• Title/Summary/Keyword: 점근해

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Analysis of Underwater Noise in the North Sea (북해에서의 수중소음분석)

  • 윤갑동
    • Journal of the Korean Society of Fisheries and Ocean Technology
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    • v.21 no.1
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    • pp.1-6
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    • 1985
  • The underwater noise was measured by piezo-electric hydrophones submerged in the water at three different depths. The signals were led through connection cables to preamplifiers, and recorded simultaneously by a four channel tape recorder, and analysed by high resolution signal analyzer. The measurements were carried out at the fjord Skossvassen in archipelago off Bergen and at the cost of Norway in the North Sea. The results of the measurements and the analysis showed that the underwater noise consists of a steady broad band noise superposed by intermittent pulse of various strength. The noise levels measured in fjord Skossvassen indicated that they were generally higher at the shallow (10m) hydrophone than at the deeper hydrophone (25m, 50m). This tendency was not very distinct, however, the noise sources are close to the surface. The underwater noise spectrums measured in the open sea of Norway showed almost similar situation in all layers. This tendency showed that the noise sources are not close to the surface but they are far away from the measuring positions.

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Comparison of the Insertion Loss Results of Semi-infinite Plane Screen by the Analytical Method and Boundary Element Method (반무한 방음벽의 삽입손실의 이론과 BEM해석에 의한 결과치 비교)

  • 김문섭;김관주
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 1995.10a
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    • pp.25-31
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    • 1995
  • 본 연구는 방음벽의 성능예측을 위해 BEM의 접근 방법을 시도하였으며 범용 음향 소프트웨어인 Sys-noise 5.2의 direct collocation bem을 사용하여 반무한 평면 방음벽에 대한 해석을 수행하였으며, 그 결과를 검증하기 위해 Maekawa에 의한 근사해와 해석적 점근해에 비교하였다. 또한, 수음점이 방음벽으로부터 떨어진 거리, 방음벽의 폭, 방음벽의 높이에 따른 삽입손실을 계산하였고, 방음벽에 흡음처리를 한 경우와 방음벽상단의 형상변화에 따른 삽입손실의 변화를 계산하였다.

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트리플 덱 이론에 의한 경계층 해석 (II)

  • 서용권
    • Journal of the KSME
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    • v.27 no.6
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    • pp.515-521
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    • 1987
  • O(1)의 상하류지역에서 점근해를 가지고 $O(Re^{-3/8})$구역내에서 유동변화를 동반하는 유동문제는 트리플 덱(triple deck)을 적용하여 풀 수 있다. 예를 들면, 아주 완만한 모서리, 작은 돌출부(hump), 작은 구덩이(trough), 높이가 낮은 계단(step), 디퓨우저(diffuser)등과 같이 국소적으로 $O(Re^{-5/8})$규모의 기하학적 변화를 가지는 평판위의 유동문제등이다. 이하, 수치계산결과를 바탕으로 각종 유동문제에 대한 적용예를 살펴보기로 한다.

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The Effect of the Second-Order Approximation on Chaotic Responses (이차근사가 혼돈응답에 미치는 영향)

  • 이원경;박해동
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 1994.04a
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    • pp.134-147
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    • 1994
  • 고차근사가 혼돈응답에 미치는 영향을 조사하기 위하여 비선형문제의 전형인 탄성진자계를 집중적으로 조사하였다. 조화가진력을 가진 탄성진자계는 비자율계(원래계)로 나타나는데 다중시간법을 사용하여 이 계를 이차근사에 의한 자율계 (근사화계)로 변환하였다. 점근해의 초기조건에 대한 민감도의 척도인 Lyapunov 지수를 통하여 비교해 본 결과, 이차근사에 의한 근사화계가 일차근사에 의한 근사화계보다 원래계를 더 잘 반영하고 있음을 확인하였다. 이로써 고차근사가 정상상태 주기응답 뿐만 아니라 혼돈응답을 더 정확하게 예측하는 데도 유용함을 알 수 있었다.

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A Study on the Cartesian Boundary Condition of curved Walls in Computational Aeroacoustics Scheme (전산공력음향학에서 직교좌표를 이용한 곡면에서의 경계조건에 대한 고찰)

  • Bin Jonghoon;Cheong Cheolung;Lee Soogab
    • Proceedings of the Acoustical Society of Korea Conference
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    • spring
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    • pp.299-302
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    • 2000
  • 본 연구에서는 원형실린더에 의한 음향파의 산란현상을 전산공력음향학 기법을 이용하여 계산하였다. 특히 전산공력음항학에서 정확도를 위해 요구되는 좌표의 직교성을 유지하기 위해서 그에 대한 적절한 관계식을 유도하였으며 정확성의 검증을 위해서 수치적인 해를 이론적인 해와 비교, 분석하였다. 공간차분법으로는 Taylor 전개를 통하여 차 정확도를 가진 차분법을 바탕으로 주파수 공간에서 최적화 된 DRP(Dispersion Relation Preserving) 기법을 사용하였으며, 시간차분법으로는 Adams-Bashford 방법을 기준으로 최적화된 4단계 외재적(explicit) 적분방법을 사용하였다 벽면 경계조건으로는 가상점 개념을 이용한 경계조건을 사용하였으며 원방 경계조건으로서는 선형화 된 Euler 방정식의 점근해(Asymptotic Solution)을 이용한 방사경계조건(Radiation Boundary Condition)을 사용하였다.

