• 제목/요약/키워드: Wind Vibration

검색결과 996건 처리시간 0.026초

헬리콥터용 차세대 블레이드의 공력탄성학적 안정성에 관한 시험적 연구 (An Experimental Investigation of the Aeroelastic Stability of Next-generation Blade for Helicopter)

  • 김준호;김승호;이제동;이욱;송근웅
    • 한국소음진동공학회논문집
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    • 제16권8호
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    • pp.848-856
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    • 2006
  • This paper describes the aeroelastic stability test of the small-scaled 'Next-generation Blade(NRSB)' with NRSH (next-generation hub system) and HCTH hingeless hub system in hover and forward flight conditions. Excitation tests of rotor system installed in GSRTS (general small-scale rotor test system) at KARI (Korea Aerospace Research Institute) were carried out to get lead-lag damping ratio of blades with flexures as hub flexure. MBA(moving block analysis) technique was used for the estimation of lead-lag damping ratio. First, NRSB-1F blades with HCTH hub system, then NRSB- 1F with NRSH hub system were tested. Second, NRSB-2F blades with NRSH hub system were tested. Tests were done on the ground and in the wind tunnel according to the test conditions of hover and forward flight, respectively. Non-rotating natural frequencies, non-rotating damping ratios and rotating natural frequencies were showed similar level for each cases. Estimated damping ratios of NRSB-1F, NRSB-2F with HCTH and NRSH were above 0.5%, and damping ratio increased by collective pitch angle increasement. Furthermore damping ratios of NRSB-2F were higher than damping ratios of NRSB-1F in high Pitch angle. It was confirmed that the blade design for noise reduction would give observable improvement in aeroelastic stability compared to paddle blade and NRSB-1F design.

Control of the VIV of a cantilevered square cylinder with free-end suction

  • Li, Ying;Li, Shiqing;Zeng, Lingwei;Wang, Hanfeng
    • Wind and Structures
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    • 제29권1호
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    • pp.75-84
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    • 2019
  • A steady slot suction near the free-end leading edge of a finite-length square cylinder was used to control its aerodynamic forces and vortex-induced vibration (VIV). The freestream oncoming flow velocity ($U_{\infty}$) was from 3.8 m/s to 12.8 m/s. The width of the tested cylinder d = 40 mm and aspect ratio H/d = 5, where H was the height of the cylinder. The corresponding Reynolds number was from 10,400 to 35,000. The tested suction ratio Q, defined as the ratio of suction velocity ($U_s$) at the slot over the oncoming flow velocity at which the strongest VIV occurs ($U_{\nu}$), ranged from 0 to 3. It was found that the free-end slot suction can effectively attenuate the VIV of a cantilevered square cylinder. In the experiments, the RMS value of the VIV amplitude reduced quickly with Q increasing from 0 to 1, then kept approximately constant for $Q{\geq}1$. The maximum reduction of the VIV occurs at Q = 1, with the vibration amplitude reduced by 92%, relative to the uncontrolled case. Moreover, the overall fluctuation lift of the finite-length square cylinder was also suppressed with the maximum reduction of 87%, which occurred at Q = 1. It was interesting to discover that the free-end shear flow was sensitive to the slot suction near the leading edge. The turbulent kinetic energy (TKE) of the flow over the free end was the highest at Q = 1, which may result in the strongest mixing between the high momentum free-end shear flow and the near wake.

