• Title/Summary/Keyword: Cavitation tests

Search Result 113, Processing Time 0.024 seconds

Cavitation studies on axi-symmetric underwater body with pumpjet propulsor in cavitation tunnel

  • Suryanarayana, Ch.;Satyanarayana, B.;Ramji, K.;Rao, M. Nageswara
    • International Journal of Naval Architecture and Ocean Engineering
    • /
    • v.2 no.4
    • /
    • pp.185-194
    • /
    • 2010
  • A pumpjet propulsor (PJP) was designed for an underwater body (UWB) with axi-symmetric configuration. Its performance was predicted through CFD study and models were manufactured. The propulsor design was evaluated for its propulsion characteristics through model tests conducted in a Wind Tunnel (WT). In the concluding part of the study, evaluation of the cavitation performance of the pumpjet was undertaken in a cavitation tunnel (CT). In order to assess the cavitation free operation speeds and depths of the body, cavitation tests of the PJP were carried out in behind condition to determine the inception cavitation numbers for rotor, stator and cowl. The model test results obtained were corrected for full scale Reynolds number and subsequently analyzed for cavitation inception speeds at different operating depths. From model tests it was also found that the cavitation inception of the rotor takes place on the tip face side at higher advance ratios and cavitation shifts towards the suction side as the RPS increases whereas the stator and cowl are free from cavitation.

Comparison of Cavitation Patterns between Model Scale Observations using Model and Full-Scale Wakes and Full Scale Observations for a Propeller of Crude Oil Carrier (원유운반선 프로펠러의 모형 및 실선 축척 반류에서의 공동현상과 실선에서 관측된 공동현상의 비교)

  • Choi, Gil-Hwan;Chang, Bong-Jun;Hur, Jae-Wook;Cho, Dae-Seung
    • Journal of the Society of Naval Architects of Korea
    • /
    • v.48 no.1
    • /
    • pp.15-22
    • /
    • 2011
  • In this paper, cavitation patterns of model tests were compared with those of full-scale measurement for a propeller of crude oil carrier which was suffered from erosions on suction side of blade tip region. Cavitation tests were performed at design and ballast draft using model and full scale nominal wakes. A model ship and wire mesh method was used for the simulation of wake patterns of model nominal wakes. For the prediction of full-scale wake patterns, a RANS solver(Fluent 6.3) was used and wire mesh method was used for the simulation of the full scale wakes. Comparison results show that cavitation patterns using predicted full-scale wake patterns are closer to cavitation patterns of full-scale measurement at ballast draft condition. Also, cloud cavitations were observed on the position of eroded area at both full-scale measurement and cavitation tests using simulated full-scale wake patterns.

The Hydraulic Tests of LOX Pumps for a Liquid Rocket Engine (로켓엔진용 산화제펌프의 수류 시험)

  • Kim, Dae-Jin;Hong, Soon-Sam;Choi, Chang-Ho;Kim, Jin-Han
    • 유체기계공업학회:학술대회논문집
    • /
    • 2006.08a
    • /
    • pp.523-526
    • /
    • 2006
  • A series of hydraulic and cavitation tests are performed in water environment in order to verify the hydraulic and cavitation performance of three types of LOX pumps. All the performances of the pumps are found to be satisfied with each design requirement. In the hydraulic tests, the head and efficiency are increased as the gap between floating ring seals and the impeller shoulder is decreased. In the cavitation tests, some pumps show decrease in the cavitation performance as the flowrate of the pump is decreased.

  • PDF

Effect of Tip Clearance on the Performance of a Turbopump Inducer (끝틈새가 터보펌프 인듀서의 성능에 미치는 영향)

  • Hong, Soon-Sam;Kim, Jin-Sun;Choi, Chang-Ho;Kim, Jinhan
    • 유체기계공업학회:학술대회논문집
    • /
    • 2004.12a
    • /
    • pp.558-563
    • /
    • 2004
  • Experiments were performed to see the effect of radial tip clearance on a turbopump inducer, which has two blades with inlet tip blade angle of 7.8 degree and tip solidity of 2.7. Hydraulic and cavitation tests were done for three cases of tip clearance ratio, that is, 0.026, 0.053, and 0.079. With increase in the tip clearance, inducer head and pressure on the inducer tip decreased. Attached cavitation and cavitation surge were found in the cavitation tests. In the attached cavitation one cell rotated at the same rotational speed as that of the inducer. Cavitation performance deteriorated with increase in the tip clearance. The level of casing vibration increased in the cavitation condition and the level was very high when the attached cavitation appeared.

