• Title/Summary/Keyword: 진동분리

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The Effect of Reference Mic. Array Shape on MUSIC and Beamforming Methods in Acoustical Holography (음향 홀로그래피에서 기준 마이크로폰 어레이가 빔형성 방법과 다중 신호 분리 방법에 미치는 영향)

  • 이원혁;이명준;강연준
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2001.05a
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    • pp.1003-1008
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    • 2001
  • In beamforming method, source positions are predicted by MUSIC (Multiple Signal Classification) power method and composite sound fields can then be decomposed into each partial field by beamforming, detenninistically without restriction of the distance between reference microphones and sources. However, reference microphone array shape is important in both MUSIC and beamforming method. Thus the present paper describes the effect of the reference microphone array shape.

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Development of a Modal Parameter Estimation Method Using Optimization Techniques (최적화기법을 이용한 모드매개변수 추정방법의 개발)

  • 이건명;주영호
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 1995.10a
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    • pp.217-220
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    • 1995
  • 본 논문에서는 최적화기법을 이용하여 모드매개변수를 추정하는 방법을 개발하였다. 최적화기법중 steepest descent method와 Fletcher-Powell method를 1자유도계의 시뮬레이션 데이터에 사용하여 Fletcher-Powell method가 초기값이나 계의 감쇠비에 관계없이 항상 정확한 모드매개변수를 추정함을 밝혀 내었다. 2자유도계의 시뮬레이션 데이터에 적용하였을 때도 본 방법은 정확한 모드매개변수를 추정하였다. 본 방법은 기존의 모드해석방법처럼 실제모드수보다 많은 모드수를 가정할 필요가 없고, 밀집한 모드를 분리하는 능력도 우수하였다. 본 방법을 실험 데이터에 적용하였을 때에도 만족할만한 결과를 나타내었다.

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Partial Field Decompositon Using Beamforming Method Under Reflective Condition (반사면이 존재하는 환경에서 빔포밍 방법을 이용한 부분 음장 재구성)

  • 선종천;강연준
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2003.11a
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    • pp.730-734
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    • 2003
  • A beamforming method is a kind of spatial filter that focus the amy's signal capturing abilities in a desired direction. In this paper, we detect the location of a source under reflective condition using the multi-dimensional MUSIC algorithm then, we can iud the image source locations from the experimental geometry, and we reconstruct the partial fields for direct wave and reflected wave by using Adaptive nulling algorithm. Numerical simulations are performed to verify its performance under various conditions.

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Development of Experimental Dynamic Modification Technique for Mounted System (마운트계의 실험적 변경설계법의 개발)

  • 정의봉;조영희
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 1996.10a
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    • pp.351-356
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    • 1996
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New Approach for Economic Treatment Solution of Industrial Waste Water by New Separation Technology (VSEP) (새로운 진동막 분리기술을 이용한 산업폐수의 경제적 처리방안)

  • 신대윤;김용대;지은상
    • Proceedings of the Membrane Society of Korea Conference
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    • 1998.10a
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    • pp.19-30
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    • 1998
  • 1. 서론 : 그동안 막분리공정 기술이 이십년 여러산업 분야에서 사용되어 오면서 새로운 막제조 기술 및 적용 또한 발전을 하여 오고 있다. 막분리기술이 폭넓게 사용을 되어오고 있지만 높은 투자비 (특히 저용량일 경우), 운전비용 그리고 막의 오염 등으로 국내의 대부분 적용업체가 적잖은 문제를 경험을 하여왔다. 특히 막의 오염은 잦은 화학세정과 교체비용의 부담이 가져다 준다.(생략)

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Free vibrational analysis of a circular ring with a concentrated mass (집중질량을 가지는 원환의 자유진동 해석)

  • 홍진선;김석현;이장무
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.11 no.1
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    • pp.170-176
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    • 1987
  • This study is concerned with dynamic characteristics of a circular ring with a concentrated mass attached. The equations of motion are set up and are solved by using Laplace transformation. The ratio of a concentrated mass to the mass of circular ring is used as a parameter. Experiment was performed by employing impulse test and the results show good agreement with those of analysis. The results of this study can be utilized in vibrational analysis of axisymmetric shells with slight asymmetries.

