• 제목/요약/키워드: Flutter Test

검색결과 67건 처리시간 0.025초

자유진동 및 강제진동 기법을 이용한 플레이트 거더교의 플러터 계수 산정 (Estimation of Flutter Derivatives for a Plate Girder Bridge Using Forced and Free Oscillation Tests)

  • 김종대
    • 한국전산구조공학회:학술대회논문집
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    • 한국전산구조공학회 2011년도 정기 학술대회
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    • pp.332-335
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    • 2011
  • 바람에 의해 발생하는 장대교량의 진동현상은 버펫팅과 와류진동 그리고 플러터 등으로 구분할 수 있으며, 특히 설계풍속에 해당하는 강풍에 안전한 교량을 설계하는 것이 주된 관심사항이다. 이러한 장대교량의 공기역학적인 안정성 검토에 사용되는 플러터 계수를 풍동실험을 통하여 산정하였다. 본 논문에서는 일반적인 플레이트 거더교의 강풍에 대한 안정성을 검토하기 위하여 풍동실험을 수행하였으며, 자유진동 기법과 강제진동 기법을 사용하여 추출한 플러터 계수를 비교하였다. 자유진동 기법은 교량단면에 초기변위를 주어 상하 및 회전 진동을 하는 교량단면의 변위를 측정한 후 system identification 기법으로 플러터 계수를 구하게 된다. 그리고 강제진동 기법은 상하방향의 강제진동과 회전방향의 강제진동 실험을 독립적으로 수행하여 교량단면에 작용하는 풍하중과 단면의 진동을 분석함으로써 플러터 계수를 추정하게 된다. 그리고 플러터 계수의 비교를 통하여 강제진동 기법과 자유진동 기법의 장단점을 분석하였다.

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실시간 플러터 해석 프로그램 개발 (Development of Real-Time Flutter Analysis Program)

  • 이주연;배재성;황재혁;노진호
    • 한국항공우주학회지
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    • 제45권2호
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    • pp.99-105
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    • 2017
  • 공력탄성학적 현상들을 확인하는 방법 중 하나인 풍동실험은 축소 모델을 제작해야하기 때문에 복잡하고 비용이 많이 들며, 유동 속도의 제한이 있는 등의 단점이 있다. 이러한 단점을 보완하여 풍동실험을 대체할 수 있는 Dry Wind-Tunnel(DWT) 기법이 제안되었다. 이는 지상 진동 실험 장치와 공기력을 계산하는 소프트웨어로 구성되어 실시간으로 유체의 영향을 고려해준다. 본 연구에서는 DWT의 핵심적인 요소인 실시간 공기력 계산프로그램을 개발하고, 구조 모델을 소프트웨어로 표현하여 두 시스템을 실시간 연동해 플러터 해석을 수행하였다. Matlab Simulink와 dSPACE를 이용하여 실시간 플러터 해석을 수행하고 이를 상용프로그램인 ZAERO를 사용한 결과와 비교하여 검증하였다.

키트용 접이식 복합재 날개 개발 (A Development of Pivoting Composite Wing for Mounting Kit)

  • 주영식;전우철;변관화;조창민
    • 한국군사과학기술학회지
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    • 제16권4호
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    • pp.486-492
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    • 2013
  • The pivoting composite wing is developed for the kit to be mounted on the external stores. The wing has a pivoting structure for the installation to an aircraft and high aspect ratio to increase lift drag ratio. The wing needs to be light and have sufficient strength and stiffness to satisfy structural design requirements. The wing is designed with carbon fiber composite and the structural parts are integrated to reduce cost to manufacture. In order to verify the structural performances, the design load analysis and flight load survey, the static analysis and test, the ground vibration test and flutter analysis are performed. It is shown that the wing has sufficient structural strength and stiffness to satisfy the structural design requirements.

크랙을 가진 유체유동 파이프의 안정성 해석 (Stability Analysis of Pipe Conveying Fluid with Crack)

  • 안태수;손인수;윤한익
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2006년도 추계학술대회논문집
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    • pp.865-868
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    • 2006
  • In this paper, a dynamic behavior(natural frequency) of a cracked simply supported pipe conveying fluid is presented. In addition, an analysis of the flutter and buckling instability of a cracked pipe conveying fluid due to the coupled mode (modes combined) is presented. Based on the Euler-Bernouli beam theory, the equation of motion can be constructed by using the Lagrange's equation. The crack section is represented by a local flexibility matrix connecting two undamaged beam segments. The stiffness of the spring depends on the crack severity and the geometry of the cracked section. The crack is assumed to be in the first mode of fracture and to be always opened during the vibrations. This study will contribute to the safety test and stability estimation of structures of a cracked pipe conveying fluid.

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비점성 저차모델링 기법을 활용한 비선형 플러터 해석 (NONLINEAR FLUTTER ANALYSIS USING INVISCID REDUCED ORDER MODELING TECHNIQUE)

  • 김요한;김동현
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2011년 춘계학술대회논문집
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    • pp.458-464
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    • 2011
  • A new method identifies coupled fluid-structure system with a reduced set of state variables is presented. Assuming that the structural model is known a priori either from an analysis or a test and using linear transformations between structural and aeroelastic states, it is possible to deduce aerodynamic information from sampled time histories of the aeroelastic system. More specifically given a finite set of structural modes the method extracts generalized aerodynamic force matrix corresponding to these mode shapes. Once the aerodynamic forces are known, an aeroelastic reduced-order model can be constructed in discrete-time, state-space format by coupling the structural model and the aerodynamic system. The resulting reduced-order model is suitable for constant Mach, varying density analysis.