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Induced steady flow around two oscillating circular cylinders (저동하는 두 원통둘레의 정상류에 관한 연구)

  • Suh, Y. K.
    • Journal of Ocean Engineering and Technology
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    • v.1 no.1
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    • pp.65-72
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    • 1987
  • 두개의 동일한 원통이 두중심점을 잇는 선에 대하여 수직인 방향으로 저동할때 발생되는 정상류에 대한 해를 구하였다. 관련된 자변수들간의 어떤 가정하에서 본문제는 Stokes문제가 될 수 있었다. 유동함수를 급수전개하였으며, 급수의 계수수함수는 penta-diagonal matrix를 풀어 구할 수 있었다. 해의 결과에 의하면 원통 주위에 몇개의 소용돌이가 생겼며 그소용돌이의 수는 두 원통간의 거리에 따라 달라 졌다. 두 원통간의 거리가 커짐에 따른 점근적 성질을 단일 원통의 경우와 비교하여 확인하였다.

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Diffraction of Electromagnetic Waves by Right Angle Dielectric Wedge (직각 쐐기형 유전분에 의한 전자파 회절)

  • Ju, Chang-Seong;Ra, Jeong-Ung;Sin, Sang-Yeong
    • Journal of the Korean Institute of Telematics and Electronics
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    • v.18 no.5
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    • pp.35-45
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    • 1981
  • An asymptotic solution of electromagnetic waves scattered by a right-angled dielectric wedge for plane wave incidence is obtained. Scattered fields are constructed by waves reflected and refracted from dielectric interfaces (geometric-optical fields) and a cylindrical wave diffracted from the edge. The edge diffracted field is obtained by adding a correction to the edge diffraction of physical optics approximation, where the correction field is calculated by solving a dual series equation amenable to simple numerical calculation. Validity of this result is assured by two limits of relative dielectric constant $\varepsilon$ of the wedge. The total asymptotic field calculated results in a Rawlins' Neumann series solution for small $\varepsilon$, and the edge diffraction pattern is shown to approach that of a perfectly conducting wedge for large $\varepsilon$. Calculated field patterns are presented and the accuracy of physical optics approximation is discussed.

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A Boundary-layer Stress Analysis of Laminated Composite Beams via a Computational Asymptotic Method and Papkovich-Fadle Eigenvector (전산점근해석기법과 고유벡터를 이용한 복합재료 보의 경계층 응력 해석)

  • Sin-Ho Kim;Jun-Sik Kim
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.37 no.1
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    • pp.41-47
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    • 2024
  • This paper utilizes computational asymptotic analysis to compute the boundary layer solution for composite beams and validates the findings through a comparison with ANSYS results. The boundary layer solution, presented as a sum of the interior solution and pure boundary layer effects, necessitates a mathematically rigorous formalization for both interior and boundary layer aspects. Computational asymptotic analysis emerges as a robust technique for addressing such problems. However, the challenge lies in connecting the boundary layer and interior solutions. In this study, we systematically separate the principles of virtual work and the principles of Saint-Venant to tackle internal and boundary layer issues. The boundary layer solution is articulated by calculating the Papkovich-Fadle eigenfunctions, representing them as linear combinations of real and imaginary vectors. To address warping functions in the interior solutions, we employed a least squares method. The computed solutions exhibit excellent agreement with 2D finite element analysis results, both quantitatively and qualitatively. This validates the effectiveness and accuracy of the proposed approach in capturing the behavior of composite beams.

Buoyant Slot Jets in Flowing Environment (가로흐름에 방류(放流)되는 평면부력(平面浮力)?)

  • Yoon, Tae Hoon;Han, Woon Woo
    • KSCE Journal of Civil and Environmental Engineering Research
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    • v.8 no.3
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    • pp.53-60
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    • 1988
  • The behavior of plane buoyant jet issuing vertically upwards into cross flow is analysed by experiments and integral scheme. The integral scheme is based on the self similarity and characteristic length scales to governing equations of continuity, momentum and constituent transport equation, in the horizontal and vertical flow region, respectively. Jet trajectories and the temperature distributions of jet centerlines obtained from experiments are analysed for various velocity ratios and densimetric Froude numbers. It was found that the analytical results about the trajectories and temperatures of jet center lines agree with the experiments and can be expressed as power laws.

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Non-Similarity Solution for Two-Dimensional Laminar Jet (이차원 층류제트를 위한 비 상사해)

  • 이상환
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.18 no.1
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    • pp.150-155
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    • 1994
  • An Approximate solution for plane two-dimensional incompressible laminar jet issuing from a finite opening with arbitrary initial profile into the same ambient fluid is proposed. For an arbitrary initial velocity profile, the problem is generated from the well known similarity solution for the jet of infinitesimal opening and provides good approximations in the region where the similarity solution cannot be used as an approximation. The asymptotic behavior of this solution is investigated and it is shown that, as goes downstream, the present solution approachs the similarity solution.