• Proceedings of the Acoustical Society of Korea Conference
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• 1996.06a
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• pp.45-50
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• 1996

천해에서 얻은 잔향음신호를 역추정 알고리즘으로 분석하여 자료수집 당시의 환경 변수인 해상풍의 세기와 해저면의 상태를 추정하는 방법에 대하여 기술하였다. 소오나 시스템과 잔향음신호 수집 당시의 환경 자료를 알고 있다면 음원에서 방사된 음파가 해수면에 처음 도달하는 시간과 수평입사각을 multipath eigenray model에 의해서 계산할 수 있고 이 정보를 이용하여 수신된 잔향음 신호를 분석하여 해수면에 의한 산란잔향음 준위와 시간을 계산할 수 있다. 해수면 후방산란강도는 수평입사각, 음원의 주파수, 해상풍의 세기 등에 의해 특징지어지며 계산된 잔향음 준위로부터 소오나 방정식을 이용하여 후방산란강도를 알아낼 수 있다. 이 후방산란강도를 입력자료로 하여 Method of Small Perturbation이론과 Chapman과 Harris가 유도한 실험식을 사용하여 입력된 값과 일치할 때까지 후방산란강도를 계산하여 이때의 환경변수를 찾아내었다. 한편 해저면 잔향음신호는 표준화된 후방산란강도값들의 PDF를 만들어 그 분포양상을 분석하였다. 본 논문에서 사용된 알고리즘의 검증을 위해서는 보다 다양한 환경하에서 실시된 많은 음향괸측자료를 필요로 한다.

• Journal of Industrial Technology
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• v.9
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• pp.79-85
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• 1989

In this paper, the static limit of Helmhortz equation is discussed in the analysis of acoustic wave scattering in a waveguide. Boundary integral equation method is used to formulate the scattering process in the exerior of the scatterer and finite element method in the interior of the scatterer. And hybrid Ray-Mode Method is used the provide the Green's function of the waveguide. The proposed algorithm is applied to a sample poblem with arbitrary scatterer in a waveguide. The results are compared with those of Laplace's equation which is the governing equation in the static problems.

• Proceedings of the KIEE Conference
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• 2007.07a
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• pp.961-964
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• 2007

본 논문에서는 FEM (Finite Element Method)을 이용한 압전세라믹의 특성해석을 통하여 잉크젯 프린트헤드를 설계, 제작하였다. 압전세라믹의 물질특성과 잉크유체 특성을 고려한 굽힘 모드방식의 구동원리와 이론정립을 하였다. 압전방정식은 압전구조에 의한 공진주파수로 압전 파라미터를 구할 수 있고, 실험을 통하여 이러한 측정값을 얻을 수 있었다. 제작된 압전세라믹 프린트헤드의 잉크드롭 실험결과 통하여 이에 대한 특성을 알 수 있었다. 이때 잉크유체의 음파와 압전 공진주파수 범위 내에서 압전세라믹 응력(변형)의 이득을 발생할 수 있음을 제작한 128노즐의 압전세라믹 잉크젯 프린트헤드로부터 알 수 있었다.

• The Journal of the Acoustical Society of Korea
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• v.23 no.8
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• pp.576-582
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• 2004

A computer code that is based on the Pseudo-spectral finite difference algorithm using staggered grid is developed for the wave propagation modeling in the time domain. The advantage of a finite difference approximation is that any geometrically complicated media can be modeled. Staggered grids are advantageous as it provides much more accuracy than using a regular grid. Pseudo-spectral methods are those that evaluate spatial derivatives by multiplying a wavenumber by the Fourier transform of a pressure wave-field and performing the inverse Fourier transform. This method is very stable and reduces memory and the number of computations. The synthetic results by this algorithm agree with the analytic solution in the infinite and half space. The time domain modeling was implemented in various models. such as half-space. Pekeris waveguide, and range dependent environment. The snapshots showing the total wave-field reveals the Propagation characteristic or the acoustic waves through the complex ocean environment.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.35 no.2
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• pp.94-100
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• 2007

