• 한국공작기계학회논문집
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• 제11권3호
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• pp.33-38
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• 2002

This paper deals with pressure ripple attenuation far separated-type Hydrostatic Transmission (HST) consisting ova variable axial piston pump connected in an open loop to a fried displacement axial piston motor. Pressure ripples in HST is major source of vibration which can lead to fatigue failure of components and cause noise. In order to reduce the pressure ripple, an annular tube tripe hydraulic filter is proposed to attenuate pressure ripples with the high frequencies components to achieve better noise reduction in HST. The basic principle of a hydraulic filter is allied to propagation of pressure wave, reflection, absorption in cross section of discontinuity and resonance in the hydraulic pipeline. It is experimentally shown that the hydraulic filter attenuates about 30∼40dB of pressure ripple with high frequencies. These results will assist in modeling and design of noise reduction in hydraulic control systems, and provide a means of designing a quieter HST.

• 한국공작기계학회:학술대회논문집
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• 한국공작기계학회 2003년도 춘계학술대회 논문집
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• pp.117-123
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• 2003

This paper deals with pressure ripple and noise reduction characteristics for a hydrostatic transmission(HST) consisting of a variable axial piston pump connected in an open loop to a fixed displacement axial piston motor. Pressure ripples in HST is major source of vibration, which can lead to fatigue failure of components and cause noise. In order to reduce the pressure ripple, an annular tube type hydraulic filter proposes to absorb pressure ripples with the high frequencies components to achieve better noise attenuation in HST. The basic principle tube is applied to propagation of pressure wave, reflection, absorption in cross section of discontinuity and resonance in the hydraulic pipeline. It is experimently confirmed that a hydraulic filter is absorbed to be about 30∼40dB of pressure ripple with high frequencies. These results will assist in modeling and design of noise reduction in hydraulic control systems, and here, should provide a means of designing a quieter HST.

• 한국음향학회지
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• 제23권8호
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• pp.576-582
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• 2004

본 논문에서는 시간영역에서 음파 전달 모델링을 위해 엇갈림 격자에서 유사 스펙트럴 유한 차분 알고리듬을 기반으로 한 전산조직을 개발하였다. 유한 차분 근사는 기하학적으로 복잡한 매질에서 모델링을 가능하게 하고, 엇갈림 격자는 정규 격자에 비해 훨씬 정확한 해를 제공한다. 유사 스펙트럴 방법은 파수 영역에서 파수에 음압의 푸리에 변환을 곱한 후 이를 역푸리에 변환하므로서 공간 도함수를 구하는 방법이다. 이 방법은 매우 안정적이며, 메모리와 계산시간을 감소시키는 장점을 지니고 있다. 무한 및 반무한 영역에서 이 알고리듬에 의한 결과가 해석해와 잘 일치함을 확인하였고, 무한영역과 Pekeris도파관, 거리종속 해양환경에서 시간영역 모델링을 수행하여 스냅사진을 얻어내었으며 이 스냅사진을 통해 복잡한 해양환경에서 신호의 전파 양상을 파악할 수 있었다.

• 한국추진공학회지
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• 제7권3호
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• pp.15-21
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• 2003

본 연구에서는 다공관의 출구로부터 전파하는 충격성 소음의 전파특성을 실험적으로 파악하였다. 다공관은 공극율, 구멍지름 그리고 관의 길이를 각기 다르게 제작하여 충격파 관 출구에 부착하여 실험하였다. 충격파 전파마하수는 실제의 적용조건을 참고하여 1.02-1.2의 범위로 하였다. 지향성은 근음장과 원음장으로 구분하여 측정하였다. 또한 충격성 소음원인 펄스파의 전파과정을 조사하기 위하여 쉴리렌 광학장치를 이용하였다. 실험결과로부터 다공관의 소음저감 성능은 음장조건에 좌우됨을 알았다. 즉 근음장 조건에서는 다공관의 공극율과 관의 길이가 소음저감에 다소간의 영향을 미치지만, 원음장 조건에서는 다공관이 충격성 소음의 저감에 거의 기여하지 못하였다. 이와 같이 음장조건에 따라 충격성 소음의 저감성능이 다르게 되는 것은 근음장 조건에서는 관축방항으로 강한 지향성을 보이지만, 원음장 조건에서는 모든 방향으로 같은 세기로 전파하는 무지향성이기 때문이다.

