• 제목/요약/키워드: Oscillating foil

검색결과 8건 처리시간 0.021초

동요하는 날개를 이용한 파랑 중 선박의 추력발생 (Propulsion by Oscillating Foil Attached to Ship in Waves)

  • 최윤락
    • 한국해양공학회지
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    • 제27권1호
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    • pp.31-36
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    • 2013
  • In this paper, the effects of a foil attached to a ship on the ship motion, added resistance, and thrust generation in waves are analyzed. The unsteady theory for a two-dimensional foil is introduced to determine the coupled motion responses of the ship and foil. The thrust caused by the oscillating foil is evaluated and compared to the added resistance of the ship, so that a positive net thrust can be possible in waves. A comparison of the results of unsteady, quasi-steady, and experimental analyses is performed.

전파하는 파동유장 중 전진하며 동요하는 2차원 날개의 동력해석 (Powering Analysis of Oscillating Foil Moving in Propagating Wave Flow Field)

  • 최윤락
    • 한국해양공학회지
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    • 제33권3호
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    • pp.229-235
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    • 2019
  • In this study, a two-dimensional oscillating foil with forward speed in a propagating wave flow field was considered. The time-mean power to maintain the heaving and pitching motions of the foil was analyzed using the perturbation theory in an ideal fluid. The power, which was a non-linear quantity of the second-order, was expressed in terms of the quadratic transfer functions related to the mutual product of the heaving and pitching motions and incoming vertical flow. The effects of the pivot point and phase difference among the disturbances were studied. The negative power, which indicates energy extraction from the fluid, is shown as an example calculation.

Characteristics of Vortical Jet Structures of a Hydrofoil

  • Yang, Chang-Jo;Kim, You-Taek;Choi, Min-Seon
    • Journal of Advanced Marine Engineering and Technology
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    • 제31권7호
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    • pp.842-851
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    • 2007
  • Oscillating foil propulsion, the engineering application of fish-like movement of a hydrofoil, has received in recent decades as a possible competitor for propellers. The oscillating foil produces an effective angle of attack, resulting in a normal force vector with thrust and lift components, and it can be expected to be a new highly effective propulsion system. We have explored propulsion hydrodynamics as a concept in wake flow pattern. The present study has been examined various conditions such as oscillating frequencies and amplitudes in NACA0010 profile. Flow visualizations showed that high thrust was associated with the generation of moderately strong vortices, which subsequently combine with trailing-edge vorticity leading to the formation of a reverse $K\acute{a}rm\acute{a}n$ vortex street. Vortex generation was inherent to jet production and playeda fundamental role in the wake dynamics. And it was shown that the strong thrust coefficient obtained as the Strouhal number was larger.

피칭 운동익에 작용하는 비정상 유체력 (Unsteady Fluid Forces Acting on a Pitching Foil)

  • 양창조
    • 한국유체기계학회 논문집
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    • 제8권6호
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    • pp.47-54
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    • 2005
  • An oscillating foil can produce a driving force through the generation of a reversed $K\'{a}rm\'{a}n$ vortex street, and it can be expected to be a new highly effective propulsion system. A simple pitching foil model was made and it was operated within a water channel. The wake formation behind a pitching foil was visualized and unsteady fluid forces were measured using a 6-axis force sensor based on force and moment detectors. We have been examined various conditions such as reduced frequency, amplitude and pivot point in NACA 0010. The results showed that thrust coefficients increased with a reduced frequency. We also presented the experimental results on the characteristics of a pitching foil at various parameters.

