• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2007.04a
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• pp.295-298
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• 2007

The effectiveness of passive control techniques for reducing the pressure oscillation generated in a supersonic cavity flow was investigated numerically and experimentally, respectively. The control device includes a sub-cavity installed in the upstream edge of a rectangular cavity. Time-dependent supersonic cavity flow characteristics with turbulent features were examined by using the three-dimensional, mass-averaged Navier-Stokes computation based on a finite volume scheme and large eddy simulation. The results show that the pressure oscillation near the trailing edge dominates overall time-dependent cavity pressure variations. Such an oscillation can be attenuated more significantly in the presence of the sub-cavity compared with the cavity without sub-cavity, and a larger sub-cavity leads to better control performance.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2010.05a
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• pp.84-85
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• 2010

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2009.11a
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• pp.359-362
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• 2009

Damping characteristics of pressure oscillation induced by an orifice in fluid feeding line for are investigated numerically and experimentally. Assuming small pressure oscillation, acoustic damping effect of orifice is confirmed experimentally, and with the mean flow, damping characteristics of an orifice are investigated numerically. When an orifice is installed at the node of pressure oscillation corresponding to the anti-node of velocity oscillation, suppression of pressure oscillation is maximized and with the mean flow, the resonant frequency is decreased. And, it is found that the optimal position of an orifice for damping shouled be changed.

• Journal of the Korean Society of Propulsion Engineers
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• v.20 no.5
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• pp.77-83
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• 2016

A considerable amount of researches has been performed to investigate the flow characteristics produced in the cavity system over straight wall. However, many practical applications of the cavity flows are found on curved walls, which are strongly subject to the centrifugal force effects. No work has been made on the cavity flows on the curved wall to date. In the present study, a computational fluid dynamics method has been applied to investigate the cavity flows over curved walls at Mach numbers in range of 0.4 to 0.8. The aspect ratio of the cavity was fixed at L/H=3, but the radius of curvature of the curved wall is changed in considering the real engineering practice. The results reveal that the pressure oscillations in the curved walls are stronger than those in the straight wall. It is found that the ratio of curvature of the curved wall significantly affects the unsteady flow characteristics inside the cavity.

• Journal of KSNVE
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• v.21 no.4
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• pp.13-17
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• 2011

• Journal of KSNVE
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• v.1 no.2
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• pp.95-101
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• 1991

가전제품의 고부가가치를 위해서는 제품의 기본성능 충실화와 함께 소음진동 의 발생을 최대한 억제하여야 한다. 소음진동의 제어는 소음진동을 일으키는 원인에 대한 특성을 파악하고 최적의 소음진동방지 대책을 제시함으로서 효과를 얻을 수 있다. 국내의 가전 3사와 학계는 산학협동연구를 통한 제품의 고부가가치화를 위한 소음진동 제어 연구 활동이 활발히 진행되고 있으며, 본 글에서는 가전제품중 다양한 소음 특성을 갖고 있는 냉장고의 경우 진동에 의한 소음 제어 방법으로 진동 전달 특성 변경이 유효한 방법임을 제시 하고자 한다. 가전제품의 소음진동의 발생은 주로 홴등에 의한 유체유동 소음특성과 기계 구조물의 진동에 의한 소음 특성을 모두 갖는 냉장고에 대하여 알아보았다. 연구방법으로 Sound Intensity법과 가속도 측정법을 이용하여 진동의 전달 경로를 파악하고 냉장고의 압축기 진동에 의한 소음 제어의 대책을 제시하였다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2007.11a
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• pp.293-296
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• 2007

Using the T3 free-piston shock tunnel in ANU, the cavity frequency and flow characteristics of no mass-injection, inclined mass-injection before the cavity, parallel or reverse mass-injection in the cavity are investigated in the case of Mach 3.7 inflow condition. No mass-injection doesn't have the harmonic frequencies but has high amplitude of pressure spectrum at 10 kHz. Inclined mass-injection attenuates the cavity flow fluctuation as disturbing the shear layer reflection at the trailing edge. Parallel mass-injection flow reflects at the trailing edge of the cavity directly hence, increases the cavity flow fluctuation at high injection pressure.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2005.11a
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• pp.117-120
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• 2005

The present study describes unsteady flow phenomena generated in a supersonic flow passing over a rectangular cavity and suggests a way of control of pressure oscillation, doing harm to overall performance and stable operation of aerodynamic and industrial applications. The three-dimensional, unsteady, compressible Navier-stokes equations are numerically solved based on a fully implicit finite volume scheme and large eddy simulation. The cavity flow are simulated with and without control methods, including a triangular bump and blowing jet installed near the leading edge of the cavity. The results show that the pressure oscillation is attenuated by both control techniques, especially near the trailing edge of cavity.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 1995.10a
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• pp.130-135
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• 1995

본 연구에서는 30000rpm으로 회전하는 진공청소기 원심팬의 유동장을 임펠러, 디퓨저, 케이싱을 모두 고려하여 해석하였다. 또한 삼차원으로 배출되는 출구를 간단한 sink 패널로 모델하여 출구의 효과를 충분히 고려하였다. 해석된 유동장 자료를 이용하여 먼 거리에서의 음압을 예측하였다. 예측된 음압자료는 FFT를 이용하여 측정된 값과 주파수 영역에서 비교하였다. 또한 진공청소기 원심팬의 측정자료에서 보이는 광역소음특성이 임펠러에서 흘려지는 후류와류의 교란에 의한 임펠러와 디퓨저 깃의 비정상 힘이 주된 원인임을 밝혔다.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 1993.10a
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• pp.107-111
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• 1993

본 논문에서는, 특히 고효율에 따른 소음 증가문제를 해결하기 위해 실험계획법을 이용한 머플러를 설계하였고, 설계단계에서부터 시뮬레이션 검증을 통해 효율을 고려한 저소음 머플러 설계가 가능하도록 머플러의 형상을 유한요소법에 의해 모델링한 후에, 소음해석 PACKAGE인 SYSNOISE를 이용하여 전달손실(TRANSMISSON LOSS) 해석을 해석하였고, 유동해석 PACKAGE인 PHONEMICS를 이용하여 압력손실을 최소화함으로써, 효율 및 소음측면에서 기존머플러보다도 더 우수한 머플러를 설계할 수 있는 PROCEDURE를 개발하였다. 이에 따라 차후 머플러내의 냉매유동특성과 소음특성을 동시에 고려한 머플러가 설계가능하리라 생각한다.