• 한국음향학회지
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• 제19권2호
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• pp.54-60
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• 2000

어레이를 이용한 음원 탐지는 음원의 모델을 가정하고 있다. 원거리 음원의 경우에는 평면파 모델을 적용하여 널리 적용되고 있으나, 근거리 음원의 경우에는 단극 음원을 가정한 음원 탐지법이 시도되고 있는 상황이다. 이 논문에서는 보다 효과적인 근거리 음원 추정을 위해 쌍극 음원 모델과, 삼극 음원 모델을 유도하여 MUSIC 방법에 적용할 수 있는 주사벡터(scan vector)를 제안하였다. 제안된 삼극 음원 모델의 경우, 실제 음원이 순수 쌍극 음원인 경우에 음원 탐지 성능이 다소 떨어지나, 단극 및 사극 음원이거나, 이들의 조합에 의한 음원이거나에 관계 없이 적용 가능함을 알 수 있었다. 따라서 일반적인 음원 탐지에 활용할 수 있는 효과적인 음원 모델임을 알 수 있었다.

• 지구물리와물리탐사
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• 제12권1호
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• pp.143-153
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• 2009

LWD 다극자 송신원을 구성하는 각 단극자 송신원들 사이에 진폭 또는 신호발생 시간에서 불일치가 발생할 경우 LWD 검층자료에 미치는 영향에 대해 이산파수법을 사용하여 조사하였다. 진폭-불일치 LWD 쌍극자/사극자 송신원은 굽힘 모드(flexural mode)/스크류 모드(screw mode) 이외에도 다른 모드들을 생성한다. 이들 중 가장 진폭이 큰 것은 스톤리 모드(Stoneley mode)이며 불일치 정도가 커질수록 진폭이 증가한다. 하지만 A-C 자료처리를 통해 굽힘 모드를 A-B+C-D 자료처리를 통해 스크류 모드를 각각 추출할 수 있다. 이는 LWD 검층기가 시추공의 중심에 위치해 있는 한 시추공축으로부터 같은 거리에서 같은 진폭을 갖는 스톤리 모드가 A-C와 A-B+C-D 자료처리 과정을 통해 제거되기 때문이다. 신호발생시간-불일치 LWD 다극자 송신원으로부터의 반응들은 마치 시추공 중심으로부터 벗어나서 위치한 두 개 또는 네 개의 단극자 송신원들로부터의 반응들의 합처럼 보인다. 그러나 모드들의 도착시간들과는 무관한 주파수영역 셈블란스 플랏(semblance plot)의 분산곡선들을 참조하면 매질의 속도에 대한 잘못된 해석을 피할 수 있다.

• Journal of Advanced Marine Engineering and Technology
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• 제33권8호
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• pp.1170-1179
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• 2009

본 연구의 목적은 수평축 풍력터빈인 NREL Phase VI를 대상으로 ANSYS FLUENT에서 제공하는 LES와 FW-H 상사식을 이용하여 풍력발전기로부터 방사되는 저주파 공력소음을 수치적으로 예측하는 것이다. 풍력발전기 공력소음에 관한 어떠한 실험적 자료가 존재하지 않으므로, 먼저 정격풍속에서 토크와 출력 등의 공력성능 수치결과를 실험결과와 비교하여 소음원 예측의 타당성을 검증한 후, 풍속 변화에 따른 공력소음 특성을 분석하였다. 그 결과 수치성능결과는 약0.8%이내에서 실험결과와 잘 일치하였다. 풍속이 증가함에 따라 사극자와 이극자에 의한 총음압레벨은 증가하는 경향을 나타내었다. 또한 풍력터빈 허브중심으로부터 거리가 증가함에 따라 원방에서는 $r^{-1}$, 근방에서는 $r^{-2}$에 비례하여 증가하는 것으로 나타났다. 그리고 거리가 두배 증가함에 따른 총음압레벨은 약 6dB 감소하였다.