합성데이터를 이용한 비지도학습 기반 실시간 와류진동 탐지모델 (Unsupervised Vortex-induced Vibration Detection Using Data Synthesis)

  • 이선호;김선중
    • 한국전산구조공학회논문집
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    • 제36권5호
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    • pp.315-321
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    • 2023
  • 장대교량은 낮은 고유진동수와 감쇠비를 가지는 초유연구조물로 진동사용성 문제에 취약하다. 하지만 현재 국내 설계지침에서는 풍속이나 진폭에 대한 임계값을 기반으로 유해진동 발생 여부를 평가하고 있다. 본 연구에서는 장대교량에서 발생하는 유해진동을 보다 정교하게 식별하기 위하여 딥러닝 기반 신호분할 모델을 활용한 데이터 포인트 단위의 와류진동 식별 방법론을 제안한다. 특별히 포락선을 가지는 사인파를 활용하여 와류진동에 해당하는 데이터를 합성함으로써 모델 구축에 필수적인 와류진동 데이터 획득 및 라벨링 과정을 대체하였다. 이후 푸리에 싱크로스퀴즈드 변환를 적용하여 시간-주파수 특징을 추출하여 신경망의 인풋 데이터로 사용하였다. 합성데이터만을 이용하여 양방향 장단기 기억신경망(Bidirectional Long-Short-Term-Memory) 모델을 훈련하였고 이를 라벨 정보를 포함한 실제 사장교의 계측데이터를 이용하여 학습한 모델과 비교하여 모델의 실시간 와류진동 식별 성능을 검증하였다.

초고층건축물의 수평진동사용성 평가 기준의 재고 (Review on Human Comfort Criteria in Tall Buildings)

  • 조강표;정승환;조기성;김무환
    • 한국전산구조공학회:학술대회논문집
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    • 한국전산구조공학회 2008년도 정기 학술대회
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    • pp.410-415
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    • 2008
  • This paper presents review on human comfort criteria in major codes and standards for tall buildings. In general, human comfort criteria of tall buildings have been used by magnitude of wind-induced acceleration response. Two different indexes in determination of the magnitude have been used: the peak value which occurs during a period of time and the rms value averaged over this same period. These distinctive acceleration indexes are discussed in detail and each criterion is reviewed and compared. The distinctions arisen because of the different wave forms, or acceleration signatures are addressed. It is described that which index of acceleration should be adopted in establishment of Korean human comfort criteria. In addition, some arguments from a technical standpoint that favor the use of each index are presented.

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일면지지식 Extradosed교의 계획 및 설계 (Plan IE Design Of Extradosed Bridge Supported by Single Plane Cables)

  • 이종대;이두화;권소진;김종수;손준상
    • 한국콘크리트학회:학술대회논문집
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    • 한국콘크리트학회 2001년도 가을 학술발표회 논문집
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    • pp.615-620
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    • 2001
  • The aim of this paper is to open up a relatively new type in bridge engineering by introducing plan and design of extradosed bridge which is implemented in Sungnam-Janghowon T/K project. The topic encompasses parametric study including the behavior of the bridge relevant to the cable layout, the distance from pier table to the first cable's location, the height of pylon, the stiffness of cross section and wind vibration to ascertain sectional type of bridge and span length. For the purpose of the knowledge base presented here, the important feature of design is recommended such as modeling method, camber control, finite element analysis and heat hydration of pier table. We can verify the issue related to the characteristics of extradosed bridge as a result of study and design endeavor.

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구조-음향 모드 비연성에 의한 차량의 부밍 소음 저감 (Booming Noise Reduction of Passenger Cars by Mode Decoupling of Structural-Acoustic Systems)

  • 고강호;이장무
    • 소음진동
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    • 제9권4호
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    • pp.822-827
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    • 1999
  • The reduction of booming noise level and improvement of sound quality in the vehicle interior have been major fields of vehicle NVH for many years. In order to reduce the booming noise this paper proposed a system variable, which takes account of mode shapes and natural frequencies of the structural-acoustic system, measurement points and excitation frequency. By simplifying the system variable, the major contributors of panels inculding roof, roof lining, wind shield glasses, doors and floor to booming noise at a specific frequency was experimentally found. Also the relationships between structural modes of roof lining, one of the major contributors, and acoustic modes of compartment cavity were investigated from the viewpoint fo structure-borne noise. In addition, the roof lining was modified structurally by applying marble sponge to the gap between roof and roof lining. Asthe result of structural modification, the booming noise was reduce at target frequency.