  • PDF

Effect of Tip Clearance on the Performance of a Turbopump Inducer (끝틈새가 터보펌프 인듀서의 성능에 미치는 영향)

  • Hong, Soon-Sam;Kim, Jin-Sun;Choi, Chang-Ho;Kim, Jin-Han
    • The KSFM Journal of Fluid Machinery
    • /
    • v.9 no.1 s.34
    • /
    • pp.19-24
    • /
    • 2006
  • Experiments are carried out to investigate the effect of radial tip clearance on a turbopump inducer, which has two blades with inlet tip blade angle of 7.8 degree and tip solidity of 2.7. Hydraulic and cavitation tests are performed for three cases of tip clearance ratio, that is, 0.026, 0.053, and 0.079. With increase in the tip clearance, inducer head and pressure on the inducer tip decrease. Attached cavitation and cavitation surge are observed in the cavitation tests. In the attached cavitation one cell rotates at the same rotational speed as that of the inducer. Cavitation performance deteriorates with increase in the tip clearance. The level of casing vibration increases in the cavitation condition and the level is very high when the attached cavitation appears.

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

  • Jongwoo Ahn;Hanshin Seol;Hongseok Jeong;Youngha Park;Sanghwan Kim;Jungil Han
    • Journal of the Society of Naval Architects of Korea
    • /
    • v.61 no.3
    • /
    • pp.161-169
    • /
    • 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.

Electrochemical Approach on the Corrosion During the Cavitation of Additive Manufactured Commercially Pure Titanium (적층가공 방식으로 제조된 CP-Ti의 캐비테이션 중 부식에 대한 전기화학적 접근)

  • Kim, K.T.;Chang, H.Y.;Kim, Y.S.
    • Corrosion Science and Technology
    • /
    • v.17 no.6
    • /
    • pp.310-316
    • /
    • 2018
  • The effect of passive film on corrosion of metals and alloys in a static corrosive environment has been studied by many researchers and is well known, however few studies have been conducted on the electrochemical measurement of metals and alloys during cavitation corrosion conditions, and there are no test standards for electrochemical measurements 'During cavitation' conditions. This study used commercially additive manufactured(AM) pure titanium in tests of anodic polarization, corrosion potential measurements, AC impedance measurements, and repassivation. Tests were performed in 3.5% NaCl solution under three conditions, 'No cavitation', 'After cavitation', and 'During cavitation' condition. When cavitation corrosion occurred, the passive current density was greatly increased, the corrosion potential largely lowered, and the passive film revealed a small polarization resistance. The current fluctuation by the passivation and repassivation phenomena was measured first, and this behavior was repeatedly generated at a very high speed. The electrochemical corrosion mechanism that occurred during cavitation corrosion was based on result of the electrochemical properties 'No cavitation', 'After cavitation', and 'During cavitation' conditions.

Evaluation of Waterjet Cavitating Performances for a Amphibious Vehicle (수륙양용장갑차용 워터젯 추진기 캐비테이션 성능 평가)

  • Jaemoon Han;Dojun Kim;Jeongil Seo;Taehyung Kim;Gundo Kim;Jinsuk Lee
    • Journal of the Society of Naval Architects of Korea
    • /
    • v.60 no.5
    • /
    • pp.296-304
    • /
    • 2023
  • Cavitation tests for a waterjet propulsor of an amphibious vehicle are carried out in the Large Cavitation Tunnel. Waterjet pump performances and cavitation characteristics including thrust breakdown performances are investigated in the tests. In addition, cavitation characteristics for waterjet propulsors working inside the intake are calculated by using a commercial CFD code, Star-CCM+. Sliding mesh is implemented to a rotating impeller and the k-epsilon turbulence model is chosen. Cavitation bubble growth and collapse are estimated using the Schnerr-Sauer cavitation model based on Rayleigh-Plasset equation. Calculated results agree fairly well with experimental results. The re-design of the waterjet propulsor is performed to enhance waterjet cavitating performances and calculated results show that waterjet thrust breakdown characteristics are significantly improved.

Performance Tests of the Fuel Pump for a Turbopump (터보펌프용 연료펌프의 성능 시험)

  • Kim, Dae-Jin;Hong, Soon-Sam;Choi, Chang-Ho;Kim, Jinhan
    • 유체기계공업학회:학술대회논문집
    • /
    • 2004.12a
    • /
    • pp.655-659
    • /
    • 2004
  • Performance tests of the fuel pump for a turbopump unit have been successfully carried out in water environment. The tests are performed to evaluate the hydraulic and cavitation performances. The head and volute pressure distribution of the fuel pump followed the conventional similarity rule - unlike this, the secondary passage pressure distribution showed a small deviation from the conventional similarity rule. Also, critical cavitation number decreased as the rotational speed of the pump increased.

  • PDF

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
    • /
    • v.1 no.1
    • /
    • pp.76-90
    • /
    • 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.

  • PDF