• 한국지구물리탐사학회:학술대회논문집
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• 한국지구물리탐사학회 2003년도 Proceedings of the international symposium on the fusion technology
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• pp.313-320
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• 2003

Synthetic seismograms recorded with a logging-while-drilling (LWD) tool in the presence of slow formation are computed by the discrete wavenumber method. Monopole, dipole, and quadrupole logging tools are simulated with a source center frequency of 4 kHz. The modes in the responses are identified and characterized with time and frequency semblance plots. Numerical results show that, to obtain the formation shear velocity, we need to correct the peak velocities of the multipole modes in the semblance plots by using analytical dispersion curves.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2003년도 추계학술대회
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• pp.810-815
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• 2003

Flow-induced noise propagated from flow over a sphere is numerically investigated for laminar flow at Re = 300 and 425, and for turbulent flow at Re = 3700 and $10^4$, where the Reynolds number is based on the freestream velocity and the sphere diameter. The numerical method used for obtaining the flow over a sphere is based on an immersed boundary method in a cylindrical coordinate system. The Curle’s solutions of the Lighthill’s acoustic analogy with and without the far-field and compact-source approximation are used in order to investigate the noise field from flow over a sphere. Since the drag and lift forces change irregularly in time at Re = 425, 3700 and $10^{4}$, the noise propagates in a complicated manner. At Re = 300, 425 and $10^{4}$, the noise from dipole sources is much larger than that from quadrupole sources. On the other hand, at Re = 3700, the quadrupole source becomes dominant. The temporal variation of the flow-induced noise around a sphere is obtained at some observation points, which shows that the peak frequency corresponds to the Strouhal number associated with the wake instability.

• 한국신재생에너지학회:학술대회논문집
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• 한국신재생에너지학회 2009년도 춘계학술대회 논문집
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• pp.504-507
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• 2009

The purpose of this work is to predict the low frequency aero-acoustic noise generated from the horizontal axis wind turbine, NREL Phase VI using large eddy simulation and Ffowcs-Williams and Hawkings model provided in the commercial code, FLUENT. Calculated aerodynamic performances such as shaft torque and power are compared with experimentally measured value. Performance results show a good agreement with experimental data within about 0.8%. If the distance by two times is changed from 32D to 64D toward the downstream region, sound pressure level is reduced by about 6.4dB.

• 한국음향학회:학술대회논문집
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• 한국음향학회 2002년도 하계학술발표대회 논문집 제21권 1호
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• pp.469-474
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• 2002

In recent years, modularization of engine parts has increased the application of plastic products in air intake systems. Plastic intake manifolds provide many advantages including reduced weight, contracted cost, and lower intake air temperatures. These manifolds, however, have some weakness when compared with customary aluminium intake manifolds, in that they have low sound transmission loss because of their lower material density. This low transmission loss of plastic intake manifolds causes several problems related to flow noise, especially when the throttle is opened quickly. The physical processes, responsible for this flow noise, include turbulent fluid motion and relative motion of the throttle to the airflow. The former is generated by high-speed airflow in the splits between the throttle valve and the inner-surface of the throttle body and surge-tank, which can be categorized into the quadrupole source. The latter induces the unsteady force on the flow, which can be classified into the dipole source. In this paper, the mechanism of noise generation from the turbulence is only investigated as a preliminary study. Stochastic noise source synthesis method is adopted for the analysis of turbulence-induced, i.e. quadrupole noise by throttle at quick opening state. The method consists of three procedures. The first step corresponds to the preliminary time-averaged Navier-Stokes computation with a $k-\varepsilon$ turbulence model providing mean flow field characteristics. The second step is the synthesis of time-dependent turbulent velocity field associated with quadrupole noise sources. The final step is devoted to the determination of acoustic source terms associated with turbulent velocity. For the first step, we used market available analysis tools such as STAR-CD, the trade names of fluid analysis tools available on the market. The steady state flows at three open angle of throttle valve, i.e. 20, 35 and 60 degree, are numerically analyzed. Then, time-dependent turbulent velocity fields are produced by using the stochastic model and the flow analysis results. Using this turbulent velocity field, the turbulence-originated noise sources, i.e. the self-noise and shear-noise sources are synthesized. Based on these numerical results, it is found that the origin of the turbulent flow and noise might be attributed to the process of formulation and the interaction of two vortex lines formed in the downstream of the throttle valve. These vortex lines are produced by the non-uniform splits between the throttle valve and inner cylinder surface. Based on the analysis, we present the low-noise design of the inner geometry of throttle body.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2007년도 추계학술대회논문집
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• pp.1490-1493
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• 2007