Finite Element Vibration Analysis of Structures with Cyclic Symmetry using Discrete Fourier Transform (이산푸리에 변환을 이용한 순환대칭 구조물의 유한요소 진동 해석)

  • 김창부;김정락
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 1995.10a
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    • pp.221-226
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    • 1995
  • 터빈 익렬, 펌프 익차, 원형 냉각탑, 치차 등과 같이 동일한 형상이 원주 방향으로 반복되어 있는 순환 대칭 구조물의 진동특성을 유한 요소법을 사용하여 해석하는 경우에 전체구조를 모델링하는 대신에 구조물을 동일한 형상의 부분구조로 분할하여 부분구조 한개만을 모델링하고 분할된 경계에서 적절한 경계조건을 부과하여 진동해석을 수행함으로서 컴퓨터 기억용량을 절감시키고 계산시간을 단축할 수 있는 방법이 널리 사용되고 있다. Orris and Petyt[1]는 부분구조의 양쪽 분할 경계면, 즉 연결 경계상에 있는 절점변위의 상관관계를 복소파동전파식을 이용해서 구하여 부분구조의 감소된 복소강성행렬 및 질량행렬을 만들고 실수부와 허수부를 분리하여 유한요소해석을 수행하는 방법을 제안하였다. 유한요소 프로그램 ANSYS[2]에서는 이와 같은 방법을 사용하고 있다. Thomas[3]는 순회 정규모드를 이용하였고, 참고문헌[4]에서는 순회행렬을 이용하였다. 또한 유한요소 프로그램 MSC/NASTRAN[5]에서는 푸리에 급수를 이용하고 유한요소 절점의 위치 및 변위를 원통 좌표계를 표현하여 순환대칭구조물의 유한요소해석을 수행할 수 있도록 되어있다. 본 논문에서는 순환 대칭구조물의 형상의 주기성과 순환성을 고려하여 이산퓨리에 변환을 이용함으로써 순환대칭구조물의 유한요소진동해석을 체계적으로 저용량의 컴퓨터에서 신속하고 정확하게 수행할 수 있는 방법을 제안하고자 한다.

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Design and Implementation of Arduino-based Lightweight Vibration Monitoring System (아두이노 기반의 경량 진동 모니터링 시스템 설계 및 구현)

  • Kwon, Dong-hyun;Lim, Ji-yong;Heo, Sung-uk;Oh, Am-suk
    • Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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    • 2017.05a
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    • pp.586-589
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    • 2017
  • The vibration monitoring system using the sensor network is used in various fields. However, in case of the vibration of the existing products, the size of the monitoring system is increased due to the separation of the sensor data collection function and the communication function. In this paper, we design and implement a lightweight vibration monitoring system using the MQTT protocol, which is oneM2M device standard protocol for the Arduino and Ethernet modules, to monitor frequent earthquakes and vibrations in narrow places.

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Nonlinear Transonic Flutter Analysis of a Composite Fin Considering Delamination Effect (층간분리 효과를 고려한 복합재 핀의 비선형 천음속 플러터 해석)

  • Gwang Young Lee;Ki-Ha Kim;Dong-Hyun Kim
    • Journal of Aerospace System Engineering
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    • v.17 no.6
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    • pp.82-93
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    • 2023
  • In this paper, nonlinear transonic flutter analyses of a composite missile fin considering the effect of delamination are conducted. An effective modal analysis methodology is adopted and verified with the experimental modal test data for laminated composite plates with delamination. Extended version of the in-house computational aeroelastic analysis program with the transonic small-disturbance (TSD) code is used in order to predict the flutter dynamic pressure of the delaminated composite fin models. In the subsonic, transonic, and supersonic flow regions, nonlinear time-domain flutter analyses are performed for various delamination conditions, and aeroelastic characteristics due to the delamination phenomena are examined in detail.