• 제목/요약/키워드: Cavitation observation

검색결과 43건 처리시간 0.028초

부분 프로펠러 날개 모형을 이용한 높은 레이놀즈 수에서의 공동시험 (Cavitation Test at High Reynolds Number Using a Partial Propeller Blade Model)

  • 최길환;장봉준;조대승
    • 대한조선학회논문집
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    • 제46권6호
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    • pp.569-577
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    • 2009
  • As the scale factor of model propellers utilized in cavitation test is about 40, it is difficult to find out practical countermeasures against the small area erosions on the blade tip region throughout model erosion tests. In this study, a partial propeller blade model was used for the observation of cavitation pattern for the eroded propeller. A partial propeller blade model was manufactured from 0.7R to tip with expanded profile and with adjustable device of angle of attack. Reynold's number of a partial propeller blade model is 7 times larger than that of a model propeller. Also, anti-singing edge and application of countermeasures to partial propeller blade model which produced in large scale can be more practical than a model propeller. For the observation of cavitation at high Reynold's number, high speed cavitation tunnel was used. To find out the most severe erosive blade position during a revolution, cavitation observation tests were carried out at 5 blade angle positions.

Development of KD-Propeller Series Using a New Blade Section

  • Lee, Jin-Tae;Kim, Moon-Chan;Ahn, Jong-Woo;Kim, Ho-Chung
    • Selected Papers of The Society of Naval Architects of Korea
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    • 제1권1호
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    • pp.76-90
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    • 1993
  • A new propeller series is developed using the newly developed blade section (KH 18 section) which has better cavitation characteristics and higher lift-drag ratio at wade angle-of-attack range than a conventional section. The radial patch distribution of the new series propellers is variable stance they were designed adaptively to a typical wake distribution. Basic geometric particulars of the series propellers. such as chord length, thickness, skew and rake distributions, are determined on the basis of recent full scale propeller geometric data. The series is developed for propellers having 4 blades, and blade area ratios of 0.3, 0.45, 0.6 and 0.75. Mean pitch ratios are varied as 0.5, 0.6, 0.7, 0.95 and 1.1 for each blade area ratio. The new propeller series consists of 20 propellers and is named as the KD(KRISO-DAEWOO)-propeller series. Propeller open-water tests are performed at the towing tank, and cavitation observation tests and fluctuating pressure tests are carried out at the cavitation tunnel of KRISO. $B_{p}-\delta$ curves, which can be used to select the optimum propeller diameter at the preliminary design stage, are derived from a regression analysis of the propeller open-water test results. The KD-cavitation chart is derived from the cavitation observation test results by choosing the local maximum lift coefficient and the local cavitation number as parameters. The cavity extent predicted by the KD-cavitation chart would be more accurate compared to that by an existing cavitation charts, such as the Burrll's cavitation chart, since the former is derived from the cavitation observation test results in a typical ship's wake, while the lather is derived from the test results in a uniform flow.

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

  • 임용수;조관준;연제길
    • Journal of Advanced Marine Engineering and Technology
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    • 제38권9호
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    • pp.1170-1174
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    • 2014
  • 추진기에서 캐비테이션이 발생되면 효율이 저하되고 진동과 소음이 발생한다. 소음은 캐비테이션이 처음으로 발생되는 시점부터 크게 증가되므로 캐비테이션 초생속도(CIS)를 가능한 높이는 것이 중요하다. 본 논문에서는 가변추진기의 캐비테이션 초기발생 현상을 확인하기 위하여 처음으로 캐비테이션 실선관측을 수행하였다. 관측 결과 가변추진에서 캐비테이션 초기발생은 볼트 캐비테이션으로 확인되어 볼트부위를 개선한 새로운 형상의 가변추진기를 제안하였다. 개선된 가변추진기에서는 볼트 캐비테이션이 전혀 발생되지 않았으며, CIS는 개선 전 가변추진기 보다 약 4.5 노트 향상된 것을 확인하였다. 본 연구 결과는 향후 저소음 가변추진기 개발과 CIS 성능 향상에 매우 유용한 자료로 활용될 것이다.