Aerodynamic noise generated from wind turbines is predicted by it's classified source mechanisms using computational method. BPF noise according to the blade passing motion, is modelled on monopole and dipole sources. They are predicted by Farassat 1A equation. Airfoil self noise and turbulence ingestion noise are modelled upon quadrupole sources and are predicted by semi-empirical formulas composed on the groundwork of Brooks et al. and Lowson. Retarded time is considered, not only in low frequency noise prediction but also in turbulence ingestion noise and airfoil self noise prediction. Wind turbine noise emission of a 3MW wind turbine and a 600 kW wind turbine, standing for large and middle sized wind turbines, is analyzed.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 1997년도 춘계학술대회논문집; 경주코오롱호텔; 22-23 May 1997
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• pp.636-642
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• 1997

Laminar vortex shedding behind a circular cylinder with and without splitter plates attached to the circular cylinder at low Reynolds numbers are simulated by solving the unsteady incompressible Navier-Strokes equations. The Strouhal number, lift and drag rapidly change with the splitter plate. Far-field noise from the vortex shedding behind the cylinder is computed using the Lighthill acoustic analogy and the Curle's solution for the Lighthill equation. The acoustic source functions are obtained from the computed near-field velocity and pressure. Numerical results show that the volume quadrupole noise is small at low Mach numbers, compared with the surface dipole noise. Also the amplitude and frequency of the acoustic density fluctuations are varied with the length of splitter plates. The scattering effects at the edge of a splitter plate are considered by using the half-plane Green's function.

• Journal of Mechanical Science and Technology
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• 제20권12호
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• pp.2292-2314
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• 2006

Efficient numerical method is developed for the prediction of aerodynamic noise generation and propagation in low Mach number flows such as aeolian tone noise. The proposed numerical method is based on acoustic/viscous splitting techniques of which acoustic solvers use simplified linearised Euler equations, full linearised Euler equations and nonlinear perturbation equations as acoustic governing equations. All of acoustic equations are forced with immersed surface dipole model which is developed for the efficient computation of aerodynamic noise generation and propagation in low Mach number flows in which dipole source, originating from unsteady pressure fluctuation on a solid surface, is known to be more efficient than quadrupole sources. Multi-scale overset grid technique is also utilized to resolve the complex geometries. Initially, aeolian tone from single cylinder is considered to examine the effects that the immersed surface dipole models combined with the different acoustic governing equations have on the overall accuracy of the method. Then, the current numerical method is applied to the simulation of the aeolian tones from twin cylinders aligned perpendicularly to the mean flow and separated 3 diameters between their centers. In this configuration, symmetric vortices are shed from twin cylinders, which leads to the anti-phase of the lift dipoles and the in-phase of the drag dipoles. Due to these phase differences, the directivity of the fluctuating pressure from the lift dipoles shows the comparable magnitude with that from the drag dipoles at 10 diameters apart from the origin. However, the directivity at 100 diameters shows that the lift-dipole originated noise has larger magnitude than, but still comparable to, that of the drag-dipole one. Comparison of the numerical results with and without mean flow effects on the acoustic wave emphasizes the effects of the sheared background flows around the cylinders on the propagating acoustic waves, which is not generally considered by the classic acoustic analogy methods. Through the comparison of the results using the immersed surface dipole models with those using point sources, it is demonstrated that the current methods can allow for the complex interactions between the acoustic wave and the solid wall and the effects of the mean flow on the acoustic waves.