• 비파괴검사학회지
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• 제30권6호
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• pp.578-586
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• 2010

This paper describes a theoretical model and acoustic analysis of hysteresis of contacting surfaces subject to compression pressure. Contacting surfaces known to be nonlinear and hysteretic is considered as a simple spring that has a complex stiffness connecting discontinuous displacements between two solid contact boundaries. Mathematical formulation for 1-D interfacial wave propagation between two contacting solids is developed using the complex spring model to derive the dispersion relation between the interface wave speed and the complex interfacial stiffness. Existence of the interface wave propagating along the hysteretic interface is studied in theory and discussed by investigating the solution to the dispersion equation. Unlike the linear interface without hysteresis, there can exist only one distinct mode of interface waves for the hysteretic interface, which is anti-symmetric motion. The anti-symmetric mode of interface wave propagates with the velocity faster than the Rayleigh surface wave but less than the shear wave depending on the interfacial stiffness. If the contacting surfaces are compressed so much that the linear interfacial stiffness is very high, the hysteretic stiffness does not affect the interface wave velocity. However, it has an effect on the speed of interface wave for a loosely contact surfaces with a relatively low linear stiffness. It is also found that the phase velocity of anti-symmetric wave mode converges to the shear wave velocity in despite of the linear stiffness value if the hysteretic stiffness approaches 0.5.

• 한국가시화정보학회지
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• 제16권3호
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• pp.8-15
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• 2018

Recently, as the high speed railway becomes more common, new environmental problems such as noise around tunnels are appearing. When a high speed train enters a tunnel, a compression wave in the tunnel is generated and propagated toward the tunnel exit at a sonic speed. When it reaches the tunnel exit, a part of compression wave radiates as a pulse typed impulse wave to the outside of tunnel. The impulse wave has an explosive noise. When the impulse wave is propagated around a village, it induces a serious noise or other problems to the resident. In order to solve these engineering problems, it is important to investigate the radiation characteristics of the impulse wave radiated from the tunnel exit. In this study, the effect of the length and angle of the baffle plate at the tunnel exit on the impulse wave radiated from the tunnel exit was investigated by numerical analysis. As a results, the baffle plate greatly affected the propagation of impulse wave.

• 대한기계학회논문집B
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• 제31권1호
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• pp.51-61
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• 2007

This paper presents numerical and theoretical studies of acoustic wave interactions in slightly compressible liquids within piezoelectrically driven inkjet print heads. The interconnected flow channels may cause jet crosstalk, resulting in poor printing quality. It should be reduced by modifying the channel structure with the acoustic wave interactions considered. Compressible gas flow driven by the sudden movement of a top wall in the channel is calculated using Flow3D and is validated with the narrow gap theory. Limited compressibility model of the Flow3D is employed to calculate pressure waves of slightly compressible ink flow. It is found that reducing restrictor width can damp out the jet crosstalk by inhibiting the pressure wave propagation. The degree of crosstalk has been quantified using the maximum values of cross-correlations between neighboring channels and a critical channel dimension for acceptable crosstalk has been proposed. This finding is verified by drop visualization experiments using silicon-micromachined piezo inkjet print heads that are fabricated by our group.

• 한국추진공학회지
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• 제15권6호
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• pp.1-6
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• 2011

본 연구에서는 정상초음파장의 간섭에 의해 야기되는 예혼합화염의 구조 변이를 규명하기 위한 실험 결과를 제시한다. 화염전파를 관찰하기 위해 슐리렌 기법을 이용하였으며, 초기압력 및 연소챔버 개방 유무에 따른 화염선단의 형태 및 화염 전파속도를 고찰하였다. 정상초음파장에 의한 화염선단의 찌그러짐이 관찰되었고, 초음파장의 특성이 변하지 않는 한 그 수직방향으로의 위치는 일정하였다. 정상초음파의 영향을 받은 화염은 전파할수록 구조적 변화가 심해졌으며, 전파속도 또한 증가하였다. 반사파와 정상초음파의 영향으로 연꽃모양의 화염(lotus flame)이 형성되는 사실을 발견할 수 있었다.

• 비파괴검사학회지
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• 제33권3호
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• pp.276-282
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• 2013

This paper proposes an ultrasonic method for measurement of linear and hysteretic interfacial stiffness of contacting surfaces between two steel plates subjected to nominal compression pressure. Interfacial stiffness was evaluated by the reflection and transmission coefficients obtained from three consecutive reflection waves from solid-solid surface using the shear wave. A nonlinear hysteretic spring model was proposed and used to define the quantitative interfacial stiffness of interface with the reflection and transmission coefficients. Acoustic model for 1-D wave propagation across interfaces is developed to formulate the reflection and transmission waves and to determine the linear and nonlinear hysteretic interfacial stiffness. Two identical plates are put together to form a contacting surface and pressed by bolt-fastening to measure interfacial stiffness at different states of contact pressure. It is found from experiment that the linear and hysteretic interfacial stiffness are successfully determined by the reflection and transmission coefficient at the contact surfaces through ultrasonic pulse-echo measurement.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2003년도 유체기계 연구개발 발표회 논문집
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• pp.671-677
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• 2003

Two-dimensional direct numerical simulation of the edge-tones by the finite difference lattice Boltzmann method (FDLBM) is presented. We use a new lattice BGK compressible fluid model that has an additional term and allow larger time increment comparing the conventional FDLBM, and also use a boundary fitted coordinates. We have succeeded in capturing very small pressure fluctuations result from periodically oscillation of jet around the edge. That pressure fluctuations propagate with the sound speed. It is clarified that the sound wave generated in rather wide region and individual vortices do not affect the sound wave propagation.