• 제목/요약/키워드: Helmholtz mode

검색결과 48건 처리시간 0.027초

헬름홀츠 공진기에 따른 버너내의 음향장에 관한 수치해석 (Numerical Simulation of the Acoustic Field in a Burner with Helmholtz Resonators)

  • 홍정구;조한창;신현동
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2007년도 제34회 KOSCO SYMPOSIUM 논문집
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    • pp.86-91
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    • 2007
  • A study was performed to understand self-excited pressure fluctuations in the lean premixed flames and to evaluate the effect of Helmholtz resonator on the pressure fluctuations. As low-frequency pressure fluctuations have been reported to cause fatal damage to the combustor and the entire system, Helmholtz-type resonators, which reduce the damage by low-frequency pressure fluctuation in the combustor, are attached to the channel of unburned mixture flow. It is found that the range of low-frequency pressure fluctuations of flame mode 2 is narrowed by the attachment of Helmholtz resonators. From this result, if Helmholtz-type resonators are applied to actual gas turbine combustor, it is confirmed that Helmholtz resonators attached on the fuel discharge hole are also effective for narrowing the range of flame mode 2

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하이브리드 로켓 불안정성 I (Hybrid Rocket Instability I)

  • 이선재;이정표;문희장;성홍계;김진곤
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2012년도 제38회 춘계학술대회논문집
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    • pp.81-85
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    • 2012
  • 본 연구에서는 하이브리드 로켓에서 발생되는 대표적인 불안정성 모드에 대한 연구를 수행하였다. 연소 불안정을 유도하기 위하여 연료 전방 및 후방에 다이아프램(diaphragm)을 설치하여 연소 실험을 수행 하였다. 길이방향 음향 모드(Longitudinal Acoustic Mode)와 헬름홀츠 모드(Helmholtz Mode)의 이론 모델을 사용한 주파수 계산 결과와 FFT 분석을 이용해 얻은 실험 주파수 비교를 통해 해당 모드를 찾을 수 있었고, 이론 주파수와 실험 주파수가 유사함을 확인하였다.

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구조-음향 연성계의 경계값 변화에 따른 방사음 변화 (A Parameter Study on the Frequency Characteristics of the Structural-acoustic Coupled System)

  • 김양한;서희선
    • 한국소음진동공학회논문집
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    • 제14권7호
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    • pp.604-611
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    • 2004
  • It is well known that wall impedance essentially determines how sound wave transmits from one place to another. The wall impedance is related with its dynamic properties : for example, the mass, stiffness, and damping characteristics. It is noteworthy, however, that the wall impedance is also function of spatial characteristics of two spaces that is separated by the wall. This is often referred that the wall is not locally reacting. In this paper, we have attempted to see how the acoustic characteristics of the two spaces is affected by various structure parameters such as density, applied tension, and a normalized length of the wall. Calculations are conducted for two different modally reacting boundary conditions by modal expansion method. The variation of the Helmholtz mode and the structural-dominated mode are analyzed as the structure parameters vary. The displacement distribution of the structure, pressure and active intensity of the inside and outside cavity are presented at the Helmholtz mode and the structure-dominated mode. It is shown that the frequency characteristics are governed by both structure-and fluid-dominated mode. The results exhibit that the density of the structure is the most sensitive design parameter on the frequency characteristics for the coupling system as we could imagine in the beginning. The Helmholtz mode frequency decrease as density increases. However. it increases as applied tension and an opening size increase. The bandwidth of the Helmholtz mode is mainly affected by density of the structure and its opening size.

