• Title/Summary/Keyword: Cavitation inception

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An Experimental Study on Noise Characteristics of Propeller Cavitation Inception (프로펠러 캐비테이션의 초기발생과 소음특성에 대한 실험연구)

  • Lee, Phil-Ho;Ahn, Byoung-Kwon;Lee, Chang-Sup;Lee, Jung-Hoon
    • Journal of the Society of Naval Architects of Korea
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    • v.48 no.1
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    • pp.1-7
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    • 2011
  • Cavitation is the formation of vapour bubbles of a flowing liquid in a region where the pressure of the liquid falls below its vapor pressure. Various types of cavitations are generated on the propeller blades. As cavity bubbles passing the blade are forced to oscillate in size or shape and come to collapse, they cause very strong local acoustic waves in the fluid and radiate noise. Comparing the Sound Pressure Level(SPL) before and after cavitation, SPL increases 2dB per 1 knot increase in ship speed above the cavitation inception speed(CIS). Consequently, the CIS is an important criteria to design silent propellers. In this work, experimental measurements of radiated noise according to various types of cavitations from the model propeller are carried out in a large cavitation tunnel and their acoustical characteristics are extensively investigated.

Cavitation inception in oil hydraulic pipeline (유압관로에서의 캐비테이션 초생)

  • 이일영;염만오;이진걸
    • Journal of Advanced Marine Engineering and Technology
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    • v.12 no.4
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    • pp.46-52
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    • 1988
  • The cavitation inception in oil hydraulic pipeline was investigated experimentally and numerically. In the experiment, negative pressures below-1 MPa(absolute pressure) were measured, associated with the transient flows in oil hydraulic pipeline. These experimental results show that the common hydraulic oil in the experimental pipeline withstands large tensions. In order to interpret the experimental results on cavitation inception, the growth of a spherical bubble in viscous compressible fluid due to a stepwise pressure drop was investigated by numerical analysis, and the critical bubble radius was obtained. The calculated value of the critical bubble radius corresponding to the negative pressure measured in the experiment is so small that the premised conditions about the bubble shape in the analysis is unsatisfactory. The physical significance of this calculated result implies the fact that there hardly exist free bubbles which can act as cavitation nuclei in the experimental pipeline.

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Experimental Study on the Cavitation Noise of a Hydrofoil (3차원 날개의 캐비테이션 소음 계측시험)

  • Lee, Seung-Jae;Seo, Jong-Soo;Han, Jae-Moon
    • Journal of the Society of Naval Architects of Korea
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    • v.44 no.2 s.152
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    • pp.111-118
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    • 2007
  • In order to investigate the noise characteristics of the different caviation, noise measurements were carried out in a large cavitation tunnel of the Samsuug Ship Model Basin(SSMB). The noise measurements for a 3-dimensional hydrofoil were carried out at the angle of attack of $12^{\circ}$ and $16^{\circ}$ according to the decrease in cavitation number. It is exhibited that sound pressure level(SPL) increased sharply with cavitation inception. The frequency of the noise induced by sheet cavitation was higher than that of tip vortex cavitation in the phase of cavitation inception. Within the range of the high frequency, in the case of fully developed cavitation, sheet cavitation noise was significantly increased in sound pressure level compared with tip vortex cavitation noise. In this study, the noise characteristics of the different cavitation types were considered experimentally and would be utilized as a basis for the analysis of propeller cavitation noise.

A Numerical Study on Cavitation Suppression Using Local Cooling

  • Zhang, Yuan-Yuan;Sun, Xiao-Jing;Huang, Dian-Gui
    • International Journal of Fluid Machinery and Systems
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    • v.3 no.4
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    • pp.292-300
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    • 2010
  • This study strives to develop an effective strategy to inhibit cavitation inception on hydrofoils by using local cooling technique. By setting up a temperature boundary condition and cooling a small area on the upper surface of a hydrofoil, the fluid temperature around the cooling surface will be decreased and thereby the corresponding liquid saturation pressure will drop below the lowest absolute pressure within the flow field. Hence, cavitation can never occur. In this paper, a NACA0015 hydrofoil at $4^{\circ}$ angle of attack was numerically investigated to verify the effectiveness of the proposed technique. The CFD results indicate that the cooling temperature and the cooling surface roughness are the critical factors affecting the success of such technique used for cavitation suppression.

A study on the improvement of cavitation inception speed for controllable pitch propeller in the actual warship (실선관측에 의한 가변추진기의 캐비테이션 초생속도 향상에 관한 연구)

  • Lim, Yong-Su;Jo, Kwan-Jun;Yeun, Je-Gil
    • Journal of Advanced Marine Engineering and Technology
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    • v.38 no.9
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    • pp.1170-1174
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    • 2014
  • If cavitation occurs in propeller, it generates vibration and noise accordingly which results in low efficiency of propeller. It's important to increase cavitation inception speed(CIS) since the noise of cavitation increases significantly from the beginning of cavitation. This paper describes the result of actual observation and measurement onboard ship with controllable pitch propeller(CPP), so as to verify the first occurrence phenomenon of cavitation. The research suggests new type of controllable pitch propeller with improved CIS at the bolt as it started with bolt cavitation as result of observation. It's not found bolt cavitation on the CPP proposed in this paper, furthermore its CIS is increased approximately by 4.5 knots than the existing CPP. The result of the research can be used for development of low-noise CPP and improving performance of CIS.