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크랙을 가진 유체유동 파이프의 안정성 해석 (Stability Analysis of Pipe Conveying Fluid with Crack)

  • 손인수;안태수;윤한익
    • 한국소음진동공학회논문집
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    • 제17권1호
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    • pp.10-16
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    • 2007
  • In this paper, the dynamic stability of a cracked simply supported pipe conveying fluid is investigated. In addition, an analysis of the flutter and buckling instability of a cracked pipe conveying fluid due to the coupled mode(modes combined) is presented. Based on the Euler-Bernouli beam theory, the equation of motion can be constructed by using the Galerkin method. The crack section is represented by a local flexibility matrix connecting two undamaged pipe segments. The stiffness of the spring depends on the crack severity and the geometry of the cracked section. The crack is assumed to be in the first mode of fracture and to be always opened during the vibrations. This results of study will contribute to the safety test and a stability estimation of the structures of a cracked pipe conveying fluid.

영상신호의 시가지 이동수신에 의한 화상열화요인의 평가법에 관한 연구 (A Study on Picture Quality Impairing Factors and Evaulation Method for The Video Signal in Urban Mobile Reception)

  • Deock Ho Ha
    • 전자공학회논문지A
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    • 제30A권3호
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    • pp.52-60
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    • 1993
  • Fluttering ghost which is the most severs picture impairment in mobile TV reception under multipath fading environments can be detected by measuring the dynamic variation of the synchronizing pulse timing. And also, the occurrence-stucture of fluttering ghost are directly correlated with the multipath parameters. This paper describes the quantitative evaluating method of the mobile TV pictures impaired by multipath parameters by means of the spectral analysis of synchronizing timing fluctuation. The ghost-flutter curve derived from the spatial amplitue spectrum of synchronizing pulse timing fluctuation express well the spatial variation characteristic, and it has been found to be the quantitative evaluating measure of picture impairment in mobile reception. A correspondence between the ghost-flutter curve (and/or index) and picture quality opinion test results is established.

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Wind-induced vibrations and suppression measures of the Hong Kong-Zhuhai-Macao Bridge

  • Ma, Cunming;Li, Zhiguo;Meng, Fanchao;Liao, Haili;Wang, Junxin
    • Wind and Structures
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    • 제32권3호
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    • pp.179-191
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    • 2021
  • A series of wind tunnel tests, including 1:50 sectional model tests, 1:50 free-standing bridge tower tests and 1:70 full-bridge aeroelastic model tests were carried out to systematically investigate the aerodynamic performance of the Hong Kong-Zhuhai-Macao Bridge (HZMB). The test result indicates that there are three wind-resistant safety issues the HZMB encounters, including unacceptable low flutter critical wind speed, vertical vortex-induced vibration (VIV) of the main girder and galloping of the bridge tower in across-wind direction. Wind-induced vibration of HZMB can be effectively suppressed by the application of aerodynamic and mechanical measures. Acceptable flutter critical wind speed is achieved by optimizing the main girder form (before: large cantilever steel box girder, after: streamlined steel box girder) and cable type (before: central cable, after: double cable); The installations of wind fairing, guide plates and increasing structural damping are proved to be useful in suppressing the VIV of the HZMB; The galloping can be effectively suppressed by optimizing the interior angle on the windward side of the bridge tower. The present works provide scientific basis and guidance for wind resistance design of the HZMB.

횡방향 새그를 가진 자정식 현수교의 공탄성 거동(I) -주형의 거동을 중심으로- (Aeroelastic Behaviors of Self-anchored Suspension Bridge with Lateral Sag of Main Cable(I) -Focused on the Behavior of Girder-)

  • 권순덕;장승필
    • 한국강구조학회 논문집
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    • 제9권2호통권31호
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    • pp.259-267
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    • 1997
  • 본 연구에서는 주 케이블에 횡방향 새그를 가진 자정식 현수교의 내풍안정성을 검토하기 위하여 풍동실험을 수행하고, 주형의 거동을 중심으로 그 결과를 분석하였다. 등류와 난류하에서 수행한 부분 모형 실험에서 가장 내풍안정성이 뛰어난 단면을 최종단면으로 선정하고, 전교 모형 실험을 통하여 검증하였다. 또한 차후 연구를 위한 플러터 계수를 측정하여 제시하였다. 교량의 사용성과 피로문제를 검토하기 위하여 버페팅 응답을 조사하였지만, 공학적 관점에서 만족할 만한 수준인 것으로 나타났다. 주형의 항력계수가 상당히 큼에도 불구하고 횡방향 변위가 매우 작게 나타났는데, 이는 주 케이블의 횡방향 새그가 주형의 변위를 구속하기 때문인 것으로 판단된다.

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A novel method for the vibration optimisation of structures subjected to dynamic loading

  • Munk, David J.;Vio, Gareth A.;Steven, Grant P.
    • Advances in aircraft and spacecraft science
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    • 제4권2호
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    • pp.169-184
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    • 2017
  • The optimum design of structures with frequency constraints is of great importance in the aeronautical industry. In order to avoid severe vibration, it is necessary to shift the fundamental frequency of the structure away from the frequency range of the dynamic loading. This paper develops a novel topology optimisation method for optimising the fundamental frequencies of structures. The finite element dynamic eigenvalue problem is solved to derive the sensitivity function used for the optimisation criteria. An alternative material interpolation scheme is developed and applied to the optimisation problem. A novel level-set criteria and updating routine for the weighting factors is presented to determine the optimal topology. The optimisation algorithm is applied to a simple two-dimensional plane stress plate to verify the method. Optimisation for maximising a chosen frequency and maximising the gap between two frequencies are presented. This has the application of stiffness maximisation and flutter suppression. The results of the optimisation algorithm are compared with the state of the art in frequency topology optimisation. Test cases have shown that the algorithm produces similar topologies to the state of the art, verifying that the novel technique is suitable for frequency optimisation.