SQUID 2차미분기 성능 평가용 균일자기장 및 2차 미분 자기장 발생원 (Sources of uniform and 2nd-order gradient fields for testing SQUID performance)

  • 이순걸
    • Progress in Superconductivity
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    • 제8권2호
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    • pp.152-157
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    • 2007
  • Uniaxial square Helmholtz coils for testing SQUID sensors were designed and their field distributions were calculated. Optimum parameters for maximizing the uniform region in the Helmholtz mode were obtained for different uniformity tolerances. The coil system consists of 2 pairs of identical square loops, a Helmholtz pair for generating uniform fields and the other for the 2nd-order gradient fields in combination with the Helmholtz pair. Full expressions of the axial component of the field were calculated by using Biot-Savart's law. To understand the behavior of the field near the coil center, analytical expressions were obtained up to the 4th-order in the midplane and along the coil axis. The Helmholtz condition for generating uniform fields was calculated to be $d/{\alpha}=0.544505643$, where 2d is the inter-coil distance and $2{\alpha}$ is the side length of the coil square. Maximized uniform range can be obtained for a given nonuniformity tolerance by choosing $d/{\alpha}$ slightly lower than the Helmholtz condition. The pure second-order gradient field can be generated by subtracting the Helmholtz field from the field of the 2nd pair with equal magnitudes of the center fields of the two pairs. The coil system is useful for testing balance and sensitivity of SQUID gradiometers.

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Changing PEO coating formation on Mg alloys by particle additions to the treatment electrolyte

  • Blawert, Carsten;Srinivasan, Bala;Liang, Jun;Huang, Yuanding;Hoche, Daniel;Scharnagl, Nico;Heitmann, Volker;Burmester, Ulrich
    • 한국표면공학회:학술대회논문집
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    • 한국표면공학회 2012년도 추계총회 및 학술대회 논문집
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    • pp.7-11
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    • 2012
  • Plasma electrolytic oxidation of magnesium alloys is a well known technique to produce corrosion and wear resistant coatings. The addition of particles to the electrolyte provides a possibility to produce coatings with an increasing range of composition by in-situ incorporation of those particles into the coating. An extensive literature review has revealed that the mode of incorporation depends mainly on the melting point of the used particles and the energy provided by the discharges of the PEO process. The spectrum ranges from inert to partly reactive incorporation, but a complete reactive incorporation and a formation of a new single phase coating was not observed so far. Thus a new approach in PEO processing is introduced using specific particles as a kind of sintering additive, changing not only the composition but lowering the melting temperature and increase the liquid phase fraction during the discharges, resulting in a new amorphous coating.

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헬름홀츠 솔버 기반의 3차원 열음향해석을 통한 발전용 단일 캔 연소기에서의 공진 모드 분석 (Resonance Mode Anlaysis in a Single Can-type Combustor through 3D Thermo-acoustic Analysis based on Helmholtz Solver)

  • 정준우;김대식
    • 한국분무공학회지
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    • 제29권1호
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    • pp.23-31
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    • 2024
  • This study conducted a 3D thermo-acoustic analysis based on the helmholtz solver to analyze the major resonance modes causing combustion instability in a single-can combustor. The experimental investigations were carried out on a test rig designed by the Korea Institute of Machinery & Materials (KIMM) under various conditions of hydrogen co-firing and fuel staging. Through these experiments, two primary unstable frequencies were identified. To determine the resonance modes of these frequencies, a 3D thermo-acoustic analysis was conducted using temperature information from the test rig. The results confirmed that the unstable frequencies observed in the experiments were all longitudinal modes. Additionally, the mode shapes identified in the analysis facilitated a simplification of the exit geometry for the low-order network model, confirming that this did not significantly affect the fundamental resonance modes.