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Bending analysis of FGM plates using a sinusoidal shear deformation theory

  • Hadji, Lazreg;Zouatnia, Nafissa;Kassoul, Amar
    • Wind and Structures
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    • 제23권6호
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    • pp.543-558
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    • 2016
  • The response of functionally graded ceramic-metal plates is investigated using theoretical formulation, Navier's solutions, and a new displacement based on the high-order shear deformation theory are presented for static analysis of functionally graded plates. The theory accounts for a quadratic variation of the transverse shear strains across the thickness, and satisfies the zero traction boundary conditions on the top and bottom surfaces of the plate without using shear correction factors. The plates are assumed to have isotropic, two-constituent material distribution through the thickness, and the modulus of elasticity of the plate is assumed to vary according to a power-law distribution in terms of the volume fractions of the constituents. Numerical results of the new refined plate theory are presented to show the effect of the material distribution on the deflections, stresses and fundamental frequencies. It can be concluded that the proposed theory is accurate and simple in solving the static and free vibration behavior of functionally graded plates.

The near wake of three circular cylinders in an equilateral triangular arrangement at a low Reynolds number Re=100

  • Bai, Honglei;Lin, Yufeng;Alam, Md. Mahbub
    • Wind and Structures
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    • 제30권5호
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    • pp.451-463
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    • 2020
  • Two-dimensional numerical simulations are conducted at a low Reynolds number Re = 100 to investigate the near wake of three identical circular cylinders that are arranged in an equilateral triangular configuration. The incident angle of the three-cylinder configuration with respect to incoming flow is varied from θ = 0° to 60°, while the spacing between adjacent cylinders (L) covers a wide range of L/D = 1.25-7.0, where D is diameter of the cylinder. Typical flow structures in the near wake of the three-cylinder configuration are identified, including a single Karman vortex street, bistable flip-flopping near wake, anti-phase and/or in-phase vortex shedding, shear layer reattachment, and vortex impingement, depending on the configuration (L/D, θ). The behavior of Strouhal number (St) is discussed in detail, echoing the distinct structures of near wake. Furthermore, fluid forces on the individual cylinders are examined, which, though highly depending on (L/D, θ), exhibit a close correlation to the near wake behavior.

Numerical study of the effect of periodic jet excitation on cylinder aerodynamic instability

  • Hiejima, S.;Nomura, T.
    • Wind and Structures
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    • 제5권2_3_4호
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    • pp.141-150
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    • 2002
  • Numerical simulations based on the ALE finite element method are carried out to examine the aerodynamics of an oscillating circular cylinder when the separated shear flows around the cylinder are stimulated by periodic jet excitation with a shear layer instability frequency. The excitation is applied to the flows from two points on the cylinder surface. The numerical results showed that the excitation with a shear layer instability frequency can reduce the negative damping and thereby stabilize the aerodynamics of the oscillating cylinder. The change of the lift phase seems important in stabilizing the cylinder aerodynamics. The change of lift phase is caused by the merger of the vortices induced by the periodic excitation with a shear layer instability frequency, and the vortex merging comes from the high growth rate, the rapid increase of wave number and decrease of phase velocity for the periodic excitation in the separated shear flows.

On the flutter characteristics of separated two box girders

  • Matsumoto, Masaru;Shijo, Rikuma;Eguchi, Akitoshi;Hikida, Tetsuya;Tamaki, Hitoshi;Mizuno, Keisuke
    • Wind and Structures
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    • 제7권4호
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    • pp.281-291
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    • 2004
  • The flutter characteristics of long span bridges are discussed from the point of the unsteady pressure distribution on bridge deck surface during heaving/torsional vibration related to the aerodynamic derivatives. In particular, it is explained that the coupling terms, which consist of $A_1^*$ and $H_3^*$, play a substantial role on the coupled flutter, in comparison with the flutter characteristics of various structural sections. Also the effect of the torsional/heaving frequency ratio of bridge structures on the flutter instability is discussed from the point of the coupling effect between heaving and torsional vibrations.