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    An Experimental Investigation of Aspect Ratio and Incidence Angle Effects for the Flow Around Surface Mounted Finite Height Square Prisms

    Source: Journal of Fluids Engineering:;2014:;volume( 136 ):;issue: 008::page 81206
    Author:
    McClean, J. F.
    ,
    Sumner, D.
    DOI: 10.1115/1.4027138
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The flow around a surfacemounted finiteheight square prism was investigated using a lowspeed wind tunnel. The experiments were conducted at a Reynolds number of Re = 7.3 أ— 104 for prism aspect ratios of AR = 3, 5, 7, 9, and 11 and incidence angles from خ±â€‰= 0 deg to 45 deg. The thickness of the boundary layer on the ground plane relative to the side length was خ´/D = 1.5. Measurements of the vortex shedding frequency were made with a singlecomponent hotwire probe, and measurements of the mean drag and lift forces were obtained with a force balance. For all aspect ratios and incidence angles, the mean drag coefficient and Strouhal number were lower than those of an infinite prism, while the mean lift coefficient was of nearly similar magnitude. As the aspect ratio was increased from AR = 3 to 11, the force coefficients and Strouhal number slowly approached the infinitesquareprism data. The mean drag coefficient and Strouhal number for the finite prism were less sensitive to changes in incidence angle compared to the infinite square prism. The critical incidence angle, corresponding to minimum mean drag coefficient, minimum (most negative) mean lift coefficient, and maximum Strouhal number, shifted to a higher incidence angle compared to the infinite square prism, with values ranging from خ±critical = 15 deg to 18 deg; this shift was greatest for the prisms of higher aspect ratio. The behavior of the force coefficients and Strouhal number for the prism of AR = 3 was distinct from the other prisms (with lower values of mean drag coefficient and mean lift coefficient magnitude, and a different Strouhal number trend), suggesting the critical aspect ratio was between AR = 5 and AR = 3 in these experiments. In the wallnormal direction, the power spectra for AR = 11 and 9 tended to have weaker and/or more broadbanded vortex shedding peaks near the ground plane and near the free end at خ±â€‰= 0 deg and 15 deg. For AR = 7 to 3, welldefined vortex shedding peaks were detected along the entire height of the prisms. For AR = 11 and 9, at خ±â€‰= 30 deg and 45 deg, vortex shedding peaks were absent in the power spectra in the upper part of the wake.
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      An Experimental Investigation of Aspect Ratio and Incidence Angle Effects for the Flow Around Surface Mounted Finite Height Square Prisms

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    http://yetl.yabesh.ir/yetl1/handle/yetl/155032
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    contributor authorMcClean, J. F.
    contributor authorSumner, D.
    date accessioned2017-05-09T01:08:41Z
    date available2017-05-09T01:08:41Z
    date issued2014
    identifier issn0098-2202
    identifier otherfe_136_08_081206.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/155032
    description abstractThe flow around a surfacemounted finiteheight square prism was investigated using a lowspeed wind tunnel. The experiments were conducted at a Reynolds number of Re = 7.3 أ— 104 for prism aspect ratios of AR = 3, 5, 7, 9, and 11 and incidence angles from خ±â€‰= 0 deg to 45 deg. The thickness of the boundary layer on the ground plane relative to the side length was خ´/D = 1.5. Measurements of the vortex shedding frequency were made with a singlecomponent hotwire probe, and measurements of the mean drag and lift forces were obtained with a force balance. For all aspect ratios and incidence angles, the mean drag coefficient and Strouhal number were lower than those of an infinite prism, while the mean lift coefficient was of nearly similar magnitude. As the aspect ratio was increased from AR = 3 to 11, the force coefficients and Strouhal number slowly approached the infinitesquareprism data. The mean drag coefficient and Strouhal number for the finite prism were less sensitive to changes in incidence angle compared to the infinite square prism. The critical incidence angle, corresponding to minimum mean drag coefficient, minimum (most negative) mean lift coefficient, and maximum Strouhal number, shifted to a higher incidence angle compared to the infinite square prism, with values ranging from خ±critical = 15 deg to 18 deg; this shift was greatest for the prisms of higher aspect ratio. The behavior of the force coefficients and Strouhal number for the prism of AR = 3 was distinct from the other prisms (with lower values of mean drag coefficient and mean lift coefficient magnitude, and a different Strouhal number trend), suggesting the critical aspect ratio was between AR = 5 and AR = 3 in these experiments. In the wallnormal direction, the power spectra for AR = 11 and 9 tended to have weaker and/or more broadbanded vortex shedding peaks near the ground plane and near the free end at خ±â€‰= 0 deg and 15 deg. For AR = 7 to 3, welldefined vortex shedding peaks were detected along the entire height of the prisms. For AR = 11 and 9, at خ±â€‰= 30 deg and 45 deg, vortex shedding peaks were absent in the power spectra in the upper part of the wake.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAn Experimental Investigation of Aspect Ratio and Incidence Angle Effects for the Flow Around Surface Mounted Finite Height Square Prisms
    typeJournal Paper
    journal volume136
    journal issue8
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.4027138
    journal fristpage81206
    journal lastpage81206
    identifier eissn1528-901X
    treeJournal of Fluids Engineering:;2014:;volume( 136 ):;issue: 008
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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