• 제목/요약/키워드: Turbulent Boundary Layer Pressure Fluctuation

검색결과 17건 처리시간 0.021초

유연재 코팅 평판의 난류 변동압력 특성에 관한 실험적 연구 (Experimental Study on the Characteristics of Turbulent Wall Pressure Fluctuation Over Compliant Coatings)

  • 박경훈;이승재;신구균
    • 한국음향학회지
    • /
    • 제26권6호
    • /
    • pp.293-300
    • /
    • 2007
  • 수중운동체가 주행할 때 수중운동체의 표면에는 난류 경계층이 형성되고, 난류 경계층 내 벽면 변동압력은 탄성체인 수중운동체의 표면을 가진시켜 유동 유기 소음을 발생시킨다. 이러한 유체 소음을 감소시키기 위한 하나의 방법으로 수중운동체 표면에 유연재를 부착하여 수중운동체의 유동 유기 방사 소음을 감소시키는 방법이 제안되기도 한다. 본 논문에서는 유연재 부착에 따른 수중에서의 유체소음의 변화 특성을 살펴보기 위하여 유연재가 코팅되지 않은 강판 시편과, 고무 재질의 Neoprene 및 폴리우레탄 재질의 유연재가 부착된 강판시편을 저소음 공동수조에 설치한 후 여러 가지 유속 조건에서 유체소음의 주요 소음원인 난류 경계층 내 벽면 변동압력을 측정하고 그 결과를 비교 분석하였다. 그 결과 유연재를 코팅한 경우에는 유연재로 인하여 난류 경계층의 두께가 두꺼워지는 등 경계층 유동이 변화하지만, 유연재에서의 난류 에너지의 소산으로 인하여 고주파수 대역에서 약 10dB의 벽면 변동압력의 감소 효과를 확인할 수 있었다.

역압력 구배가 존재하는 난류 경계층의 발달에 트리핑 구조물이 미치는 영향에 관한 연구 (The effects of tripping structure on the development of turbulent boundary layer subjected to adverse pressure gradient)

  • 임태현;김대성;윤순현
    • 한국마린엔지니어링학회:학술대회논문집
    • /
    • 한국마린엔지니어링학회 2001년도 추계학술대회 논문집(Proceeding of the KOSME 2001 Autumn Annual Meeting)
    • /
    • pp.36-44
    • /
    • 2001
  • The effects of various tripping structures on turbulent boundary layer subjected to adverse pressure gradient were examined. The profiles are compared to zero pressure gradient and adverse pressure gradient. The increases of tripping structures of height, k are affects almost flow parameter included velocity fluctuation, skin friction coefficient and turbulent boundary thickness.

  • PDF

적층구조물내의 유체유발 탄성응력파의 전파해석 및 1 자유도계 모델링 (An Analysis of the Wave Propagation of the flow-induced Elastic Stress Waves in the Layered Structure and it's 1 D.O.F. Modelling)

  • Lee, J.K.;Lee, U.S.
    • 한국정밀공학회지
    • /
    • 제12권11호
    • /
    • pp.132-139
    • /
    • 1995
  • Turbulent boundary layer pressure fluctuation exerted on the surface of a structure can give rise to a elastic stress wave on the surface of the structure. The stress wave so called surface wave, will not only propagate along the surface of structure but also penerate into the structure. To reduce the transmission of stress wave into the structure the elastomer layer is usually attactched on the surface of structure. The transfer function, which is defined herein as the ratio of stress waves at the surface and bottom of the elastomer layer, is derved by use of the cylindrical coordinates system. The elastodynamics of the elastomer layer subjected to the turbulent boundary layer pressure fluctuation is represented by the simplified one degree-of-freedom model for easy prediction of the stress wave transmission as well as efficient design of the elastomer layer.

  • PDF

축대칭 물체 선단에서 발생하는 경계층 내 벽면 변동 압력에 관한 연구 (Wall Pressure Fluctuations of the Boundary Layer Flow at the Nose of and Axisymmetric Body)

  • 신구균;홍진숙;김상윤;김상렬;박규철
    • 소음진동
    • /
    • 제10권4호
    • /
    • pp.602-609
    • /
    • 2000
  • When an axisymmetric body moves through air the boundary layer near the stagnation region remains laminar and subsequently it goes through transition to turbulent. The experimental investigation described in this paper concerns the characteristics of wall pressure fluctuations at the initial stage of boundary layer flow including transition. Flush-mounted microphones are used to measure the wall pressure fluctuations at the transition and turbulent boundary layer region of a blunt axisymmetric body in the low noise wind tunnel. It if found from this study that the wall pressure fluctuations in the transition region is higher than that in the turbulent region.

  • PDF

난류경계층에 의한 다층재질 원통형 실린더의 유체소음 해석 연구 (A Study of Flow Induced Noise for Multilayered Cylinder due to Turbulent Boundary Layer)

  • 신구균;홍진숙;이헌곤
    • 소음진동
    • /
    • 제6권5호
    • /
    • pp.671-677
    • /
    • 1996
  • This paper presents the analytical method for predicting turbulence- induced noise in the multilayered cylinder composed of an outer hose, an inner fluid and an internal core. It is assumed that an infinite axisymmetric cylinder is located horizontally in water with free stream velocity and the turbulent boundary layer (TBL) surrounding the outer hose is fully developed and homogeneous. The transfer function at the core surface due to the propagation of the pressure fluctuation within the TBL is formulated using the linearized Navier-Stockes equation for solid and fluid. In the estimation of the energy spectrum of wall pressure fluctuation, the empirical formula proposed by Strawderman based on the Corcos model is used. A general algorithm for the calculation of the pressure level at the surface of a core, that is, turbulence- induced noise, is presented. Through the detailed numerical simulation, it is found that the major noise mechanism is the propagation of the bulge wave along hose.

