Fluid Flow and Heat Transfer Around a Circular Cylinder with Vortex Generators
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概要
- 論文の詳細を見る
Experimental studies on the fluid flow and heat transfer around a circular cylinder with vortex generators were carried out in the range 1.3×10^4<__=Re<__=5.2×10^4. Depending on the height of the vortex generator and the Reynolds number, four flow patterns were found to result from the transition of the boundary layer and the flow separation. The local and average heat transfer coefficients on the rear surface vary with changes in the drag coefficient, the rms fluctuating pressure and the reciprocal of the Strouhal number. The heat transfer coefficients at the rear stagnation point, h_r, for the four patterns are related to the Strouhal number as Nu_r/Re^<2/3>=0.018/S^<1.4>, within an error of 10%, and also to the rms fluctuating pressure, Δp_r, at the rear stagnation point as : h_<r∝>Δp_r^<0.31>.
- 一般社団法人日本機械学会の論文
- 1988-11-15
著者
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Iida Yasuhisa
Defense Facilities Administration Agency
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IGARASHI Tamotsu
The National Defense Academy
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Igarashi Tamotsu
The National Defence Academy
関連論文
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- Characteristics of the Flow around Two Circular Cylinders Arranged in Tandem : 2nd Report, Unique Phenomenon at Small Spacing
- Characteristics of the Flow around Rectangular Cylinders : The Case of the Angle of Attack 0 Deg
- Characteristics of the Flow around a Square Prism
- Fluid Flow and Heat Transfer around Rectangular Cylinders : The Case of a Width/Height Ratio of a Section of 2.0〜4.0
- Characteristics of the Flow around Three Circular Cylinders
- Characteristics of a Flow around Two Circular Cylinders of Different Diameters Arranged in Tandem
- Characteristics of the Flow around Two Circular Cylinders Arranged in Tandem : 1st Report
- Flow Characteristics around a Circular Cylinder with a Slit : 2nd Report, Effect of Boundary Layer Suction
- Effect of Tripping Wires on the Flow around a Circular Cylinder Normal to an Airstream