• 한국음향학회지
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• 제16권5호
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• pp.60-67
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• 1997

서기 771년(신라, 혜공왕 7년)에 주조된 성덕 대왕 신종은 지면으로부터 약 50cm 떨어지게 설치되어 있으며 지면에 울림통을 가지고 있다. 이 울림통은 일종의 공명기의 역할을 하여 종 내부와 함께 성덕 대왕 신종의 고유한 소리 특성에 영향을 줄 것이라 예측되어 왔다.[1, 2, 3]. 본 논문에서는 이를 규명하기 위한 내부 음장의 3차원 측정 실험을 소개하고 있으며 울림통이 종소리에 끼치는 영향을 단순하나 물리적 현상을 대표하는 모델을 이용하여 설명하고 있다. 이러한 해석 방법을 기초로 하여 새로운 울림통의 크기를 제안하고 있다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2013년도 추계학술대회 논문집
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• pp.374-379
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• 2013

Helmholtz resonators have high transmission loss in a narrow band at the resonance frequency. The transmission loss characteristics of resonators at high sound pressure levels can change due to variations of the impedance as a result of nonlinear behavior. Different sound pressure levels are applied to each resonator when resonators were arranged along the path. Therefore, impedance variation due to incident sound pressure level should be considered in order to predict the transmission loss.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2005년도 춘계학술대회논문집
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• pp.521-524
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• 2005

To protect a satellite and electronic equipment from the acoustic loads generated by rocket propulsion system, many launch vehicle use acoustic blanket. Most high frequency region of the acoustic loads is reduced by nose fairing skins and acoustic barrier, but low frequency region is not. In order to control low frequency acoustic mode, we designed away resonator panel which was made of composite materials. This paper shows the absorption coefficient measurement result of resonator and SPL(Sound Pressure Level) reduction by using resonators in a rectangular cavity for experiment. Proper arrangement of acoustic resonators at each mode reduce effectively SPL around the satellite through changing boundary condition.

• 동력기계공학회지
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• 제12권4호
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• pp.46-51
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• 2008

Honeycomb panel has a constructive advantage because it is constructed with a honeycomb core, so it has relatively higher strength ratio to weight. Therefore honeycomb panel has been used as the light weight panels in the high-speed railway technology and high-speed ship like as cruise yachts. Also it has been used in the aircraft and aerospace industry as a structural panel because light weight structure is indispensible in that field of industry. Recently, the honeycomb panel is embossed in the viewpoints of high oil prices as the lightweight panel of the transport machine, however the sound insulation capacity of the honeycomb panel is poorer than those of uniform and another sandwich panels. In this paper a method to improving the sound absorption coefficient of a honeycomb panel Is studied by using the Helmholtz resonator. The sound absorption coefficients for some kinds of honeycomb cores are demonstrated by the normal incident absorption coefficient method.

• 한국음향학회지
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• 제37권5호
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• pp.276-283
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• 2018

이 연구는 헬름홀쯔 공명기 구조를 갖는 매미 소리의 중심주파수에 주요 영향을 주는 발음기관이 무엇인지를 최초로 초고속영상분석을 통해 규명하는 데 목적이 있다. 말매미와 참매미를 대상으로 소리를 녹음 후 분석하였고, 초고속카메라로 촬영한 진동막의 움직임을 분석하여 소리의 주파수와 진동막 운동 사이의 관계를 비교하였다. 연구결과, 말매미와 참매미 모두 유인음과 비명음의 주파수분포에는 차이가 거의 없었으며, 말매미의 진동막은 3개, 참매미의 진동막은 1개 모드로 진동하였다. 두 매미 모두 양쪽 진동막의 진동수에는 차이가 나타나지 않았으며, 말매미의 진동막의 3개 진동 모드는 서로 다른 진동수 대역의 소리가 발생하였다. 두 매미 모두 진동막의 진동수 대역과 유인음의 중심주파수 대역이 매우 유사하였다. 결론적으로, 헬름홀쯔 공명기 구조를 갖는 매미 소리의 주파수는 복부의 공명조건보다는 진동막의 모드별 진동수에 의해 결정되는 것으로 추정된다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2000년도 춘계학술대회논문집
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• pp.785-790
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• 2000

The resonant frequency of a gas-filled cylindrical Helmholtz resonator in a liquid is obtained analytically. The equation of motion of the resonator is derived by using the condition of equilibrium of forces acting on the mass in the neck of the resonator. The reaction force on the upper side of the cylinder due to the acceleration of external fluid and sound radiation is obtained by using the analytical results for the baffled circular-piston problem. From the frequency response function of the resonator, a formula to predict the resonant frequency of the resonator is derived. It is shown that the resonant frequency of the Helmholtz resonator significantly decreases due to the cushioning effect of gas inside the cavity. Therefore, when a pressure transducer is to be installed in a pin-hole type mounting method, much care should be paid to remove the gas from the cavity.

