• 제목/요약/키워드: Forced Resonance

검색결과 128건 처리시간 0.022초

Effects of oscillation parameters on aerodynamic behavior of a rectangular 5:1 cylinder near resonance frequency

  • Pengcheng Zou;Shuyang Cao;Jinxin Cao
    • Wind and Structures
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    • 제38권1호
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    • pp.59-74
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    • 2024
  • Large Eddy Simulation (LES) is used to explore the influence of vibration frequency and amplitude on the aerodynamic performance of a rectangular cylinder with an aspect ratio of B/D=5 (B: breadth; D: depth of cylinder) at a Reynolds number of 22,000 near resonance frequency. In smooth flow conditions, the research employs a sequence of three-dimensional simulations under forced vibration with diverse frequency ratios fe / fo = 0.8-1.2 (fe : oscillation frequency; fo : Strouhal frequency when the rectangular cylinder is stationary ) and oscillation amplitudes Ah/D = 0.05 - 0.3. The individual influences of fe / fo and Ah/D on the characteristics of integrated and distributed aerodynamic forces are the focal points of discussion. For the integrated aerodynamic force, particular emphasis is placed on the analysis of the dependence of velocity-proportional component C1 and displacement-proportional component C2 of unsteady aerodynamic force on amplitude and frequency ratio. Near the resonance frequency, the dependencies of C1 and C2 on amplitude are stronger than that of frequency ratio. For the distributed aerodynamic force, the increase in frequency and amplitude promotes the position of the main vortex core and reattachment to the leading edge in the streamwise direction. In the spanwise direction, vibration enhances the spanwise correlation of aerodynamic force to weaken the three-dimensional effect of the flow field, and a lower frequency ratio and larger amplitude amplify this effect.

위성 안테나 구조물의 자유진동 및 정현파 강제 진동 해석 (Free Vibration and Forced Sinusoidal Vibration Analysis for Satellite Antenna Structures)

  • 신원호;오일권;한재흥;오세희;이인;김천곤;박종흥
    • Composites Research
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    • 제14권5호
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    • pp.20-25
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    • 2001
  • 본 논문 MSC/NASTRAN을 사용하여 Ka 와 Ku 대역 위성 탑재형 안테나 구조물의 자유진동현상 및 정현파 강제 진동 응답에 대한 유한요소해석을 수행하였다 안테나 구조물과 위성 버스체간의 동적 연성을 피하고, 기본 강성 조건을 입증하기 위해 최소 고유진동수 조건을 만족하도록 설계하였다. 정현파 강제 진동의 경우, Large mass 방법을 사용하여 기저 진동형태로 해석하였고, X-, Y-, Z- 축에 대해 독립적으로 입력 가속도에 대한 응답 가속도들을 관찰하였다. 유한요소해석을 통해 얻어진 결과들은 실제 위성 안테나 검증 실험에 있어서 검증 및 비교 자료로 사용될 수 있고, 시험 계획 수립에도 응용될 수 있다

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A multiple scales method solution for the free and forced nonlinear transverse vibrations of rectangular plates

  • Shooshtari, A.;Khadem, S.E.
    • Structural Engineering and Mechanics
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    • 제24권5호
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    • pp.543-560
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    • 2006
  • In this paper, first, the equations of motion for a rectangular isotropic plate have been derived. This derivation is based on the Von Karmann theory and the effects of shear deformation have been considered. Introducing an Airy stress function, the equations of motion have been transformed to a nonlinear coupled equation. Using Galerkin method, this equation has been separated into position and time functions. By means of the dimensional analysis, it is shown that the orders of magnitude for nonlinear terms are small with respect to linear terms. The Multiple Scales Method has been applied to the equation of motion in the forced vibration and free vibration cases and closed-form relations for the nonlinear natural frequencies, displacement and frequency response of the plate have been derived. The obtained results in comparison with numerical methods are in good agreements. Using the obtained relation, the effects of initial displacement, thickness and dimensions of the plate on the nonlinear natural frequencies and displacements have been investigated. These results are valid for a special range of the ratio of thickness to dimensions of the plate, which is a characteristic of the Multiple Scales Method. In the forced vibration case, the frequency response equation for the primary resonance condition is calculated and the effects of various parameters on the frequency response of system have been studied.

내부공진을 가진 원판의 비선형 강제진동해석 (Nonlinear Analysis of a Forced Circular Plate with Internal Resonance)

  • 김철홍;이원경
    • 대한기계학회논문집
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    • 제16권11호
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    • pp.2098-2110
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    • 1992
  • 본 연구에서는 중간평면의 비선형 신장을 고려한 원판의 강제진동을 해석하기 위해 Fig.1과 같은 경계조건 즉 꺽쇠로 고정된(clamped) 경우를 생각한다.이 경우 에 고유진동수 사이엔 .omega.$_{1}$+2.omega.$_{2}$=.omega.$_{3}$의 관계가 존재하는데 이 관계가 내부공진 조건이 됨이 입증된다. 원판에 작용하는 가진력으로는 조화가진을 가정하 고 가진진동수가 2.omega.$_{1}$+.omega.$_{2}$에 가까운 경우 즉 조합공진(combination reso- nance)일 때를 고려한다.

