• Title/Summary/Keyword: 주유동 방향 와류

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Large Eddy Simulation of Turbulent Heat Transfer in a Straight Cooling Passage with Various Aspect Ratios (형상비변화에 따른 직선냉각유로에 대한 난류열전달 LES해석)

  • Park, Tae-Seon
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2012.05a
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    • pp.274-277
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    • 2012
  • Large eddy simulation is applied to the turbulent flow and heat transfer in straight cooling passages with varying aspect ratio. The turbulent statistics of the flow and thermal quantities are calculated and the characteristics of Nusselt number are investigated. To scrutinize near-wall streamwise vortices, a conditional sampling technique is adopted. Clockwise and counter-clockwise rotating streamwise vortices are sampled and the probability density function of the vortex circulation Reynolds number and wall Nusselt number are calculated.

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Effect of Secondary Flow Direction on Film Cooling Effectiveness (이차유동의 방향이 막냉각 효율에 미치는 영향)

  • Park, Sehjin;Choi, Seok Min;Sohn, Ho-Seong;Chung, Heeyoon;Cho, Hyung Hee
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.37 no.7
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    • pp.655-663
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    • 2013
  • Several studies of film cooling were accomplished with a secondary flow channel parallel to the main flow. In real turbine blades, however, the direction of the secondary flow channel is generally normal to the main flow. Thus, this study performs a numerical analysis to investigate the effects of the direction of secondary flow on the effectiveness of double-jet film cooling. The blowing ratio is 1 and 2, and the lateral injection angle is $22.5^{\circ}$. The parallel channel case creates a well-developed anti-kidney vortex with a blowing ratio of 1, and the laterally averaged film cooling effectiveness of the parallel channel is enhanced compared to the normal channel. The normal channel shows higher performance with a blowing ratio of 2. Both cases show high film cooling effectiveness. These phenomena can be attributed to a high blowing ratio and flow rate rather than an anti-kidney vortex.

Visualization of Vortex Lock-on to Oscillatory Incident Flow in the Cylinder Wake Using Time-Resolved PIV (고속 PIV계측에 의한 실린더 근접후류 공진 유동 가시화)

  • 송치성
    • Journal of Advanced Marine Engineering and Technology
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    • v.25 no.6
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    • pp.1353-1361
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    • 2001
  • Vortex lock-on or resonance behind a circular cylinder is visualized using a time-resolved PW when a single frequency oscillation is superimposed on the mean incident velocity. For vector processing, a cross-correlation algorithm in conjunction with a recursive correlation and interrogation window shifting techniques is used. Measurements are made of the Karmas and streamwise vertices in the wake-transition regime at Reynolds lumber 360. When lock-on occurs, the vortex shedding frequency is found to be half the oscillation frequency as expected from previous experiments. At the lock-on state, the Karman vortices are observed to be more disordered by the increased strength and spanwise wavelength of the streamwiee vortices, which lead? to a strong three-dimensional motion.

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A Experimental Study on Chracteristics of a Mixed Convection Heat Transfer in a Cavity with upper Channel (상부채널을 갖는 캐비티의 혼합대류 열전달에 관한 실험적연구)

  • Bae, Suk-Tae
    • Solar Energy
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    • v.18 no.2
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    • pp.115-121
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    • 1998
  • In this study a channel cavity flow was performed. The channel has small size in the upper cavity region. At the gap is supplied by driven flow for Reynolds number. The experimental study was carried out in a channel cavity with square heat surface by visualization equipment with Mach-Zehnder interferometer and laser apparatus. Heat source was uniform heat flux($0.4W/cm^2,\;0.8W/cm^2,\;1.2W/cm^2$). When the bottom wall is heated, the tendency of natural convection flows are vigorous increasing heat flux.

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LES for Turbulent Duct Flow with Surface Mass Injection (질량분사가 있는 덕트 난류유동의 LES 해석)

  • Kim, Bo-Hoon;Na, Yang;Lee, Chang-Jin
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.39 no.3
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    • pp.232-241
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    • 2011
  • The hybrid rocket shows interesting characteristics of complicated mixing layer developed by the interaction between turbulent oxidizer flow and injected surface mass flow from fuel vaporization. In this study, the compressible LES was conducted to explore the physical phenomena of surface oscillatory flow induced by the flow interferences in a duct domain. From the numerical results, the wall injection generates the stronger streamwise vorticites and the negative components of axial velocity accompanied with the azimuthal vorticity near the surface. And the vortex shedding with a certain time scale was found to be developed by hydrodynamic instability in the mixing layer. The pressure fluctuations in this calculation exhibit a peculiar peak at a specific angular frequency($\omega$=8.8) representing intrinsic oscillation due to the injection.