• 한국음향학회지
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• 제26권5호
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• pp.220-226
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• 2007

캐비테이션 터널에서 소음계측 실험의 주 목적은 프로펠러 소음레벨 계측과 소음원의 위치 판별이다. 한국해양연구원의 소음계측 실험용 "저소음 대형 캐비테이션 터널"의 기초연구의 일환으로 소음계측 실험이 동 연구원의 소형 캐비테이션 터널에서 수행되었다. 본 실험에서는 프로펠러 캐비테이션이 발생할 수 있는 반류조건을 만들기 위해 반류 생성용 모형체(dummy body)를 제작하였고, 유동장 내의 청음기에 의한 자체소음을 줄이기 위해 유선형으로 설계된 하이드로포일내에 청음기 배열을 설치하였다. 다양한 압력조건에서 발생한 소음장과 가상 음원의 복제음장을 계측한 후, 소음원의 위치를 추적하기 위해 주파수 비상관 Bartlett 프로세서를 적용하였다. 본 논문에서는 수행된 소음계측 시험에 대해 기술하고, 계측된 소음의 분석 및 위치추적 결과를 제시한다.

• 대한조선학회지
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• 제49권4호
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• pp.33-40
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• 2012

• 대한조선학회논문집
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• 제39권2호
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• pp.1-10
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• 2002

선체-프로펠러-타의 상호작용 해석을 반복계산에 의해 수행하였다. 계측된 공칭속도를 입력자료로 하고 보오텍스 링 이론을 이용하여 유효속도를 계산함으로써 선체와 프로펠러사이의 상호작용을 고려하였고, 계산된 유효속도를 입력자료로 하여 프로펠러-타 상호작용을 계산할 수 있는 포텐셜 기저 패널법을 개발하였다. 프로펠러에 의해 타에 유기되는 속도와 반대로 타에 의해 프로펠러에 유기되는 속도는 수렴된 해가 얻어질 때까지 반복 계산하여 타 주위의 정상유동 해석을 수행하였다. 이와 함께 삼성중공업의 대형 캐비테이션 터널에서 L.D.V를 사용하여 프로펠러 및 타 주위의 유동장을 계측하였고 수치계산 결과와 비교하였다. 실선에 설치되고 있는 혼 타주위의 유동장 계산을 위해 gap flow 모델을 적용하였고, 여러 가지 타각에 대한 수치계산을 수행하여 대형캐비테이션 터널에서 계측된 타 표면에서의 압력과 비교하였으며, 계산된 표면 압력 치는 실험 값과 비교적 일치되는 만족스러운 결과를 얻었다.

• 대한조선학회논문집
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• 제37권2호
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• pp.22-29
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• 2000

고속 프로펠러들의 캐비테이션 소음특성이 KRISO의 캐비테이션 터널에서 실험적으로 연구되었다. 대형 고속선용 프로펠러에 대한 날개단면 및 부하분포의 변화에 대한 일련의 캐비테이션 소음이 계측되었으며, 이런 실험결과로부터 캐비테이션 형태 및 프로펠러 형상에 대한 소음성능이 분석되었다. 이러한 결과는 소음특성이 중요한 고속함정의 추진기 설계에 활용될 수 있을 것으로 보인다.

• 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.

• 대한조선학회논문집
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• 제59권5호
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• pp.271-279
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• 2022

In order to study the self-propulsion test and analysis techniques for the submerged body with pumpjet propulsors in the Large Cavitation Tunnel (LCT), at the Korea Research Institute of Ships and Ocean Engineering, a set of test equipment was designed and manufactured. The pumpjet propulsor is composed of rotor, stator and duct which results in the strong interaction between the components. To measure the thrust and torque for duct and stator, a ring-shaped sensor was applied. The test equipment including pumpjet is installed on the stern of the submerged body. As the whole pumpjet including duct and stator was considered as the propulsor from pumpjet open-water test, the self-propulsion test was conducted in the same way. The total thrust, combined thrust of rotor, duct and stator was used for the pumpjet self-propulsion test analysis. Accordingly, the self-propulsion test and analysis were conducted in the same way as those of the conventional propeller. The full-scale performances of the pumpjet propulsor were compared with those of the reference propeller. On the basis of the present study, it is thought that the pumpjet propulsor would be designed optimally.