An axisymmetric supersonic jet screech in the Mach number range from 1.07 to 1.2 is numerically simulated. The axisymmetric mode is the dominant screech mode for an axisymmetric jet. The Reynolds-averaged Navier-Stokes equations in the conjunction with a modified Spalart-Allmaras turbulence model are employed. A high resolution finite volume essentially non-oscillatory(ENO) schemes are used along with nonreflecting characteristic boundary conditions that are crucial to screech tone computations to accurately capture the sound waves, shock-cell structures and large-scale instability waves.

• The Journal of the Acoustical Society of Korea
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• v.20 no.4
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• pp.71-80
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• 2001

In order to consider the sediment layer's effect to total acoustic field, we composed a 3 layered fluid model of 2 sediment layers by adding an additional layer to the Pekeris model and found solutions by using Green's function, boundary conditions and Sommerfeld radiation condition. The modes were divided into discrete modes and virtual modes, and confirmed that the characteristic equation to find discrete modes was same as that of Tolstoy and Clay for normal modes. Also, we confirmed that under similar conditions the 3 layered model showed same results as that of Pekeris model. We believe this 3 layered model can be used to study the sediment's effect on the virtual mode of near field.

• Journal of the Society of Naval Architects of Korea
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• v.36 no.3
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• pp.29-40
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• 1999

A numerical method in frequency domain for the analysis of the acoustic wave equation governing the sound field generated by a non-cavitating propeller under a steady of unsteady loading condition is developed. Theory shows that only multiples of the blade passage frequency exist and that the wave number consists of the frequency component due to the nonuniformity of the wake and the Doppler effect originated from the rotation of the blades. Correlation with experiments for a two bladed propeller, designed to be load-free at a particular advance speed, indicate that the thickness effect can be significant in steady case, but can be negligible compared to the unsteady loading effect.

• The Journal of the Acoustical Society of Korea
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• v.13 no.2E
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• pp.83-91
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• 1994

Three components contribute to the acoustic field propagating in a wedge or over a ridge : a direct path arrival, an image component due to reflection from the boundaries and a component diffracted by the apex. All three contributions are included in a new, exact solution of the Helmholtz equation for the three-dimensional time harmonic field from a point source in a wedge(or over a ridge) formed by two intersecting, pressure-release plane boundaries. The solution is obtained by applying three integral transforms, and consists of and infinite sum of uncoupled normal nodes. The mode coefficients are given by a finite integral involving a Gegenbauer polynomial in the integrand, which may be computed relatively efficiently. Results of the theory for propagation over a 90 degree ridge is discussed.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2007.04a
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• pp.329-334
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• 2007

An axisymmetric supersonic jet screech in the Mach number range from 1.07 to 1.2 is numerically simulated. The axisymmetric mode is the dominant screech mode for an axisymmetric jet. The Reynolds-averaged Navier-Stokes equations in the conjunction with modified Spalart-Allmaras turbulence model are employed. A high resolution finite volume essentially non-oscillatory(ENO) schemes are used along with nonreflecting characteristic boundary conditions that are crucial to screech tone computations to accurately capture the sound waves, shock-cell structures, unsteady shock motions and large-scale instability waves.

• Journal of Korea Water Resources Association
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• v.39 no.12 s.173
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• pp.1023-1030
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• 2006

The characteristics of the longitudinal velocity in a $180^{\circ}$ constant-radius, recirculating laboratory channel were investigated. Three-dimensional velocity fields were measured using a side-looking ADV. The shortcomings of existing equations for longitudinal velocity are discussed. An eddy viscosity model is adopted in the downstream momentum equation. A mathematical equation was developed to describe the vertical distribution of longitudinal velocity. The comparisons of the longitudinal velocity show generally good agreement. It is found that the curvature change in the curved channel affects the vertical location of maximum velocity and the vertical profile of longitudinal velocity.