유동가시화를 이용한 혼-타의 간극유동 차단장치 효과에 관한 실험적 검증 (Experimental Verification on the Effect of the Gap Flow Blocking Devices Attached on the Semi-Spade Rudder using Flow Visualization Technique)

  • 신광호;서정천;김효철;유극상;오정근
    • 대한조선학회논문집
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    • 제50권5호
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    • pp.324-333
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    • 2013
  • Recently, rudder erosion due to cavitation has been frequently reported on a semi-spade rudder of a high-speed large ship. This problem raises economic and safety issues when operating ships. The semi-spade rudders have a gap between the horn/pintle and the movable wing part. Due to this gap, a discontinuous surface, cavitation phenomenon arises and results in unresolved problems such as rudder erosion. In this study, we made a rudder model for 2-D experiments using the NACA0020 and also manufactured gap flow blocking devices to insert to the gap of the model. In order to study the gap flow characteristics at various rudder deflection angles($5^{\circ}$, $10^{\circ}$, $35^{\circ}$) and the effect of the gap flow blocking devices, we carried out the velocity measurements using PIV(Particle Image Velocimetry) techniques and cavitation observation using high speed camera in Seoul National University cavitation tunnel. To observe the gap cavitation on a semi-spade rudder, we slowly lowered the inside pressure of the cavitation tunnel until cavitation occurred near the gap and then captured it using high-speed camera with the frame rate of 4300 fps(frame per second). During this procedure, cavitation numbers and the generated location were recorded, and these experimental data were compared with CFD results calculated by commercial code, Fluent. When we use gap flow blocking device to block the gap, it showed a different flow character compared with previous observation without the device. With the device blocking the gap, the flow velocity increases on the suction side, while it decreases on the pressure side. Therefore, we can conclude that the gap flow blocking device results in a high lift-force effect. And we can also observe that the cavitation inception is delayed.

5.5MW급 아지무스 추진기(azimuth thruster)에 대한 대형 캐비테이션 터널 모형시험 (Performance Test of 5.5MW Azimuth Thruster Model in LCT(Large Cavitation Tunnel))

  • 백부근;박영하;김기섭;김주인;나윤철
    • 대한조선학회논문집
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    • 제52권1호
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    • pp.34-42
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    • 2015
  • The development of an azimuth thruster which has the function of dynamic positioning and propulsion has been greatly required as the demand of vehicles with it increases. To develop or design a reliable azimuth thruster, it is appropriate that the performance and cavitation observation tests should be conducted in the regime of high Reynolds number. In the present study, to satisfy high Reynolds number condition new dynamometer for a large azimuth thruster is manufactured and arranged in the test section of the Large Cavitation Tunnel (LCT). The test method composed of the open water and the cavitation observation tests is established successfully in LCT, considering the thruster design.

복합재료를 이용한 유동유체 환경하의 각종 구조물의 캐비테이션 침식손상의 최소화 방안 (Minimizing of Cavitation-Erosion Damage for Various Structures using Composites under the various Condition of Fluid Flow Systems)

  • 이정주;김찬공;김용직;김윤해
    • 한국복합재료학회:학술대회논문집
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    • 한국복합재료학회 1999년도 추계학술발표대회 논문집
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    • pp.227-233
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    • 1999
  • This study is mainly concerned with phenomenon of cavitation-erosion on the several materials and corrosive liquids which were applied with vibrator (suggested by ASTM G-32, 20KHZ, 24{$mu}m$).The main results obtained are summarized as follows ; (1) The maximum erosion rate by cavitation erosion in both of fresh-water and sea-water appeared to be proportioned to their hardness and tensile strength. (2) Cavitation weight loss and rate of cast iron in sea-water condition were greater (approximately 3 times) than that in distilled-water condition, however in case of stainless and brass the cavitation weight loss and their rates were not so different in both of their conditions. (3) Cavitation weight loss of composite materials were shown as below on this test, DuraTough DL : Weight loss in sea-water condition were greater (approximately 2.3 times) than it's fresh-water condition. (4) As the result of observation with digital camea of specimens, the main tendency of cavitation erosion for metals, was that small damaged holes causing by cavitation e개sion was appeared with radial pattern, and composites materials was that small damaged holes were appeared randomly.

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프로펠러 및 선미반류에 의해 영향을 받는 혼-타의 캐비테이션 관찰 및 간극 유동에 대한 가시화 연구 (Cavitation Observation and Visualization of the Gap Flows on a Rudder Influenced by Propeller Slipstream and Hull Wakes)

  • 백부근;김경열;안종우;박선호;허재경;유병석
    • 대한조선학회논문집
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    • 제45권3호
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    • pp.238-246
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    • 2008
  • In the present study, the influences on the gap cavitaiton of the semi-spade rudder are investigated experimentally in the condition with propeller and hull wakes. To reduce the scale effect in the given experimental conditions, 1/28.5-scale-down models of propeller and rudder are manufactured. We have the propeller rotate ahead of the rudder, inducing the three dimensional effects originated from the propeller action. Experimental methods are composed of the cavitation observation using high speed camera, PIV (particle image velocimetry) measurements to visualize the cavitaition and flows around the gap. The propeller slipstream affects both of the gap flows and cavitation of the rudder.

