• The Journal of the Acoustical Society of Korea
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• v.38 no.3
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• pp.328-333
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• 2019

In this paper, to investigate the cavitation erosion phenomenon on the ship propeller, the correlation between the propeller noise and the cavitation intensity was analyzed. Cavitation erosion is closely related to cavitation collapsing intensity, which can be defined as the frequency and intensity of cavitation collapse. The pressure wave generated by cavitation collapse appears as a continuous acoustic pulse and this result is analyzed with the cavitation behavior to determine the relationship of the propeller noise to cavitation collapse intensity. This technique is applied to the propeller erosion test using the inclined shaft propeller model.

• Journal of Aerospace System Engineering
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• v.14 no.5
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• pp.100-106
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• 2020

Turbopumps for liquid rocket engines are exposed to various cavitation instabilities under their operating conditions. The instabilities affect the stability of the turbopumps. To make sure of the stability of the turbopump of KSLV-II, the present work examined the characteristics of the cavitation instabilities during the turbopump assembly test. In the test, the LOx pump was operated under super-synchronous rotating cavitation and attached to uneven cavitation. In the vibration analysis of the fuel pump, the characteristic frequency by the super-synchronous cavitation of the LOx pump was clearly shown.

• Journal of the Korean Society of Propulsion Engineers
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• v.11 no.1
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• pp.64-70
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• 2007

A test facility was developed where an inducer for a liquid rocket engine turbopump can be tested using liquid nitrogen as a working fluid. At the facility, a hydrodynamic performance test and a cavitation performance test for an oxidizer turbopump were carried out. Head-flow relation at liquid nitrogen test was similar to the case at water test. However, cavitation performance at the liquid nitrogen was superior to the case at water test, which results from the thermodynamic effect of cavitation.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2006.05a
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• pp.93-99
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• 2006

A test facility was developed where an inducer for a liquid rocket engine turbopump can be tested using liquid nitrogen as a working fluid. At the facility, a hydrodynamic performance test and a cavitation performance test for an oxidizer turbopump were carried out. Head-flow relation at liquid nitrogen test was similar to the case at water test. However, cavitation performance at the liquid nitrogen was superior to the case at water test, which results from the thermodynamic effect of cavitation.

• Proceedings of the Korean Institute of Surface Engineering Conference
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• 2017.05a
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• pp.119.2-119.2
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• 2017

무전해 니켈도금은 전기 공급 없이 환원재의 화학반응에 의해 도금이 진행되며, 복잡한 형상의 제품에도 균일한 도금 층을 형성시킬 수 있어 널리 적용되는 기술이다. 특히, 전기 니켈도금 층에 비해 무전해 니켈도금 층의 내식성과 내마모성이 우수하여 산업현장에서 가장 많이 사용되고 있다. 그러나 해양환경에서 빠른 유속 변화에 의해 발생되는 캐비테이션-침식 방지를 위한 무전해 니켈도금의 적용은 전무한 실정이다. 따라서 본 연구에서는 회주철의 캐비테이션-침식 방지를 위해 최적의 무전해 니켈도금 조건을 규명하고, 그 캐비테이션 저항성을 평가하고자 하였다. 무전해 니켈코팅을 위한 모재는 gray cast iron (FC250)을 $19.5mm{\times}19.5mm{\times}5mm$의 크기로 제작하였다. 회주철의 인장강도는 $330N/mm^2$이며, 그 성분 조성(wt.%)은 3.23 C, 1.64 Si, 0.84 Mn, 0.016 P, 0.013 S 그리고 나머지는 Fe이다. 시험편은 SiC 페이퍼 grit #1200까지 연마하였으며, 시험편의 표면 거칠기(centre line average, Ra)는 $1.6-2.1{\mu}m$ 범위 내로 제작하였다. 연마된 시험편은 증류수(distilled water) 세척 후 hot air로 건조하였다. 무전해 도금 전 시험편은 탈지를 위해 아세톤 용액(room temperature, RT)에서 3분간 초음파 세척하고, $90^{\circ}C$의 알카리 수용액으로 5분간 세척하였다. 그리고 표면활성화를 위한 산세척(acid pickling)은 5% sulfuric acid 용액에서 30초 동안 실시하였다. 무전해 Ni-P(electroless nickel, EN) 도금 전과 모든 과정마다 증류수로 시험편을 철저하게 세척하였다. EN 도금을 위한 도금욕(the bath)은 기존 문헌 연구를 통해 조성성분, 도금조건 및 변수들(the parameters)의 적절한 범위를 결정하였다. 도금조로 500mL 비커를 사용하였으며, 모든 시험편은 2시간 동안 EN deposition을 실시하였다. 캐비테이션 실험 결과 EN 도금의 표면경도가 증가함에 따라 캐비테이션 저항성도 현저하게 향상되었다.