A Study on Autonomous Cavitation Image Recognition Using Deep Learning Technology (딥러닝 기술을 이용한 캐비테이션 자동인식에 대한 연구)

  • Ji, Bahan;Ahn, Byoung-Kwon
    • Journal of the Society of Naval Architects of Korea
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    • v.58 no.2
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    • pp.105-111
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    • 2021
  • The main source of underwater radiated noise of ships is cavitation generated by propeller blades. After the Cavitation Inception Speed (CIS), noise level at all frequencies increases severely. In determining the CIS, it is based on the results observed with the naked eye during the model test, however accuracy and consistency of CIS values are becoming practical issues. This study was carried out with the aim of developing a technology that can automatically recognize cavitation images using deep learning technique based on a Convolutional Neural Network (CNN). Model tests on a three-dimensional hydrofoil were conducted at a cavitation tunnel, and tip vortex cavitation was strictly observed using a high-speed camera to obtain analysis data. The results show that this technique can be used to quantitatively evaluate not only the CIS, but also the amount and rate of cavitation from recorded images.

Cavitation in Fuel Pump with 2D Cascade Modeling (2차원 Cascade에 의한 연료펌프의 공동발생 해석)

  • Quangnha, Thai;Lee, Chang-Jin
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.37 no.5
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    • pp.483-489
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    • 2009
  • A CFD code was developed to investigate the inception of cavitation around impeller blades of centrifugal fuel pump using two dimensional cascade modeling. With the verification test for numerical validity of the developed code, the prediction of the onset of cavitation was made for the configuration of a newly designed KHP fuel pump. The calculation results show impeller design was free of cavitation if the pump operates within the operational temperature and rotational speed range. However, the cavitation would be relatively easy to occur at off design region of fuel pump where the rotational speed is higher than design limit. Specially, the onset of cavitation is sensitively dependent on the increase in fuel temperature while the decrease in temperature will reduce the possibility of cavitation inception in the pump.

Study of the Cavitation Inception Speed (CIS) Improvement Through the Propeller Design and the Stern Appendage Modification (프로펠러 설계 및 선미 부가물 수정에 따른 캐비테이션 초기발생 선속(CIS) 성능 향상 연구)

  • Jong-Woo Ahn;Gun-Do Kim;Bu-Geun Paik;Young-Ha Park;Han-Shin Seol
    • Journal of the Society of Naval Architects of Korea
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    • v.60 no.4
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    • pp.231-239
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    • 2023
  • In order to improve the propeller Cavitation Inception Speed (CIS) performance, it needs to modify the propeller geometry and the wake distribution that flows into the propeller. In the previous study, the twisted angles of the V-strut were modified to improve propeller CIS, cavitation behavior and pressure fluctuation performances. Then the propeller behind the modified V-strut (New strut) showed better cavitation characteristics than that behind the existing V-strut (Old strut). However, the CIS of Suction Side Tip Vortex (SSTV) and Pressure Side Tp Vortex (PSTV) showed a big difference at behind each V-strut. In this study, the balance design is conducted to minimize the difference between SSTV CIS and PSTV CIS at behind each V-strut. To improve the propeller CIS performance, 1 propeller is designed at behind the old strut and 3 propellers are designed at behind the new strut. The propeller CIS is increased through the balance design and the stern appendage modification. The final propeller CIS is increased about 5.3 knots higher than that of the existing propeller at behind the old strut. On the basis of the present study, it is thought that the better improvement method for the propeller CIS would be suggested.

Propeller Tip Vortex Cavitation Control Using Water Injection (물 분사를 이용한 프로펠러 날개 끝 보오텍스 캐비테이션 제어)

  • Lee, Chang-Sup;Han, Jae-Moon;Kim, Jin-Hak;Ahn, Byoung-Kwon
    • Journal of the Society of Naval Architects of Korea
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    • v.47 no.6
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    • pp.770-775
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    • 2010
  • As considerable interests in noise emission from the ships have been increased, control of the propeller cavitation generating vibration and radiating noise is looming large. In general, the tip vortex cavitation is first produced in case of full scale propellers, and noise levels rise dramatically from that moment. In order to reduce induced noise from the tip vortex cavitation and hence increase the cavity inception speed, we propose the mass injection method. Water injected from the propeller tip decreases rotating speed of the tip flow, and it restrains growing the tip vortex cavity. Experimental investigations of the model tests carried out in a large cavitation tunnel show that the tip vortex cavitation is effectively controled by water injection from the propeller tip.

Study on estimation of propeller cavitation using computer vision (컴퓨터 비전을 이용한 프로펠러 캐비테이션 평가 연구)

  • Taegoo, Lee;Ki-Seong, Kim;Ji-Woo, Hong;Byoung-Kwon, Ahn;Kyung-Jun, Lee
    • Journal of the Korean Society of Visualization
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    • v.20 no.3
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    • pp.128-135
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    • 2022
  • Cavitation occurs inevitably in marine propellers rotating at high speed in the water, which is a major cause of underwater radiated noise. Cavitation-induced noise from propellers rotating at a specific frequency not only reduces the sonar detection capability, but also exposes the ship's location, and it causes very fatal consequences for the survivability of the navy vessels. Therefore cavity inception speed (CIS) is one of the important factors determining the special performance of the ship. In this study, we present a method using computer vision that can detect and quantitatively estimate tip vortex cavitation on a propeller rotating at high speed. Based on the model test results performed in a large cavitation tunnel, the effectiveness of this method was verified.