• 제목/요약/키워드: Antisymmetric Mode

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균일 열부가 하중을 받는 사각판의 자유 진동특성 연구 Part I. 이론 및 유한요소 해석 (Free Vibration Characteristics of the Rectangular Plates under Uniform Thermal Loading Part I. Analytic and FEM analysis)

  • 전병희;강휘원;이영신
    • 한국항공우주학회지
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    • 제39권2호
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    • pp.97-105
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    • 2011
  • 본 논문에서는 균일 열부가 하중을 받는 사각판의 자유 진동특성을 중첩법에 의한 수치해석과 유한요소 해석을 통하여 연구하였다. 사각판의 재질은 알루미늄, 강재 및 스테인레스강 이다. 부가한 온도 조건은 상온에서부터 $300^{\circ}C$까지 부가하였고, 경계조건은 자유-자유 조건이다. 완전 대칭 모드, 완전 역대칭 모드 및 대칭-역대칭 모드에 대한 해석이 수행되었다.

유도초음파를 이용한 박판에서의 결함의 검출에 관한 연구 (Detection of Defects in a Thin Steel Plate Using Ultrasonic Guided Wave)

  • 정희돈;신현재
    • 비파괴검사학회지
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    • 제18권6호
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    • pp.445-454
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    • 1998
  • 본 연구는 박판 용접부 결함 검출 기법의 확립을 위해서 실시된 기초 연구로서, 전기강판 소재의 모재에 인위적인 결함을 작성하고, 이론 및 시험적 결과를 이용하여 결함을 검출하기 위한 최적의 조건과 임계 검출 결함 크기를 조사한 것이다. 이를 위해서 소재의 dispersion curve를 구하고, 두께 2.4mm의 박판에 대해서 tone burst방식에 의한 초음파 탐상을 실시하였다. 실험적 검토를 행한 결과 840kHz의 가진 주파수와 30도 그리고 85도의 입사각이 최적의 탐상 조건임을 알았다. 한편, 초음파의 속도와 dispersion커브를 비교 검토하여 본 바, 30도의 입사각에서 발생하여 전파하는 초음파는 symmetic mode이고 85도의 입사각에서는 antisymmetric mode의 파가 전파하고 있었다. 결함의 위치와 형상에 따라 반사파의 특성이 다르게 나타나고 있었으며, 특히 표면 결함의 경우에는 antisymmetric 모드의 초음파가 symmetric 모드 보다 높은 반사파 에너지를 나타내고 있었다. 또한 이러한 초음파 모드의 종류와 결함 검출과의 관계에 대해서는 유도파의 구조에 의해서 설명이 가능했다.

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실험모드해석에 의한 승용차용 레디얼 타이어의 3차원 진동특성 (Experimental Modal Analysis for 3-D Vibration Characteristics of Radial Tire for Passenger Car under Free-Suspension)

  • 김용우;남진영
    • 한국자동차공학회논문집
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    • 제10권3호
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    • pp.227-236
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    • 2002
  • We have performed two kinds of experimental modal analyses fur a radial tire for passenger car under free-suspension. One is the modal analysis to obtain three-dimensional modes of tire using accelerometers and the other is the one to identify cavity resonance frequency using a pressure sensor. From the first analysis, we have obtained the three-dimensional natural modes, which makes it possible to grasp the features of the modes and to classify the vibrational modes into symmetric, non-symmetric, and antisymmetric modes in a simple way by using the experimental results. From the first and the second experimental analyses we have identified the cavity resonance frequency and its three-dimensional mode shape.

Antisymmetric-Symmetric Mode Conversion of Ultrasonic Lamb Waves and Negative Refraction on Thin Steel Plate

  • Sung, Jin Woo;Kim, Young H.
    • 비파괴검사학회지
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    • 제33권3호
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    • pp.270-275
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    • 2013
  • In this study, focusing of ultrasonic Lamb wave by negative refraction with mode conversion from antisymmetric to symmetric mode was investigated. When a wave propagates backward by negative refraction, the energy flux is antiparallel to the phase velocity. Backward propagation of Lamb wave is quite well known, but the behavior of backward Lamb wave at an interface has rarely been investigated. A pin-type transducer is used to detect Lamb wave propagating on a steel plate with a step change in thickness. Conversion from forward to backward propagating mode leads to negative refraction and thus wave focusing. By comparing the amplitudes of received Lamb waves at a specific frequency measured at different distance between transmitter and interface, the focusing of Lamb wave due to negative refraction was confirmed.

평면 충돌제트의 불안정특성(2)-원통음- (Characteristics of Plane Impinging Jets(2)- Cylinder-tone -)

  • 권영필;김욱;이주원
    • 한국소음진동공학회논문집
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    • 제14권2호
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    • pp.105-110
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    • 2004
  • The objective of this study is to obtain the instability characteristics of the plane jet impinging on circular cylinder associated with the cylinder-tone. It is found that the characteristics depends upon he ratio of the cylinder diameter to the nozzle width, D/h, and the jet velocity. When the ratio is oderate the cylinder-tone is similar to the edge-tone. With increase of the ratio, its characteristics ecomes similar to that of the plate-tone in which only the high-speed tone associated with turbulent et is generated. When D/h 〈1. the frequency range, especially the lower limit of frequency, is ignificantly influenced by the cylinder diameter. At around D/h = 1/2, while low speed tones are nduced with the antisymmetric mode of instability and affected by the vortex shedding from the ylinder, high-speed tones are generated, at first, with the symmetric mode of instability. and then, ith antisymmetric mode, as the jet velocity increases.