유입수로폭의 조정을 통한 항만부진동 제어 (Control of Seiches by Adjustment of Entrance Channel Width)

  • Yong Jun Cho
    • 한국해안해양공학회지
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    • 제9권2호
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    • pp.57-62
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    • 1997
  • 우리나라 항만의 응답스펙트럼중 상당부분을 설명하는 Helmholtz mode를 중심으로 기운영되고 있는 항만중 정온도 확보에 어려움을 겪고 있는 항만을 대상으로 입사된 파랑에너지의 항내체류시간의 최소화를 통해 경제적 항내정온도 개선책을 모색하고자 고유진동수 등 항만 시스템의 동적특성을 해석하였다. 이를 기초로 항내 정온도 개선책으로 유공방파제 등에 부분적으로 도입되고 있는 에너지 소산 구조를 확대 적용하는 방안과 항만유입수로 폭을 제어수단으로 활용하는 방안을 제안한다. 수치모의 결과 항만유입수로 폭이 축소됨에 따라 부가 Hydrodynamic length에 의해 항만의 고유진동수는 감소하고 따라서 lower bound tunning을 통해 내습하는 파랑의 spectrum의 energy containing part와 유리할 수 있음을 입증하였다.

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하이브리드 로켓 불안정성 II (Hybrid Rocket Instability II)

  • 이정표;이선재;김영남;문희장;성홍계;김진곤
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2012년도 제38회 춘계학술대회논문집
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    • pp.86-90
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    • 2012
  • 본 연구에서는 '하이브리드 로켓 불안정성 I'에 이어 하이브리드 로켓에서 발생할 수 있는 연소불안 정성에 대해 연구하였다. 하이브리드 로켓 연소기 내부에 와류가 발생할 수 있도록 연소기를 설계하여 연소시험을 수행하였고, 연소실 압력 공진 주파수의 다이아프램 유 무에 따른 특성, 연료 길이에 따른 특성, 연료 포트 직경에 따른 특성, 다이아프램 직경에 따른 특성, 노즐목 직경에 따른 특성, 산화제 유량 변화에 따른 특성에 대한 연구를 수행하였다. 본 연구의 주요 연소실 압력 공진 주파수는 Vortex shedding으로 판단되며, Hybrid low frequency와 Helmholtz mode가 또다른 공진주파수 인 것으로 판단된다.

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FDF를 이용한 메탄 희박 예혼합 연소기의 비선형 열음향학적 불안정성 해석 (FDF-based analysis of nonlinear combustion instability in the lean premixed combustor)

  • 오승택;신영준;김용모
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2015년도 제51회 KOSCO SYMPOSIUM 초록집
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    • pp.115-116
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    • 2015
  • In the present approach, the flame-acoustics interaction is represented by FDF (Flame Describing Function) which is a important source term in the Helmholtz' equation. In this study, the combustion instability is analyzed by the forced mode strategy with the measured FDF. Numerical results indicate that the present approach reasonably well predicts the essential features of the combustion instability characteristics in the lean premixed combustor under the gas-turbine like environment.

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음향공이 장착된 로켓엔진 연소실의 음향장 수치해석 (A Numerical Analysis of Acoustic Behavior in Combustion Chamber with Acoustic Cavity)

  • 손채훈;김영목
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2003년도 제20회 춘계학술대회 논문집
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    • pp.249-252
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    • 2003
  • 음향불안정을 억제하는 수동제어기구중 하나인 음향공의 음향학적 효과를 파악하기 위해, 음향공이 장착된 로켓엔진 연소실의 음향장 특성을 수치해석적으로 조사하였다. 음향공 모델로서 Helmholtz 형태의 공명기가 채택되었고, 조화해석을 통해 주로 음향공에 의해 야기되는 음향학적 효과를 관찰하였다. 음향공의 동조주파수를 변화시켜가면서 연소실의 음향진동 응답을 구하고, 제1접선방향 음향모드의 감쇠인자를 구하였다. 동조주파수가 공진주파수에 접근함에 따라 모드분할 현상이 나타났고, 이로 인해 음향공을 본래의 제1접선방향 음향모드에 동조시키더라도 음향감쇠효과가 저하됨을 알았다. 효과적인 감쇠를 위해서는, 억제하고자 하는 음향모드로부터 모드분할 현상이 나타나지 않으면서 그 음향모드의 감쇠효과를 극대화하도록 음향공을 동조시키는 것이 바람직함을 알 수 있었다.

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