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- W1964929618 abstract "Experimental studies on drag reduction of a circular cylinder of diameter D were conducted in the subcritical flow regime at Reynolds numbers in the range <TEX>$4{times}10^4{leq}Re{leq}10^5$</TEX>. To shield the cylinder rear surface from the pressure deficit of the unsteady vortex generation in the near wake, two shield plates were attached downstream of the separation points to form a cavity at the base region. The chord of the shield plates, L, ranged from 0.22 to 1.52 D and the cavity width, G, was in the range from 0 to 0.96 D. It is concluded that significant drag reductions from that of a plain cylinder may be achieved by proper sizing of the shield plates and the base cavity. The study shows that using a pair of shield plates at G/D of 0.86 and angular position <TEX>${theta}$</TEX> of <TEX>${pm}121^{circ}$</TEX> results in a configuration with percentage drag reduction of 40% for L/D of 0.5, and 55% for L/D of 1.0." @default.
- W1964929618 created "2016-06-24" @default.
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- W1964929618 date "2003-10-25" @default.
- W1964929618 modified "2023-09-26" @default.
- W1964929618 title "Drag reduction of a circular cylinder at subcritical flow regime using base shield plates" @default.
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- W1964929618 doi "https://doi.org/10.12989/was.2003.6.5.347" @default.
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