• 제목/요약/키워드: Karman와

검색결과 287건 처리시간 0.024초

Theoretical Flow Instability of the Karman Boundary Layer

  • Hwang, Young-Kyu;Lee, Yun-Yong
    • Journal of Mechanical Science and Technology
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    • 제14권3호
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    • pp.358-368
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    • 2000
  • The hydrodynamic stability of the Karman boundary-layer flow due to a rotating disk has been numerically investigated for moving disturbance waves. The disturbed flow over a rotating disk can lead to transition at much lower Re than that of the well-known Type I instability mode. This early transition is due to the excitation of the Type II instability mode of moving disturbances. Presented are the neutral stability results concerning the two instability modes by solving new linear stability equations reformulated not only by considering whole convective terms but by correcting some errors in the previous stability equations. The reformulated stability equations are slightly different with the previous ones. However, the present neutral stability results are considerably different with the previously known ones. It is found that the flow is always stable for a disturbance whose dimensionless wave number k is greater than 0.75.

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관통유동 해석 방법을 이용한 축류형 홴의 소음예측 (The Prediction of the Axial Flow Fan Noise by Using Through-Flow Analysis Method)

  • 이찬;정동규;홍순성
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2000년도 춘계학술대회논문집
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    • pp.371-379
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    • 2000
  • A noise prediction method of axial flow fan is developed by incorporating through-flow method and vortex shedding noise model. Fan noise is assumed to be generated due to the pressure fluctuation induced by wake vortices of fan blades and radiate as diploe distribution. The wake vortices are analyzed by combining Karman vortex street model and through-flow analysis results, and the vortex-induced fluctuating pressure on blade surface is calculated by thin airfoil theory. The predicted sound pressure levels and directivity patterns of fan noise by the present method are favorably compared with fan noise test data. Furthermore, the present method is shown to be very useful for predicting the aero-acoustic performance map of the fan operated at off-design point.

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다공성 표면 평판 끝 단 위의 비정상 공력 특성에 대한 연구 (Unsteady Aerodynamics of Flat Plate with Porous Trailing-edge)

  • 정예은;문영준
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2008년도 춘계학술대회논문집
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    • pp.134-137
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    • 2008
  • In this study, a computational analysis is conducted to investigate the effects of porous surfaces on the lift and drag forces of the flat plate. With the porous treatment, it is found that the strength of the Karman vortex as well as its influences over the trailing-edge surface are much weakened, resulting in significant reduction of the pressure fluctuations over the flat plate. The drag and lift coefficients are decreased by 85% and 18%, respectively, compared to the solid surface. The computed results also indicate that the size of the porous surface area does not have much influences but the back side of the flat plate has non-negligible effects on the interaction between the wall and the Karman vortex. As a result, the lift coefficient for the solid back side case is decreased only by 50.5% compared to the solid case and the drag coefficient is even increased by 65%.

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원주의 진동과 칼만 와유출의 동기현상 (Lock-in Phenomenon in Oscillation of a Circular Cylinder Subject to a Uniform Flow)

  • 배헌민;김인철
    • 한국해양공학회지
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    • 제7권1호
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    • pp.114-123
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    • 1993
  • In is well known that a cyclic Karman vortex street is thrown out periodically from cylinder whose axis is vertical to the bulk flow. When the cylinder is vibrating in the frequency close to that of Karman vortex street, the vortex shedding frequency is locked onto that of cylinder. While there are many experimental studies for this phenomenon compared with analytical studies by numerical calculation, are very limited. In this study, a new algorithm for moving boundary is proposed and a simulator is develoed, which can deal with this phenomenon with experimental studies.