축으로 고정된 승용차용 레디얼 타이어의 3차원 진동특성 (3-D Vibration Characteristics of Radial Tire for Passenger Car under Fixed Axle)

  • 김용우;남진영
    • 한국소음진동공학회논문집
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    • 제12권3호
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    • pp.228-235
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    • 2002
  • Two kinds of experimental modal analyses have been performed on a radial tire for passenger car under fixed axle. One is the modal analysis to obtain three-dimensional modes of tire using accelerometers and the other is the one to identify cavity resonance frequency using a pressure sensor. From the first analysis, we have obtained three-dimensional natural modes and their decomposed 3-D modes in each direction, which make it possible to grasp the features of the modes that cannot be identified in the conventional 2-D modes and to classify the vibrationall modes into symmetric, non-symmetric, and antisymmetric modes in a simple way by using the experimental results. From the second experimental analysis, the cavity resonance frequency is found. Coomparing the results of the two analyses, we have Identified the three-dimensional mode of the cavity resonance. We also haute shown that natural frequencies of structural vibration depends on inflation Pressure while the cavity resonance does not.

점탄성층이 부분적으로 삽입된 샌드위치보의 횡진동 감쇠특성 (Behavior of the Flexural Vibration Damping of a Sandwich Beam System with a Partially Inserted Viscoelastic Layer)

  • 박진택;유형원;장석원;최낙삼
    • 대한기계학회논문집A
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    • 제26권2호
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    • pp.225-233
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    • 2002
  • The flexural vibration characteristics of a sandwich beam system with a partially inserted viscoelastic layer have been quantitatively studied using a finite element analysis in combination with a sine-sweep test. Antisymmetric mode shapes of the flexural vibration were visualized by the holographic interferometry and agreed with those calculated by the finite element simulation. Effects of the beam thickness as well as the length and thickness of partial viscoelastic layers on the system loss factor(η$\_$s/) and resonant frequency($\omega$$\_$r/) were significantly large fur the symmetric and antisymmetric modes of the beam system.

박판 상형 부재의 붕괴 특성연구 (Collapse of Thin-Walled Hatted Section Tubes)

  • 김천욱;한병기
    • 한국자동차공학회논문집
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    • 제2권1호
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    • pp.65-72
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    • 1994
  • Collapse characteristics of thin-walled hatted section tubes are investigated. The square section members with flanges are substituted by the equivalent rectangular tube. The stiffening effects of flanges are transformed to the restraining plate with the equivalency of buckling strength. The square tubes of single-hatted and double-hatted sections are investigated. The double-hatted section members show symmetric and antisymmetric crushing modes depending on the stiffness of flanges. The single-hatted section members show only symmetric modes. The bifurcation point of the compact crushing modes are investigated by experiments and shown almost same thickness-width ratio of the rectangular tubes. A large maximum crippling strength can be obtained by double-hatted section members with proper flange dimensions.

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점탄성층이 부분적으로 삽입된 샌드위치보의 횡진동모드별 감쇠특성 (Modal Damping of the Flexural Vibration of a Sandwich Beam with Partially Inserted Viscoelastic Layer)

  • 박진택;최낙삼
    • 한국복합재료학회:학술대회논문집
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    • 한국복합재료학회 2000년도 추계학술발표대회 논문집
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    • pp.224-227
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    • 2000
  • Modal damping characteristics of the flexural vibration of a sandwich beam with paaially inserted viscoelastic layer have been quantitatively studied using the finite element analysis in combination with an experiment. Antisymmetric mode shapes of the flexural vibration were visualized by the holographic interferometry and agreed with those calculated by the finite element simulation. Effects of the length and thickness of partial viscoelastic layers on the system loss factor($\mu$) and resonant frequency($\omega$) were considerably latge at both symmetric and antisymmetric modes of the sandwich beam.

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평면 충돌제트의 불안정 특성(1) -슬릿음- (Characteristics of Plane Impinging Jets(1) - Slit-tone -)

  • 권영필
    • 한국소음진동공학회논문집
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    • 제14권1호
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    • pp.50-55
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    • 2004
  • In this study, slit-tones by plane impinging jet are investigated experimentally over the whole subsonic flow range, especially at low speeds, in order to obtain the instability behaviour of impinging plane jet. Slit-tones are generated at low speeds associated with laminar shear layer instability as well as at high speeds associated with turbulent instability. Most of low-speed slit-tones are induced by symmetric mode instability unless the slit is not so wide, in which case antisymmetric modes are induced like edge-tones. It is found that the frequencies at low speeds ate controled by the unstable condition of the vortex at the nozzle exit and its pairings by which the frequencies are decreased by half. In the case of symmetric modes related with low-speed slit-tones, frequencies lower than those associated with one-step pairings are not found.