• 한국항공우주학회지
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• 제38권10호
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• pp.966-972
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• 2010

본 연구에서는 연소불안정 현상을 제어하는 수동적 기구의 하나인 음향공을 적용하여, 음향공의 설계 변수(오리피스 길이와 지름)와 가진 음압에 따른 감쇠 효과를 선형음향해석과 상온 음향시험을 통하여 연구하였다. 오리피스의 길이가 짧고, 지름이 클수록 감쇠효과가 증가하는 것을 확인하였으며 실험과 선형 음향 해석 결과가 서로 동일한 경향을 보이는 것을 확인하였다. 또한, 가진 음압의 크기가 110 dB 이상에서 감쇠 능력이 비선형적으로 감소하는 것을 확인하였으며, 음향공 오리피스의 단면적이 증가할수록 감소량이 감소하는 것으로부터 비선형 구간에서는 오리피스 단면적을 증가시키는 것이 유리함을 확인하였다.

• 한국분무공학회지
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• 제4권3호
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• pp.32-41
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• 1999

In this research, internal-mixing twin-fluid atomizer using sonic energy is designed and manufactured. We are trying to intimate high efficiency twin-fluid atomizer to obtain good liquid atomization in the low pressure region. Define of geometric form of atomizer, characteristics of spray is influenced by position, depth and height variation of cavity resonator, variation of sound intensity and resonant sound frequency with liquid flow rate. The liquid atomization is promoted by multi-stage disintegration of mixing flow of gas with liquid and the optimum condition of position and depth of cavity resonator according to sonic energy is obtained from the condition at a=2.5mm and L=2mm. The velocity distribution of droplets shows negative value due to recirculation region at the center of axial, and as the radial direction distance is far, the velocity distribution of droplets decrease slowly after having a maximum value. However velocity and SMD show nearly uniform distribution at the down stream and as result compared to Nukiyama and Tanasawa's equation. atomization of mixing flow with air and liquid dispersing from the outlet of the nozzle is promoted by the effect of collision at the cavity resonator.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2005년도 추계학술대회논문집
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• pp.196-199
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• 2005

Flow traveling over a cavity opening forms a vortex due to unstable shear layer and induces an aerodynamic pressure excitation from the diffusion of the vortex convecting out of the trailing edge of the opening. The interaction between the excitation force and the cavity response sustains resonance in the resonator(cavity) and locked-in vortex shedding at the leading edge of the opening. The aerodynamic excitation force can be described from the diffusion of the vortex over the trailing edge and the level of its diffusivity is related to the strength of vorticity seeded at the loading edge. In this study, the control scheme of the internal pressure oscillation was proposed from regulating the vorticity at the leading edge by use of an oscillating spoiler. It was found that the relative motion between the spoiler and the air mass at the cavity opening influenced vorticity strength and the control was achieved by direct feedback of the cavity pressure fluctuation to the actuator.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 추계학술대회논문집B
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• pp.757-763
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• 2000

In vehicle exhaust systems the sound attenuation and the reduction of flow losses are often two competing demands. The present study considers a fully vehicle exhaust system and investigates experimentally both the sound attenuation and the flow performance of production configurations including the catalyst, the resonator, and the muffler. Dynamometer experiments have been This study is on the development of a new muffler composed of a valve system using an elasticity of spring. The valve system conducted with the daewoo 1500cc Lanos engine with speeds ranging from 1000 to 5000 rpm. Measurements include the flow rates, the temperatures and the absolute dynamic pressures of the hot exhaust gases at point locations. The present study describes the experimental aspects of an ongoing effort to validate and use the nonlinear fluid dynamic models in the time-domain for the prediction of the acoustic and power performance of firing internal combustion engines with full production exhaust systems.