  • PDF

선저 소나돔의 유체소음원 특성 분석 (Investigation of Flow Noise Source of Hull Mounted Sonar Dome)

  • 신구균;강명환;이종주;서영수;이경준
    • 한국소음진동공학회:학술대회논문집
    • /
    • 한국소음진동공학회 2014년도 추계학술대회 논문집
    • /
    • pp.575-576
    • /
    • 2014
  • The Hull Mounted Sonar Dome housing the sonar sensor array is a ship's structure protruded from ship bottom, which is under turbulent flow. The flow of sonar surface is highly disturbed and turbulent. In this case the wall pressure fluctuations within the turbulent boundary layer are one of the most important flow induced self noise sources of the SONAR system. We investigate the characteristics of the wall pressure fluctuations of the hull mounted sonar dome through the model test in the cavitation tunnel. This paper contains the wall pressure fluctuation spectra at various free stream velocities.

  • PDF

난류 경계층 내 벽면 변동 압력의 구조 기진력 모델링 (A Modelling of Structural Excitation Forces Due to Wall Pressure Fluctuations in a Turbulent Boundary Layer)

  • 홍진숙;신구균;김상윤
    • 소음진동
    • /
    • 제11권2호
    • /
    • pp.226-233
    • /
    • 2001
  • It is essential to analyze structural vibrations due to turbulent wall pressure fluctuations over a body surface which moves through a fluid, because the vibrations can be a severe source of noise affecting to passengers in airplanes and SONAR performance. Generally, this kind of problems have been solved for very simplified models, e.g. plates, which can be applied to the wavenumber domain analysis. In this paper, a finite element modeling of the walt pressure fluctuations is investigated, which can be applied to those over arbitrary smooth surfaces. It is found that the modeled wall pressure fluctuation at nodes becomes uncorrelated at higher frequencies and at lower flow speeds, and the response is over-estimated due to the aliased power. Then the frequency range available for uncorrelated loading model and two power correction schemes are presented.

  • PDF

난류 경계층 내 벽면 변동 압력의 구조 기진력 모델링 (A Modelling of Structural Excitation Forces Due to Wall Pressure Fluctuations in a Turbulent Boundary Layer)

  • 홍진숙;신구균
    • 한국소음진동공학회:학술대회논문집
    • /
    • 한국소음진동공학회 2000년도 춘계학술대회논문집
    • /
    • pp.817-824
    • /
    • 2000
  • It is essential to analyze structural vibrations due to turbulent wall pressure fluctuations over a body surface which moves through a fluid, because the vibrations can be a severe source of noise affecting to passengers in airplanes and SONAR performance. Generally, this kind of problems have been solved for very simplified models, e.g. plates, which can be applied to the wavenumber domain analysis. In this paper, a finite element modeling of the wall pressure fluctuations over arbitrary smooth surfaces is investigated. It is found that the modeled wall pressure fluctuation at nodes becomes uncorrelated at higher frequencies and at lower flow speeds, and the response is over-estimated due to the aliased power. Finally, the frequency range available for uncorrelated loading model and two power correction schemes are presented.

  • PDF

수치 해석을 이용한 난류 경계층 내 벽면 변동 압력을 받는 보의 진동 해석 (Vibration of Beams Induced by Wall Pressure Fluctuation in Turbulent Boundary Layer Using Numerical Approaches)

  • 유정수;김은비
    • 한국소음진동공학회논문집
    • /
    • 제23권8호
    • /
    • pp.698-706
    • /
    • 2013
  • Structural vibration induced by excitation forces under turbulent boundary layer is investigated in terms of the numerical analysis in this paper. Since the responses of structures excited by the wall pressure fluctuation(WPF) are described by the power spectral density functions, they are calculated and reviewed theoretically for finite and infinite length beams. For the use of numerical approaches, the WPF needs to be discretized but conventional finite element method is not much effective for that purpose because the WPF lose the spatial correlation characteristics. As an alternative numerical technique for WPF modelling, a wavenumber domain finite element approach, called waveguide finite element method, is examined here for infinite length beams. From the comparison between the numerical and theoretical results, it was confirmed that the WFE method can effectively and easily cope with the excitation from WPF and hence the suitable approach.

평판 난류경계층에서의 벽 압력섭동에 대한 실험적 연구 (Experimental Study on Wall Pressure Fluctuations in the Turbulent Boundary Layer on a Flat-Plate)

  • 이승배;김휘중
    • 대한기계학회논문집B
    • /
    • 제23권6호
    • /
    • pp.722-733
    • /
    • 1999
  • The wall pressure fluctuations of a turbulent boundary layer over a flat plate have been investigated in an anechoic wind tunnel facility. The anechoic wind tunnel consists of acoustically-lined duct, muffler, and splitter-type silencer for noise suppression and vanes for reducing head losses involved. To improve spectra characteristics in high frequency range, a 1/8" pressure-type microphone sensor, which has a pin-holed cap of various diameters, was employed in this experiment. It was shown that the pin-holed microphone sensor with a dimensionless diameter $d^+$ of 7.1 resolved the high frequency pressure fluctuations most effectively among ones with various pin-hole diameters. The measured wall pressure spectra in terms of three types of scaling parameters were in good agreement with other experimental and numerical results. The pressure events of high amplitude were found to contribute to total fluctuating pressure energies in the turbulent boundary layer significantly and supposed to radiate to the far-field effectively.