진동하는 2차원 날개 단면 주위에 대한 점성 유동장 계산( Part 1. 동적실속이 없는 경우 ) (Computation of Viscous Flows around a Two-dimensional Oscillating Airfoil ( Part 1. without Dynamic Stall ))

  • 이평국;김형태
    • 대한조선학회논문집
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    • 제44권1호
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    • pp.8-15
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    • 2007
  • In this paper, numerical calculations are performed to analyze the unsteady flow of NACA airfoil sections. In order to ease the flow computation for the fluid region changing in time, improve the quality of solution and simplify the grid generation for the oscillating foil flow, the computational method adopts a moving and deforming mesh with the multi-block grid topology. The multi-block, structured-unstructured hybrid grid is generated using the commercial meshing software Gridgen V15. The MDM (Moving & Deforming Mesh) and the UDF (User Define function) function of FLUENT 6 are adopted for computing turbulent flows of the foil in pitching motion. Computed unsteady lift and drag forces are compared with experimental data. in general, the characteristics of unsteady lift and drag of the experiments are reproduced well in the numerical analysis.

히빙익 후류의 유동패턴에 관한 연구 (A Study on the Vortical patterns of a Heaving Foil)

  • 양창조
    • Journal of Advanced Marine Engineering and Technology
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    • 제29권8호
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    • pp.899-906
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    • 2005
  • It is known that an oscillating airfoil can Produce a driving force through the generation of a reversed $K\'{a}rm\'{a}n$ vortex street, and this can be expected to be a new highly effective propulsion system. The wake formation behind the heaving airfoil was visualized and was measured using PIV systems We have been examined various conditions such as frequency number, amplitude in NACA 0010. As Strouhal number is greater than 0.08. wake profile with velocity deficit can be transformed into the wake with velocity excess After evaluating vortex center flow patterns in the wake investigated using tracking trajectories in temporal evaluation of the shedding vortices. We also Presented the experimental results on the unsteady vortices structure of the heaving airfoil at various parameters.

히빙익 후류의 유통패턴에 관한 연구 (A Study on Vortical Flow Patterns of a Heaving Foil)

  • 양창조;김유택;최민선;이영호
    • 한국마린엔지니어링학회:학술대회논문집
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    • 한국마린엔지니어링학회 2005년도 후기학술대회논문집
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    • pp.31-32
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    • 2005
  • It is known that an oscillating airfoil can produce a driving force through the generation of a reversed $K\acute{a}rm\acute{a}n$ vortex street, and this can be expected to be a new highly effective propulsion system. We have been examined various conditions such as frequency number, amplitude in NACA 0010. As Strouhal number is greater than 0.08, wake profile with velocity deficit can be transformed into the wake with velocity excess. We also presented the experimental results on the unsteady vortices structure of the heaving airfoil at various parameters.

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메소스케일 유연 외팔보 센서를 이용한 진동유동의 무선 계측 (Wireless Telemetry of an Oscillating Flow using Mesoscale Flexible Cantilever Sensor)

  • 박병규;이준식
    • 대한기계학회논문집B
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    • 제37권5호
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    • pp.495-501
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    • 2013
  • 곤충을 비롯한 많은 생물은 매질의 진동을 감지할 수 있는 다양한 감각기관을 이용하여 외부 교란을 감지하고 서로 통신하며 생명 유지활동을 하고 있다. 가장 가까이 접하는 진동유동의 대표적인 예로는 인체의 호흡을 들 수 있다. 본 연구에서는 마이크로제조 공정을 통해 메소스케일 저항식 감지소자, 특히 외팔보 형상의 유연 감지소자를 이용한 유량측정법을 제안하고, 무선통신을 이용한 유동측정 시스템화 및 휴대화의 가능성을 고찰하였다. 탄성계수가 낮은 기질재료를 사용함으로써 온 습도에 영향을 받지 않는 건강 진단용 호흡센서로서의 가능성 및 확장성을 확인하였다. 또한 유동감지 센서의 측정 데이터를 분석한 결과, 정밀성과 신뢰성은 마이크로 컨트롤러의 분해능, 노이즈 제거기술에도 의존하는 것으로 나타났다. 이 시스템에서 패킷 간의 최소 전송소요 시간은 약 16 ms로 나타났다.