• 제목/요약/키워드: Cavitating flow analysis

검색결과 52건 처리시간 0.015초

Comparative Study on Viscous and Inviscid Analysis of Partial Cavitating Flow for Low Noise Propeller Design (저소음 프로펠러 설계를 위한 부분공동 유동의 점성 및 비점성 수치해석 비교 연구)

  • Kim, Ji-Hye;Ahn, Byoung-Kwon;Park, Cheol-Soo;Kim, Gun-Do
    • The Journal of the Acoustical Society of Korea
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    • 제33권6호
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    • pp.358-365
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    • 2014
  • When a ship propeller having wing type sections rotates at high speed underwater, local pressure on the blade decreases and various types of the cavitation inevitably occur where the local pressure falls below the vapor pressure. Fundamentally characteristics of the cavitation are determined by the shapes of the blade section and their operating conditions. Underwater noise radiated from a ship propeller is directly connected to the occurrence of the cavitation. In order to design low noise propeller, it is preferentially demanded to figure out key features: how the cavity is generated, developed and collapsed and how the effect of viscosity works in the process. In this study, we first perform inviscid analysis of the partial cavity generated on two dimensional hydrofoil. Secondly, viscous analysis using FLUENT with different turbulence and cavitation models are presented. Results from both approaches are also compared and estimated.

A Study on Propeller Noise Localizations in a Cavitation Tunnel Using MFP (정합장 처리를 이용한 캐비테이션 터널에서의 프로펠러 소음원 위치 추적에 관한 연구)

  • Park, Cheol-Soo;Cho, Yong-Jin;Seol, Han-Shin
    • The Journal of the Acoustical Society of Korea
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    • 제26권5호
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    • pp.220-226
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    • 2007
  • The two major objectives of acoustical measurements in a cavitation tunnel are measuring the noise levels generated by rotating propellers behind a hull and localizing possible noise sources in order to reduce noise levels. Propeller noise measurement experiments were performed in MOERI cavitation tunnel at December, 2006. In order to put the propeller into cavitating conditions, a wake-generating dummy body was devised. In addition, ten hydrophones are put inside a wing-shaped casing in order to minimize the unexpected flow induced self noise around hydrophone itself. After measuring both of the noises of the rotating propeller behind the dummy body and signals generated by a virtual source, respectively the data were matched field processed using the frequency incoherent Bartlett processor to localize noises on the propeller plane. In this paper, we presented the measured noise analysis and the localization results.