비선형 2자유도계의 비감쇠 강제진동 연구 (A Sudy on the Undamped Forced Vibration of Nonlinear Two-Degree-of-Freedom Systems)

  • 박철희;박선재;윤영석
    • 대한기계학회논문집
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    • 제12권2호
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    • pp.193-199
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    • 1988
  • 본 연구의 목적은 SCPA방법을 이용한 비선형 2자유도 비감쇠계의 해석을 통하여 응답곡선을 구하고, 그 응답곡선의 분기현상을 규명함에 있다. 결과의 비교를 위하여 4차의 Runge-Kutta방법을 이용한 수치실험을 수행하였다.

발전소 통풍계통의 가변속 적용 후 진동특성에 관한 연구 (Study on Vibration Characteristics after Applying Variable Speed Control to Constant Speed Fans used in a Power Plant)

  • 조철환;송오섭;양경현;김계연;조성태;문현동
    • 동력기계공학회지
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    • 제13권6호
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    • pp.88-94
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    • 2009
  • In this paper, vibration characteristics after applying variable speed control to fans with a rated speed used in a power plant are studied by performing experiments and analyzing finite element models. Then the campbell diagram is presented to verify the reason of the abnormal vibration measured from fan structure during variable operation of Forced Draft Fan & Induced Draft Fan. According to results, it is found that amplitude of acceleration increases abruptly when a 2X harmonic component meets the natural frequency of fan rotor. Therefore it is very important thing that investigate exactly dynamic characteristics for the rotor at variable speed zone before applying variable speed control to a rotor with a rated speed.

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유한요소법에 의한엔진 구조소음 해석 (An Engine Structure-Borne Noise Analysis by Finite Element Method)

  • 안상호;김주연;김규철
    • 한국자동차공학회논문집
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    • 제6권1호
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    • pp.122-133
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    • 1998
  • This paper presents the static analysis, the modal analysis and the forced vibration analysis on engine structures to find out the structure-borne noise sources by finite element method. The deformation of engine structures under the maximum combu- stion gas force was calculated through the static analysis, and the resonance possibilities were predicted by the modal analysis which ascertains mode shapes and the corresponding frequencies of engine global and its major noise sources in engine surfaces were investigated with the forced vibration analysis by means of finding the transfer mobilities on engine surfaces due to the piston impact and the velocity levels due to the combustion in consideration of oil film stiffness and damping coefficients. Finally, the direction of engine structure-borne noise reduction can be estabilished by the above-mentioned analysis procedure and the reduction effect of cost on proto-type engine build-up is expected.

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고속전철용 견인전동기 소음개선 (Noise Reduction of Traction Motor for High Speed Train)

  • 김정철;김대광;김봉철;박영호;최종묵
    • 한국철도학회:학술대회논문집
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    • 한국철도학회 2007년도 추계학술대회 논문집
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    • pp.95-100
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    • 2007
  • The traction motor for High Speed Train is being required reliability and stability for high-speed operation. And also required low noise level, high performance, compact size owing to the space and weight limitation for attaching to train, etc. As a result of requiring the low noise level and high power capacity, it is adopted forced-air-ventilation insead of self-ventilation that is generally used on electric multiple unit. Traction motor is cooled by cooling air through the air-ventilation hole. When the traction motor is operated with forced-air-ventilation, there is some abnormal noise in the specific RPM. This paper is dealing with the method to reduce the resonance phenomena by adopting the rotor blade.

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압전세라믹 냉각팬에 의한 강제 공랭 모듈 주위의 유체유동과 열전달 특성 (Fluid Flow and Heat Transfer Characteristics around a Surface-Mounted Module Cooled by Forced Air Flow by Piezoelectric Cooling Fan)

  • 박규진;박상희
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2003년도 추계학술대회
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    • pp.272-277
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    • 2003
  • This paper reports the fluid flow and heat transfer around a module cooled by forced air flow generated by a piezoelectric(PZT) cooling fan. A flexible PZT fan with distortion in a fluid transport system of comparatively simple structure which was mounted on a PCB in a parallel-plate channel($450{\times}80{\times}700mm^3$) accelerates surrounding fluid locally. Input voltages of 20-100V and a resonance frequency of 23Hz were used to vibrate the cooling fan. Input power to the module was 4W. The cooling effect using a PZT fan was larger than that of free convection. Fluid flow around the module were visualized by using PIV system. The temperature distribution around heated module were visualized by using liquid crystal film(LCF). We found that the flow type was y-shaped and the cooling effect was increased by the wake generated by a piezoelectric cooling fan.

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유체맥동을 고려한 배관계의 진동해석 (Vibration Analysis of Pipes Considering Fluid Pulsation)

  • 서영수;정석현;이성현;홍진숙;정의봉
    • 한국소음진동공학회논문집
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    • 제16권10호
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    • pp.1050-1056
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    • 2006
  • In this paper, a new method for the stability analysis of a pipe conveying fluid which pulsates periodically is presented. The finite element model is formulated liking into consideration of the effects of the fluid pulsating in a pipe. The damping and stiffness matrices in the finite element equation vary with time due to pulsating fluid. Coupled effects of several harmonic components in the velocity of fluid to a pipe is discussed. A new unstable region appears which will not appear in the stability analysis of single pulsating frequency. A method to directly estimate the forced response of pipe is also discussed. The results presented in this paper are verified by the time domain analysis.