• 제목/요약/키워드: 경계층난류

검색결과 293건 처리시간 0.031초

난류 경계층에서 컴플라이언트 코팅과 점탄성 벽면의 방사 소음에 관한 실험적 연구 (Radiated Sound from Compliant and Viscoelastic Plates in a Turbulent Boundary Layer)

  • 이승배;이창준;권오섭;전우평
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2002년도 학술대회지
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    • pp.779-782
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    • 2002
  • We examine the problem in which porous/viscoelastic compliant thin plates are subject to pressure fluctuations under transitional or turbulent boundary layer. Measurements are presented of the frequency spectra of the near-field pressure and radiated sound by compliant surface. A porous plate consisting of 5mm thick, open-cell foam with fabric covering and a viscoelastic painted plate of 1mm thick over an acoustic board of 4m thick were placed over a rigid surface in an anechoic wind tunnel. Streamwise velocity and wall pressure measurements were shown to highly attenuate the convective wall pressure energy when the convective wavenumber ($k_{ch}$) was 3.0 or more. The sound source localization on the compliant walls is applied to the measurement of radiated sound by using an acoustic mirror system.

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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
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    • 한국소음진동공학회 2000년도 춘계학술대회논문집
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    • pp.817-824
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    • 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.

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남극환경을 위한 고상식 건물의 Design Guideline에 관한 연구(I)-풍하중 (Design Guidelines of Elevated Buildings for Antarctic Environment (I)-Wind Load)

  • 김동혁
    • 한국해양공학회지
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    • 제4권2호
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    • pp.22-34
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    • 1990
  • 남극환경은 남극의 거센 바람 및 이에 수반되는 적설현상을 피하기 위해 땅에서 띄우는 고상식 및 지하에 설치하는, 두가지의 형태를 취하고 있다. 고상식의 경우 건물밑으로 바람을 통하게 함으로써 적설현상을 피하는데 효과적이기는 하나 남극의 거센 바람에 대응하기 위하여 구조적인 문제를 해결해야 하는 취약점을 지니고 있다. 본 연구는 경계층난류풍하를 이용하여 고상식 남극건물에 가해지는 풍하중을 파악함으로서 남극건물의 design guide line을 제시하였다.

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난류 경계층에서 컴플라이언트 코팅된 벽면과 점탄성 벽면의 방사 소음에 관한 실험적 연구 (Radiated Sound from Compliant and Viscoelastic Plates in a Turbulent Boundary Layer)

  • 이창준;이승배;권오섭;전우평
    • 대한기계학회논문집B
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    • 제27권3호
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    • pp.294-301
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    • 2003
  • We examine a problem in which porous/viscoelastic compliant thin plates are subject to pressure fluctuations under transitional or turbulent boundary layer. Measurements are presented of the frequency spectra of the near-field pressure and radiated sound by compliant surface. A porous plate consisting of 5mm thick. open-cell foam with fabric covering and a viscoelastic-painted plate of 1mm thick over an acoustic board of 4mm thick were placed over a rigid surface in an anechoic wind tunnel. Streamwise velocity and wall pressure measurements were shown to highly attenuate the convective wall pressure energy when the convective wavenumber (k$_{c}$h) was 3.0 or more. The sound source localization on the compliant walls is applied to the measurement of radiated sound by using an acoustic mirror system.

난류경계층의 헤어핀 다발구조에 대한 3차원 토폴로지 규명 (Identification of the three-dimensional topology of hairpin packet structures in turbulent boundary layers)

  • 권성훈;김경천
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2003년도 추계학술대회
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    • pp.610-615
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    • 2003
  • This experiment has been carried out to find the structure of turbulent boundary layer with instantaneous velocity fields obtained in stream-wall-normal planes using a stereo-PIV (Particle Image Velocimetry) method. And it has been measured perpendicular plane and horizontal plane with hairpin vortex structure by Reynolds number change and made third dimension shape for section of horizontal plane through stereo-PIV. In the outer layer hairpin vortices occur in streamwise-aligned packets that propagate with small velocity dispersion. A streaky structure is composed of counter-rotating vortex. According as y+ increases, streaky structure's interval space decrease, and it shows that hairpin shape of prior research is vertified. The objective of the present research is to gain a better understanding of coherent structures in the outer of wall turbulence by experimentally examining coherent structures.