선미 부가물 수정에 따른 프로펠러 캐비테이션 성능 향상 연구 (Study of the Propeller Cavitation Performance Improvement Through the Stern Appendage Modification)

  • 안종우;박영하;김건도;백부근;설한신;박일룡
    • 대한조선학회논문집
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    • 제60권1호
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    • pp.1-9
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    • 2023
  • In order to improve the propeller cavitation performance composed of Cavitation Inception Speed (CIS), cavitation extent and pressure fluctuation, it needs to improve the wake distribution that flows into the propeller. The warship propeller cavitation is strongly influenced by the wake created at the V-strut of various appendages. The inflow characteristics of the V-strut were investigated using Computational Fluid Dynamics (CFD) and the twisted angles of the V-strut were aligned with upstream flow. The resistance and self-propulsion tests for the model ship with the existing and modified V-struts were conducted in Towing Tank (TT), and wake distribution, CIS, cavitation observation and pressure fluctuation tests were conducted in Large Cavitation Tunnel (LCT). The propeller behind the modified V-strut showed better cavitation characteristics than that behind the existing V-strut. Another model test was conducted to investigate rudder cavitation performance by the change of the V-strut. The rudder cavitation characteristics were not improved by the change of the operating conditions. On the basis of the present study, it is thought that the stern appendages for better propeller cavitation performance would be developed.

균일류에서 프로펠러 앞날 근처 관통구가 모형 프로펠러 캐비테이션에 미치는 영향 (Influence of Thru Holes Near Leading Edge of a Model Propeller on Cavitation Behavior)

  • 안종우;박일룡;박영하;김제인;설한신;김기섭
    • 대한조선학회논문집
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    • 제56권3호
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    • pp.281-289
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    • 2019
  • In order to investigate the influence of thru holes near leading edge of model propeller on cavitation behavior, a model propeller with thru holes was manufactured and tested at Large Cavitation Tunnel (LCT). The pressure distribution around the thru hole on propeller blade was numerically calculated to help understand the local flow characteristics related to cavitation behavior. The model propeller is a five bladed propeller which has 2 blades with thru holes and 3 blades with smooth surface. The cavitation observation tests were conducted at angles of $0^{\circ}$ & $6^{\circ}$ using an inclined-shaft dynamometer in LCT. There are big difference on the suction side cavitation behavior each other due to the existence of thru hole. While the blades with thou holes start generation of the sheet cavitation from the leading edge on the suction side, the blades with smooth surface generate the cloud cavitation from the mid-chord. Cavitation on the blades with thru holes shows more similar behavior to those of the full-scale propeller of which the pipe line for air injection is closed. The numerical analysis result shows that the sharp pressure drop occurs around thru holes on the blade. Consequently, the thru hole around leading edge stimulates the cavitation occurrence and stabilizes the cavitation behavior. Based on these results, the effect of thru holes on propeller cavitation behavior behind a model ship should be studied in the future.

아지무스 추진기 캐비테이션 시험 장치 개발 및 캐비테이션 성능 연구 (Azimuth Thruster Cavitation Test Apparatus Development and Cavitation Performance Study)

  • 안종우;설한신;정홍석;박영하;김상환;한정일
    • 대한조선학회논문집
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    • 제61권3호
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    • pp.161-169
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    • 2024
  • In order to investigate cavitation performance for the azimuth thruster in Large Cavitation Tunnel (LCT), the cavitation test apparatus was designed and manufactured. Generally the model scale is determined by the pod dynamometer with about 70mm diameter. Recently as ships with azimuth thruster have become bigger, the problem of the model ship installation was occurred. The model ship with pod dynamometer couldn't be installed in the LCT test section. The cavitation test apparatus and technique which can conduct the cavitation test without pod dynamometer were developed. The cavitation tests were conducted in torque identity method instead of thrust identity method. The target ship with azimuth thruster is 18K LNG bunkering vessel. As the full-scale ship test was conducted, the model cavitation tests were conducted at the same operating conditions. The fluctuating pressure levels of the full-scale ship were compared to those of the model tests. Another model cavitation test was conducted in the foreign institute and the cavitation observation results were compared to those of LCT. Through the comparison with the existing results, it is thought that the cavitation test for the azimuth thruster can be conducted in torque identity method.