• 대한조선학회논문집
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• 제52권6호
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• pp.428-434
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• 2015

The objective of the present study is to analyze the results of the trial-test for the full-scale driving pump, which is arranged in the LCT (Large Cavitation Tunnel). Firstly, the reasons of selecting the final design pump are introduced in terms of the performance analysis in model tests. The trial-test items for the full-scale driving pump are measurements of output current/voltage at the inverter of the main motor and the flow velocity in the LCT test section. The test results show the increase in flow rate of about 10.7% and the decrease in pump head of about 26%, compared with those of final design-pump specification. The motor power has the margin of about 22%. The performance analysis for the full-scale pump is conducted using the commercial code (CFX-10). The delivered power calculated with CFX-10 shows good agreement with that extracted from the full-scale pump test. It is found that CFX-10 is useful to analyze a full-scale pump.

• 대한조선학회논문집
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• 제38권3호
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• pp.23-30
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• 2001

고속 프로펠러들의 단면 및 기하학적 형상변화에 대한 캐비테이션 및 소음특성 연구가 새로운 실험장치를 이용하여 KRISO의 캐비테이션 터널에서 실험적으로 연구되었다. 대형 고속선형 프로펠러에 대한 날개단면, 부하분포 및 전개면적비 변화에 대한 일련의 캐비테이션 소음시험이 수행되었으며, 이런 실험결과로부터 캐비테이션 형태 및 프로펠러 형상에 대한 소음성능이 분석되었다. 새로운 실험장치를 이용하여 얻은 소음결과는 실선추정 및 고부하 저소음 추진기 설계에 유용한 자료로 활용될 수 있다.

• 대한조선학회논문집
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• 제57권3호
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• pp.133-139
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• 2020

In order to study the resistance test technique for the submerged body in Large Cavitation Tunnel (LCT), DARPA Suboff, submarine model publicly available was manufactured. DTRC released the resistance test data of DARPA Suboff conducted at ship speeds up to 18.0 knots in high-speed towing tank in 1990. As LCT is considered restricted waterways with walls, the resistance test results must be corrected with three wall blockage effects called buoyancy effect, solid blockage effect and wake blockage effect. Before correction, the resistance of LCT was 16~20 % higher than that of DTRC. After correction, the resistance and the resistance coefficients were compared with those of DTRC. The corrected resistance of LCT shows good agreement with that of DTRC. The residual resistance coefficient shows the difference according to the calculation method of buoyancy and frictional resistance coefficient. This paper suggests the best way for the calculation of residual resistance coefficient, On the basis of the present study, it is thought that the operating conditions for the propeller cavitation and noise tests can be drawn through LCT tests.

• 대한조선학회논문집
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• 제58권2호
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• pp.58-65
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• 2021

In order to study the self-propulsion test and analysis techniques for the submerged body in Large Cavitation Tunnel (LCT). DARPA Suboff, a submarine model publicly available was manufactured. The resistance results of DARPA Suboff was acquired from the LCT tests and compared with those of DTRC. After the wall blockage correction, the resistance results of LCT were in good agreement with those of DTRC. On the basis of the resistance results of LCT, the self-propulsion tests were conducted in LCT. The test objective was to get the full-scale propeller operating conditions for the propeller cavitation and noise tests. The test results of DARPA Suboff were analyzed in a way similar to the analysis techniques of those of the Towing Tank (TT). Another submerged body, for which self-propulsion tests were conducted in TT, was selected for results verification. The results of LCT were in good agreement with those of TT. On the basis of the present study, it is thought that the operating conditions for the full-scale submerged body can be drawn through LCT tests.