tube-surge. As occurrence of this phenomenon seriously affects the limit of turbine operating range, extensive studies on the surge have been made since proposal of surge-frequency criterion given by Rheingans. According to the literature survey of related topics in recent IAHR symposiums on hydraulic machinery and systems, in which state-of-the-art contributions were mainly presented, a certain review of them may be desirable for an outlook on the future studies in this research field. Thus, in this review paper, the authors' previous attempts for the last three decades to challenge the following topics: a rational method for component test of a draft tube, nature of spiral vortex rope and its behavior in a draft tube and cavitation characteristics of pressure fluctuations, are introduced together with other related contributions, expecting that more useful and significant studies will be accomplished in the future.

엔진 윤활용 제로터 오일펌프 유동해석 (Numerical Simulation in the IC Engine Lubricating Gerotor Oil Pump)

  • 조석현;박재인;남경우
    • 대한기계학회논문집B
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    • 제30권10호
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    • pp.1019-1025
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    • 2006
  • Numerical simulations were conducted on the gerotor type oil pump. Three oil pump models having different port and groove shape were considered. Firstly, two original models (baseline & variant.1 model) were simulated in order to validate the accuracy of the simulation results and to better understand the flow characteristics in the pump. It was found that the cavitation phenomenon as well as the teeth tip leakage is most important parameter on the pump performance. Based on the simulation results of the original models, final model (variant.2 model) which has improved port shape and pressure relief valve is suggested to enhance pump performance and to reduce driving torque. The volumetric efficiency and the hydraulic torque of the Variant.2 model is improved 4% and reduced 6.1% each at 2000RPM in experiment.

Cause Analysis for a Lining Damage in Sea Water System Piping Installed in a Korean Industrial Plant

  • Hwang, K.M.;Park, S.K.
    • Corrosion Science and Technology
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    • 제20권1호
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    • pp.1-6
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    • 2021
  • Many Korean industrial plants including nuclear and fossil power plants use seawater as the ultimate heat sink to cool the heat generated by various facilities. Owing to the high corrosivity of seawater, facilities and piping made of metal material in contact with seawater are coated or lined with polymeric materials to avoid direct contact with seawater. However, polymeric materials used as coating and lining have some level of permeability to water and are degraded over time. Korean industrial plants have also experienced a gradual increase in the frequency of damage to pipes in seawater systems due to prolonged operating periods. In the event of a cavitation-like phenomenon, coating or lining inside the piping is likely to be damaged faster than expected. In this paper, the cause of water leakage due to base metal damage caused by the failure of the polyester lining in seawater system piping was assessed and the experience with establishing countermeasures to prevent such damage was described.

J-Groove Technique for Suppressing Various Anomalous Flow Phenomena in Turbomachines

  • Kurokawa, Junichi
    • International Journal of Fluid Machinery and Systems
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    • 제4권1호
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    • pp.1-13
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    • 2011
  • In operating a turbomachine at off-design conditions various instabilities caused by anomalous flow phenomena occur and sometimes lead to the damage of a turbomachine. In order to avoid these phenomena various devices characteristic to each phenomenon have been developed, however they make turbomachines large-sized and cause efficiency drop. The present author has developed a very simple and innovative device, termed "J-groove," of suppressing various anomalous flow phenomena commonly by controlling the angular momentum of the main flow. It has been revealed that J-groove makes an operation of a turbomachine stable in all flow range, causes little efficiency drop, and can be easily applied to an existing machine. Here is reviewed totally the results of suppressing various anomalous flow phenomena in turbomachines.

75톤급 액체엔진 연소시험설비의 액체산소 과냉각 시스템 (Liquid Oxygen Supercooling System in the 75 tonf-class Liquid Engine Combustion Test Facility)

  • 서대반;유병일;이정호;조남경;김승한;한영민
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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    • pp.1080-1083
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    • 2017
  • 한국형발사체의 설계안에는 산화제 배관의 geysering 현상과 펌프 입구의 cavitation 현상을 방지하기 위하여 발사대기 중 산화제인 액체산소를 과냉각 하여 공급하는 시나리오가 포함되어 있다. 이 조건을 75톤급 엔진 개발 시험 단계에서 검증하기 위해 엔진 연소시험설비에는 액체산소를 과냉각 할 수 있는 시스템이 적용되었다. 여기에는 진공 이젝터를 이용한 방법과 탱크 내 헬륨 분사를 통한 방법이 적용되었으며, 성능 평가를 위해 각각에 대한 과냉각 시험이 수행되었다. 두 시험에서 모두 약 17분간 시험이 진행되었으며, 탱크 50%수위 지점 기준 이젝터를 이용한 시험에서는 약 3.3K, 헬륨 분사를 이용한 시 험에서는 약 2.2K 의 과냉각 결과를 나타내었다.

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LOX conditioning을 위한 재순환배관의 성능해석 및 설계인자 파악

  • 권오성;조남경;정용갑;조인현
    • 항공우주기술
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    • 제4권1호
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    • pp.196-202
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    • 2005
  • 액체추진기관의 극저온 추진제 공급부에서 추진제의 주입 후 대기시간 동안의 온도상승은 배관내의 geysering 현상 및, 점화시 터보펌프에서의 cavitation을 발생시킬 수 있다. 본 자료에서는 이런 문제를 해결하는 방법 중 하나인 재순환배관 방식에 대하여 KSLV-I 예비안의 산화제부 형상을 바탕으로 LOX를 산화제로 사용한 경우에 있어서 그 성능을 파악하였다. 또한, 다양한 parametric study를 통하여 재순환배관의 설계인자를 찾고자 하였다. 재순환배관의 직경, 초기 LOX 온도, 재순환배관 높이, ullage 압력, 열전달 계수 등의 변화에 의한 영향 및 추가적인 He 분사를 통한 순환 촉진 효과를 살펴보았다. 상용 열유체해석프로그램인 SINDA/FLUINT를 사용하였고 1차원적으로 해석을 수행하였다.

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