• Bulletin of the Society of Naval Architects of Korea
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• v.31 no.4
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• pp.10-13
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• 1994

최근 선박의 대형화, 고속화로 인하여 추진기의 부하가 증가되고 있으며, 특히 최근 등장한 1,000TEU급 콘테이너선의 경우 추진기가 흡수해야되는 축마력이 70,000HP 이상인 경우도 잇다. 커다란 축마력을 흡수하여 선박을 빠른 속도로 추진시켜야 되는 최근의 추진기는 작동 원리상 캐비테이션 발생을 피할 수 없으며 캐비테이션 발생량의 허용범위 및 캐비테이션 거동의 특성을 고려하여 추진기를 설계하여야 된다. 캐비테이션의 여유가 없이 추진기 설계가 수행되기 때문에 추진기 캐비테이션의 성능해석은 엄밀한 정밀도가 요구된다. 캐비테이션이란 일정한 온도에서 유체동력학 작용에 의해서 유체주위의 압력이 일정한 압력(예 : 증기압) 이하로 낮아질 때 물이 기화하여 수증기로 변하면서 빈 공간을 형성하는 현상을 말한다. 이렇게 발생된 캐비티는 주위 압력환경에 따라 생성, 성장, 수축, 붕괴의 과정을 거치게 된다. 특히 붕괴의 과정은 짧은 시간 내에 급격히 진행되기 때문에 진동 및 소음의 원인이 되고, 심할 경우 추진기 혹은 주위 물체 표면에 침식작용의 원인이 되기도 한다. 본 고에서는 캐비테이션의 물리적 특성 및 분류방법을 간단히 소개하고, 캐비테이션에 의한 선박추진기의 성능저하 특성 및 모형시험 기법을 이용한 캐비테이션 성능해석법을 소개하였다.

• Journal of the Korean Society of Propulsion Engineers
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• v.18 no.3
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• pp.84-91
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• 2014

The flow rate control of a cavitating venturi has been investigated with downstream pressure variation. A set of cavitating venturies for a liquid rocket engine thrust chamber firing test facility have been designed and manufactured. The flow characteristics of the cavitating venturies have been analyzed by experimental and computational methods. Results showed that constant mass flow rate condition was established by the cavitation inside the venturi. However, upstream pressure less than the actual design pressure of the cavitating venturi could not supply a constant flow rate.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• v.y2005m4
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• pp.243-247
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• 2005

Hydraulic performance test was conducted for a fuel pump of a liquid rocket engine turbopump. The pump driven by an electric motor was tested in water environment. It is experimentally shown that the inducer had very small effect on the pimp's head and efficiency but great effect on the pump's cavitation performance. Additionally, inducer test was carried out to investigate the effect of the inducer on the pump in detail, and it was found that the pump had a critical cavitation number when the inducer head dropped by $55\%$.

• Journal of the Korean Society of Propulsion Engineers
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• v.10 no.1
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• pp.18-22
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• 2006

Hydrodynamic performance test was conducted for a fuel pump of a liquid rocket engine turbopump. The pump driven by an electric motor was tested using water. It is experimentally shown that the inducer had very small effect on the pump's head and efficiency but great effect on the pump's cavitation performance. Additionally, inducer test was carried out to investigate the effect of the inducer on the pump in detail, and it was found that the pump reached a critical cavitation number when the inducer head dropped by 55%.

• Journal of the Society of Naval Architects of Korea
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• v.38 no.3
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• pp.23-30
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• 2001

The cavitation noise of high-speed propellers was experimentally studied using new measurement device in KRISO cavitation tunnel. A series of cavitation noise tests were carried out for 6 propellers with various sections, loading distributions, and a different area ratio. From the experimental results, the noise characteristics for various cavitation patterns and the noise performance for a series of propellers were analyzed. These can be used for full-scale prediction study of the noise and optimum design of high-speed propellers.