• 제목/요약/키워드: Acoustic-pressure Response

검색결과 119건 처리시간 0.026초

불균질한 온도장을 고려한 가스터빈 연소기의 음향장 해석 (A Numerical Analysis of Acoustic Characteristics in Gas Turbine Combustor with Spatial Non-homogeneity)

  • 손채훈;조한창
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 춘계학술대회
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    • pp.1292-1297
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    • 2004
  • Acoustic characteristics in an industrial gas-turbine combustor are numerically investigated by adopting linear acoustic analysis. Spatially non-homogeneous temperature field in the combustor is considered in the numerical calculation and the characteristics are analyzed in view of acoustic instability. Acoustic analysis are conducted in the combustors without and with acoustic resonator, which is one of combustion stabilization devices. It has been reported that severe pressure fluctuation frequently occurs in the adopted combustor, and the measured signal of pressure oscillation is compared with the acoustic-pressure response from the numerical calculation. The numerical results are in a good agreement with the measurement data. In this regard, the phenomenon of pressure fluctuation in the combustor could be caused by acoustic instability. The acoustic effects of the resonators are analyzed in the viewpoints of both the frequency tuning and the damping capacity.

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시간지연 모델의 적용을 통한 수소/공기 확산화염의 음향파 응답 분석 (A Numerical Analysis of Acoustic-Pressure Response of H2-Air Diffusion Flames with Application of Time-Lag Model)

  • 손채훈;임준석
    • 한국추진공학회지
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    • 제16권1호
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    • pp.1-8
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    • 2012
  • 희석된 수소-공기 확산화염의 응향 응답 특성을 저압과 고압 영역에서의 화염 구조 해석을 토대로 수치적으로 조사하였다. 음향 주파수가 증가함에 따라 어느 압력 영역에서든 열방출율의 비선형 축적현상에 의해 유한 화학반응의 효과가 증진된다. 이는 결국 높은 음향 증폭으로 이어지게 된다. 동일한 계산 결과를 압력 감응 시간지연 모델에 의해 재해석하였다. 시간 지연 모델의 적절한 적용을 통해, 각 압력 영역에서 시간지연과 간섭지수 인자가 정량화되었다. 음향 증폭의 정도를 나타내는 간섭지수는 어느 압력 영역에서든 1000 Hz 근처에서 최고값을 나타내었고, 고압영역에서 화염이 더 불안정한 응답을 보였다. 음향 주파수에 따른 간섭지수의 변화 경향은 기존의 증폭지수 변화 경향과 잘 일치하였다.

다물체계내 유연체의 구조기인 소음해석 (Structure Borne Noise Analysis of a Flexible Body in Multibody System)

  • 김효식;김창부
    • 한국소음진동공학회논문집
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    • 제13권11호
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    • pp.882-889
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    • 2003
  • This paper presents the method for structure borne noise analysis of a flexible body in multibody system. The proposed method is the superposition method using the flexible multibody dynamic analysis and the finite element one. This method is executed in 3 steps. In the 1st step, time dependent quantities such as dynamic loads, modal coordinates and gross body motion of the flexible body are calculated through a flexible multibody dynamic analysis. And frequency response functions of those time dependent quantities are computed through Fourier transforms. In the 2nd step, acoustic pressure coefficients are obtained through structure-acoustic coupling analyses by the finite element method. In the final step, frequency responses of acoustic pressure at the acoustic nodes are recovered through linear superposition of frequency response functions with acoustic pressure coefficients. The accuracy of the proposed method is verified in the numerical example of a simple car model.

스피커 진동판의 음향특성 다분야통합최적설계 (Multidisciplinary Design Optimization for Acoustic Characteristics of a Speaker Diaphragm)

  • 김성국;이태희;이석순
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2004년도 추계학술대회논문집
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    • pp.763-766
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    • 2004
  • Recently, various acoustic artifacts that contains speaker have been produced such as cellular phone. Speaker consists of diaphragm generating sound and coil vibrating diaphragm. Generally, good speaker means that it has a wide frequency range, high output power rate to input power and flat sound pressure level in specified frequency range. Acoustic characteristic was estimated through the experiment and computer simulation, or sound power was controlled with acoustic sensitivity in a natural frequency range fer last decade. However, the flatness of sound pressure level has not been considered to enhance the sound quality of a speaker. Tn this study, a method for speaker design is proposed for a good acoustic characteristic, which is flatness of SPL(sound pressure level) and wideness between the first and second natural frequency. SYSNOISE is used fer acoustic analysis and ANSYS is used for harmonic response analysis and modal analysis. Optimization for acoustic characteristics of a speaker diaphragm is performed using ModelCenter. All analyses are done within a frequency domain. And we confirm that the experimental and computational simulations have similar trend.

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PZT5 spherical shell-typed hydrophone simulation using a coupled FE-BE method

  • Jarng, Soon-Suck
    • 한국음향학회:학술대회논문집
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    • 한국음향학회 1998년도 학술발표대회 논문집 제17권 1호
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    • pp.477-481
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    • 1998
  • This paper describes the application of a coupled finite element-boundary element method to obtain the steady-state response of a hydrophone. The particular structure considered is a flooded piezoelectric spherical shell. The hydrophone is three-dimensionally simulated to transduce an incident plane acoustic pressure onto the outer surface of the sonar spherical shell to electrical potentials on inner and outer surfaces of the shell. The acoustic field formed from the scattered sound pressure is also simulated. And the displacement of the shell caused by the externally incident acoustic pressure is shown in temporal motion. The coupled FE-BE method is described in detail.

