• Title/Summary/Keyword: 헤어핀 보텍스

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Process of Hairpin Vortex Packet Generation in Channel Flows (채널 유동 내에서 헤어핀 보텍스 패킷의 형성 과정)

  • Kim, Kyoung-Youn
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.36 no.8
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    • pp.839-847
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    • 2012
  • Numerical simulations for channel flows with $Re_{\tau}$ = 180, 395 and 590 have been performed to investigate the hairpin packet formation process in wall-bounded turbulent flows. Using direct numerical simulation databases, the initial flow fields are given by the conditionally averaged flow field with the second quadrant event specified at the buffer layer. By tracking the initial vortex development, the change in the initial vortex to an ${\Omega}$-shaped vortex and th generation of a secondary hairpin vortex were found to occur with time scales based on the wall units. In addition, at the time when the initial vortex has grown to the channel center, the inclination angle of the hairpin vortex packet is approximately $12{\sim}14^{\circ}$, which is similar for all three Reynolds numbers. Finally, numerical simulations of the evolution of two adjacent hairpin vortices have been performed to examine the interaction between the adjacent vortex packets.

Aerodynamic Property of Swallowtail Butterfly Wing in Gliding (글라이딩하는 제비나비 날개형상의 공력특성연구)

  • Lee, Byoung-Do;Park, Hyung-Min;Choi, Hae-Cheon
    • Proceedings of the KSME Conference
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    • 2007.05a
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    • pp.395-398
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    • 2007
  • In nature, the swallowtail butterfly is known to be a versatile flyer using gliding and flapping efficiently. Furthermore, it has long tails on the hind-wing that may be associated with the enhancement of the gliding performance. In the present study, we investigate the aerodynamic property of swallowtail butterfly wing in gliding. We use an immersed boundary method and conduct a numerical simulation at the Reynolds numbers of 1,000 - 3,000 based on the free-stream velocity and the averaged chord length for seven different attack angles. As a result, we clearly identify the existence of the wing-tip and leading-edge vortices, and a pair of the streamwise vortices generated along the hind-wing tails. Interestingly, at the attack angle of $10^{\circ},$ hairpin vortices are generated above the center of the body and travel downstream.

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Reynolds Shear Stress Distribution in Turbulent Channel Flows (난류 채널 유동 내부의 레이놀즈 전단 응력 분포)

  • Kim, Kyoung-Youn
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.36 no.8
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    • pp.829-837
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    • 2012
  • Direct numerical simulations were carried out for turbulent channel flows with $Re_{\tau}$ = 180, 395 and 590 to investigate the turbulent flow structure related to the Reynolds shear stress. By examining the probability density function, the second quadrant (Q2) events with the largest contribution to the mean Reynolds shear stress were identified. The change in the inclination angle of Q2 events varies with wall units in $y^+<50$ and with the channel half height in y/h > 0.5. Conditionally averaged flow fields for the Q2 event show that the flow structures associated with Reynolds shear stress are a quasi-streamwise vortex in the buffer layer and a hairpin-shaped vortex in the outer layer. Three-dimensional visualization of the distribution of high Reynolds shear stress reveals that the organization of hairpin vortices in the outer layer having a size of 1.5~3 h is associated with large-scale motions with high Reynolds shear stress in the outer layer.