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IPO(Iterative PO)를 이용한 Ka 대역 Von Karman 레이돔 방사 특성 해석 (Analysis of Radiation Characteristics of Ka-Band Von Karman Radome Based on IPO Scheme)

  • 고일석;박창현;선웅
    • 한국전자파학회논문지
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    • 제22권12호
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    • pp.1148-1154
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    • 2011
  • 본 논문에서는 IPO 방법을 사용하여 Ka-band Von Karman 레이돔을 해석한다. Ka-band에서 레이돔같은 큰 물체를 해석하기 위해서는 보통의 수치 방법을 사용하기 힘들다. 그리고 PO(Physical Optics) 방법은 다중 반사(multiple reflection)를 고려할 수 없어 레이돔 해석에서 중요한 파라미터인 부엽(sidelobe level) 해석의 정확도에 한계를 갖는다. 그러므로 본 논문에서는 Nystrom 기반 PO 방법을 사용하는 IPO 방법을 사용하여 Ka-band 레이돔 해석 방법을 제안하고, 정확도 검증을 위해 Ku-band 실험 데이터와 IPO 결과를 비교한다. 또 Ka-band 시뮬레이션을 통해 높은 주파수에도 제안된 IPO 방법이 사용할 수 있음을 수치적으로 보인다.

A Numerical Study on the Karman Vortex Generated by Breaking of Mountain Wave

  • Sung-Dae Kang;Fujio Kimura
    • 한국환경과학회지
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    • 제1권2호
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    • pp.105.2-117
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    • 1992
  • The formation mechanism of the vortex streets in the lee of the mountain Is Investigated by a three-dimensional numerical model. The model is based upon the hydrostatic Boussinesq equations in which the vertical turbulent momentum flux is estimated by a turbulence parameterization scheme, but the horizontal viscosity is assumed to be constant. The results show that Karman vortex streets can form even without surface friction in a constant ambient flow with uniform stratification. The vortex formation is related to breaking of the mountain wave, which depends on the Froude number (Fr). In the case of a three-dimensional bell-shaped mountain, the wave breaking occurs when Fr is less than about 0.8, while a barman vortex forms when Fr is less than about 0.22. Vortex formation also depends on Reynolds number, which is estimated from the horizontal diffusivity. The vortex formation can be explained by the wave saturation theory given by Lindzen (1981) with some modification. Simulations in this study show that in the case of Karman vortex formation the momentum flux in the lower level is much larger than the saturated momentum flux, whereas it is almost equal to the saturated momentum at the upper levels as expected from the saturation theory. As a result, large flux divergence is produced in the lower layer, the mean flow is decelerated behind the mountain, and the horizontal wind shear forms between unmodified ambient wind. The momentum exchange between the mean flow and the mountain wave is produced by the turbulence within a breaking wave. From the result, well developed vortices like Karman vortex can be formed. . The results of the momentum budget calculated by the hydrostatic model are almost the same as nonhydrostatic results as long as horizontal scale of the mountain is 10 km. A well developed barman vortex similar to the hydrostatic one was simulated in the nonhydrostatic case. Therefore, we conclude that the hydrostatic assumption is adequate to investigate the origin of the Km8n vortex from the viewpoint of wave breaking.

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The effect of Reynolds number on the elliptical cylinder wake

  • Shi, Xiaoyu;Alam, Md. Mahbub;Bai, Honglei;Wang, Hanfeng
    • Wind and Structures
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    • 제30권5호
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    • pp.525-532
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    • 2020
  • This work numerically investigates the effects of Reynolds number ReD (= 100 - 150), cross-sectional aspect ratio AR = ( 0.25 -1.0), and attack angle α (= 0° - 90°) on the forces, Strouhal number, and wake of an elliptical cylinder, where ReD is based on the freestream velocity and cylinder cross-section height normal to the freestream flow, AR is the ratio of the minor axis to the major axis of the elliptical cylinder, and α is the angle between the cylinder major axis and the incoming flow. At ReD = 100, two distinct wake structures are identified, namely 'Steady wake' (pattern I) and 'Karman wake followed by a steady wake (pattern II)' when AR and α are varied in the ranges specified. When ReD is increased to 150, an additional wake pattern, 'Karman wake followed by secondary wake (pattern III)' materializes. Pattern I is characterized by two steady bubbles forming behind the cylinder. Pattern II features Karman vortex street immediately behind the cylinder, with the vortex street transmuting to two steady shear layers downstream. Inflection angle αi = 32°, 37.5° and 45° are identified for AR = 0.25, 0.5 and 0.75, respectively, where the wake asymmetry is the greatest. The αi effectively distinguishes the dependence on α and AR of force and vortex shedding frequency at either ReD. In Pattern III, the Karman street forming behind the cylinder is modified to a secondary vortex street. At a given AR and α, ReD = 150 renders higher fluctuating lift and Strouhal number than ReD = 100.