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횡 방향 진동하는 전자기력에 대한 공간 발달하는 난류 경계층의 반응 (Response of Spatially Developing Turbulent Boundary Layer to Spanwise Oscillating Electromagnetic Force)

  • 이중호;성형진
    • 대한기계학회논문집B
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    • 제29권11호
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    • pp.1189-1198
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    • 2005
  • Direct numerical simulations were performed to investigate the physics of a spatially developing turbulent boundary layer flow subjected to spanwise oscillating electromagnetic forces in the near wall region. A fully implicit fractional step method was employed to simulate the flow. The mean flow properties and the Reynolds stresses were obtained to analyze the near-wall turbulent structure. It is found that skin friction and turbulent kinetic energy can be reduced by the electromagnetic forces. The decrease in production is responsible fur the reduction of turbulent kinetic energy. Instantaneous flow visualization techniques were used to observe the response of streamwise vortices and streak structures to spanwise oscillating forces. The near-wall vortical structures are affected by spanwise oscillating electromagnetic forces. Following the stopping of the electromagnetic force, the flow eventually relaxes back to a two-dimensional equilibrium boundary layer.

파형 표면을 갖는 원형실린더의 공력특성 (Aerodynamics Characteristics of Circular Cylinders with Riffled Surfac)

  • 김용주;원창희;이승수
    • EDISON SW 활용 경진대회 논문집
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    • 제3회(2014년)
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    • pp.539-543
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    • 2014
  • 임의의 물체가 유체 내에서 운동하거나 정지해 있을 때 유체에 의해서 운동에 방해가 되는 힘을 형상저항이라고 한다. 형상저항은 레이놀즈수에 의한 경계층의 흐름형태에 따라 변화하며, 경계층의 흐름형태는 레이놀즈수가 $10^5$보다 작은 경우 층류로, 그 이상의 경우 난류로 나타난다. 본 연구에서는 유체 내에 물체가 정지해 있을 경우 조도에 따른 형상저항의 변화를 알아보기 위해 각기 다른 조도를 가진 실린더를 모델링해 EDISON_CFD을 이용하여 전산 해석을 하였다. 실린더의 표면에 파장의 주기와 진폭, 층류와 난류 영역에서의 항력계수의 변화에 대해 검토하였다.

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OpenFOAM과 어댑티드 격자를 이용한 난류 경계층의 직접 수치 모사 (Direct Numerical Simulations of Turbulent Boundary Layer using OpenFOAM and Adapted Mesh)

  • 이상봉
    • 대한조선학회논문집
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    • 제53권3호
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    • pp.210-216
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    • 2016
  • Direct numerical simulations of a spatially developing turbulent boundary layer on a flat plate have been performed to verify the applicability of OpenFOAM and adapted mesh with prism layers to turbulent numerical simulation with high fidelity as well as provide a guideline on numerical schemes and parameters of OpenFOAM. Reynolds number based on a momentum thickness at inlet and a free-stream velocity was Reθ=300. Time dependent inflow fields with near-wall turbulent structures were generated by a method of Lund et al. (1998), which was to extract instantaneous velocity fields from an auxiliary simulation with rescaled and recycled velocities at inlet. To ascertain the statistical characteristics of turbulent boundary layer, the mean profiles of streamwise velocity and turbulent intensities obtained from structured and adapted meshes were compared with the previous data.

전난류에서의 파마찰계수 (Wave Friction Factor far Rough Turbulent Flow)

  • 유동훈
    • 한국해안해양공학회지
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    • 제5권2호
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    • pp.51-57
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    • 1993
  • 포텐셜 이론으로 구해지는 해저면 유속은 일반적으로 난류경계층에서의 파유속과 같다고 가정한다. 해저면 가까이에서 파운동에 의한 유속분포를 해석하기 위한 최근의 이론과 수치모형에서 발견되는 실험결과와의 오차는 주로 이 가정의 문제점으로부터 연유하는 것으로 사료된다. 경계층 최상점에서의 유속에 대한 이론치와 실유속치와의 관계식을 본고에서 제의하였다. 이 관계식을 이용하여 Jonsson(1967)과 Fredsoe(1984)가 각각 개발한 기존 이론식을 수정하였으며, 수정된 이론을 이용하여 파마찰계수를 산정한 결과, 발표된 실험치들과 비교하여 상당한 향상을 얻을 수 있었다.

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영압력 구배 난류 경계층에서 표면조도가 미치는 영향 (The Effect of Surface Roughness on the Zero Pressure Gradient Turbulent Boundary Layers)

  • 김문경;윤순현;김동건
    • Journal of Advanced Marine Engineering and Technology
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    • 제29권4호
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    • pp.453-460
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    • 2005
  • Experiments were conducted to investigate the effect of the surface roughness on the flat plate turbulent boundary layer. The square rods were installed at the leading edge to make surface roughness. The particle image velocimetry was used to measure the mean velocities and velocity fluctuation component. All measurements were made over a range of w/k=1. 2 5 and $Re_x=80.000{\sim}360,000$. Friction velocity was measured by using Clauser plot method. The level of turbulent intensities on roughness surface appears more strongly than that of turbulent intensities on flat plate. A correlation of boundary layer thickness in term of $Re_x$ and w/k are presented.