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수중폭발로 인한 파이프의 동적 응답해석 (Dynamic Response Analysis of Pipe Subjected to Underwater Explosion)

  • 김성범;이경재;정동호;박대효
    • 대한토목학회논문집
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    • 제34권1호
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    • pp.9-16
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    • 2014
  • 최근 수중폭발로 인한 구조물의 충격응답에 대한 연구는 매우 높은 비용과 소요시간, 민감한 환경문제 등으로 인하여 실제 시험보다는 컴퓨터를 통한 수치해석적 연구가 활발히 진행되어 왔다. 또한 시뮬레이션의 기술 향상과 더욱 정교해진 기능들로 수치 시뮬레이션의 효율성이 증가되었을 뿐 아니라 그 신뢰성까지 증가하였다. 본 연구에서는 유체 표면의 Acoustic Pressure와 구조물 표면 변위의 적절한 관계를 다루는 구조-유체 상호작용(FSI : Fluid-Structure Interaction), 수중폭파 형태를 결정하는 유체의 깊이와 폭발물과 구조물 사이의 거리에 대한 파라미터를 상용 유한요소 프로그램인 ABAQUS에 적용한 시뮬레이션 값과 실험적 이론 값 비교에 중점을 두었다. 수중폭발로 인한 파이프의 충격테스트 응답 분석은 ABAQUS/Explicit을 사용하여 수행되었고, 시간이력에 따른 충격하중, Acoustic Pressure, 타격지점의 응력, 속도, 변형에너지 등 ABAQUS CAE에서 결과를 나타내었다.

압력섭동과 연관된 연소응답모델에 기초한 고주파 연소불안정의 이론-수치적 고찰 (Hybridal Analysis of High-Frequency Combustion Instability with Pressure-Coupled Combustion Response Model)

  • 윤웅섭;이길용
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2003년도 제20회 춘계학술대회 논문집
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    • pp.253-257
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    • 2003
  • Theoretical-numerical analysis of wave instability is conducted with parametric response function model. Fluctuating instantaneous mass evaporation rate functionally coupled with pressure perturbations with phase lag is assumed to examine the validity of the method. With sufficiently large amplitude and less phase lag to perturbation, combustion response is resonant to pressure waves, unstable waves are amplified, and the system is driven to instability. Magnitude of response is a crucial instability parameter in the determination of a stability margins and makes a critical change of balancing conditions between the amplifying and damping acoustic energies. In the phase regime the unstable waves are amplified, whereas, the acoustic waves are attenuated in the out-of-phase regime. In the intermediate regime, no distinct tendency of unstable waves was determined.

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압력파에 교란된 액적내부에서의 에너지 파동 및 반응 메커니즘 (Thermal Wave Transfer and Combustion Response of Droplet Perturbed by Acoustic Pressure)

  • 이길용;윤웅섭
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2005년도 제24회 춘계학술대회논문집
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    • pp.183-188
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    • 2005
  • 본 연구에서는 기상 압력파동에 구속된 액적 내부의 에너지 파동과 연소응답의 상관관계를 고찰하였다. SRK 상태방정식과 Flash 계산법에 기초한 1차원 액적 기화모델로 기상과 액상의 2상 시스템에 대한 수치해석을 수행하였다. n-Pentane 액적과 기체 질소를 대상으로 기상압력과 압력파동 구동주파수에 따른 에너지 파동의 전파특성을 분석하였다. 액적 내부 에너지 파동의 주파수가 낮을수록 액적 내부로의 에너지 전파가 용이하였으며 결과적으로 연소응답의 크기를 감소시키는 요인이 되었다.

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배플이 장착된 로켓엔진 연소기의 음향장 해석 (A Numerical Study on Acoustic Behavior in Baffled Combustion Chambers)

  • 손채훈
    • 대한기계학회논문집B
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    • 제26권7호
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    • pp.966-975
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    • 2002
  • Acoustic behavior in baffled combustion chambers is numerically investigated by adopting linear acoustic analysis. Partial blade baffle, which is a variant of blade baffle, and hub-blade baffle with six blades are employed as baffle models. Through modal analysis, natural frequencies of each acoustic mode in baffled chambers are calculated and the reduction in natural frequencies caused by baffle installation is examined. Through harmonic analysis, acoustic pressure responses of each chamber to acoustic oscillating excitation are shown. The first tangential mode is found to be most sensitive to acoustic oscillation. Acoustic damping effect of baffle is quantified by damping factor. Damping effect of hub-blade baffle is the most appreciable and damping factor of partial blade baffle is much lower than that of blade baffle. Damping effect of six-blade baflle on the second tangential mode is as much as on the first tangential mode and hub-blade baffle can damp out appreciably the first tangential as well as the first radial mode with the aid of hub.

Optimization for the direction of arrival estimation based on single acoustic pressure gradient vector sensor

  • Wang, Xu-Hu;Chen, Jian-Feng;Han, Jing;Jiao, Ya-Meng
    • International Journal of Naval Architecture and Ocean Engineering
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    • 제6권1호
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    • pp.74-86
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    • 2014
  • The optimization techniques are explored in the direction of arrival (DOA) estimation based on single acoustic pressure gradient vector sensor (APGVS). By analyzing the working principle and measurement errors of the APGVS, acoustic intensity approaches (AI) and the minimum variance distortionless response beamforming approach based on single APGVS (VMVDR) are deduced. The radius to wavelength ratio of the APGVS must be not bigger than 0.1 in the actual application, otherwise its DOA estimation performance will degrade significantly. To improve the robustness and estimation performance of the DOA estimation approaches based on single APGVS, two modified processing approaches based on single APGVS are presented. Simulation and lake trial results indicate that the performance of the modified approaches based on single APGVS are better than AI and VMVDR approaches based on single APGVS when the radius to wavelength ratio is not bigger than 0.1, and the two modified DOA estimation methods have excellent estimation performance when the radius to wavelength ratio is bigger than 0.1.