POD를 이용한 구조기본단면 주변 비정상흐름장 특성에 관한 연구 (Study on Unsteady Flow Field around Rectangular Cylinders using Proper Orthogonal Decomposition (POD))

  • 이재형;마츠모토 마사루
    • 한국강구조학회 논문집
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    • 제20권6호
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    • pp.751-759
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    • 2008
  • 본 연구에서는 구조적 기본단면인 사각단면중에서 B/D=2,3,4,5 단면을 대상으로 단면주위 흐름상태가 단면의 공기력 특성에 미치는 영향을 살펴보고, 정지/진동하는 B/D=4 사각실린더 주위의 비정상압력장에 POD해석을 도입함으로써 흐름패턴에 따른 POD해석의 고유벡터를 규정하고 실린더 주위 흐름장 안에 공존하는 서로 다른 흐름패턴의 상호간섭과 물리적 모드분해에 관하여 검토하였다. POD해석의 고유벡터 비교를 통해서 칼만와류는 박리버블에 의해서 거의 영향받지 않지만 칼만와류는 단면후류부에서 박리버블의 발달에 상당히 간섭하고 있음을 확인하 였다. 변장비(B/D=2,34,5) 변화에 따른 ${dC_L/d\alpha}$, ${H_1^{*}}$의 정(+)부(-)의 차이, 즉 갤로핑현상에 대한 안정/불안정성은 박리전단층의 재부착에 깊은 관련이 있는 것으로 판단되며 B/D=3,4에서 시간평균적으로 재부착하던 주위흐름장이 칼만와류의 방출을 제어하면 재부착하지 않는 것으로 생각된다. 즉, 칼만와류의 억제는 후류부에서 박리전단층의 곡률이 작아지도록 간섭하고 단면에 있어서 elongation효과를 나타낸다.

Cinematic PIV 데이터의 3차원 위상평균 기법을 이용한 실린더 후류의 2차 와류 측정 (Measurements of Secondary Vortices in the Cylinder Wake by Three-Dimensional Phase-Averaging Technique Using Cinematic PIV Data)

  • 성재용;유정열
    • 대한기계학회논문집B
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    • 제24권11호
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    • pp.1540-1548
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    • 2000
  • Near-wake flow field downstream of a circular cylinder in the wake-transition regime where fine-scale secondary vortices have a spanwise wavelength of around one diameter has been studied by means of phase-averaging from cinematic PIV data. A cross-correlation algorithm in conjunction with the FFT(Fast Fourier Transform)analysis and an offset correlation technique is used for obtaining the velocity vectors. Which the help of very high sampling rate compared to the shedding frequency, it is possible to obtain phase-averaged flow fields although the shedding is not forced but natural. Phase -locked three-dimensional vortical structures are reconstructed form the phase-averaged data in one x-y(cross-sectional) and several z-x(spanwise-streamwise)planes. In this process of phase-averaging in a z-x plane, a technique to freeze the secondary vortices relative to the centerline is applied. The formation process of the secondary vortices is shown by considering spatial relations between the primary Karman and the secondary vortices and their temporal evolutions.

예선회가 존재하는 회전유동장의 불안정성 수치해석 (Numerical Instability Analysis of the Rotating Boundary-Layer flow Including Pre-Swirl)

  • 황영규;이윤용;이광원
    • 대한기계학회논문집B
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    • 제27권4호
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    • pp.415-423
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    • 2003
  • The hydrodynamic instability of the three-dimensional boundary-layer over a rotating disk has been numerically investigated for these flows; Ro = -1, -0.5, and 0, using linear stability theory. Detailed numerical values of the disturbance wave number. wave frequency. azimuth angle. radius (Reynolds number, Re) and other characteristics have been calculated for the pre-swirl flows. On the basis of Ekman and Karman boundary layer theory, the instability of the pre-swirl flows have been investigated for the unstable criteria. The disturbance will be relatively fast amplified at small fe and within wide bands of wave number compared with previously known Karman boundary-layer results. The flow (Ro =-0.5) is found to be always stable for a disturbance whose dimensionless wave number is greater than 0.9. It has a larger range of unstable interval than Karman boundary layer and can be unstable at smaller Re.