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    Air Flow and Particle Trajectories around Aircraft Fuselages. Part III: Extensions to Particles of Arbitrary Shape

    Source: Journal of Atmospheric and Oceanic Technology:;1985:;volume( 002 ):;issue: 004::page 539
    Author:
    King, W. D.
    DOI: 10.1175/1520-0426(1985)002<0539:AFAPTA>2.0.CO;2
    Publisher: American Meteorological Society
    Abstract: Earlier work that produced generalized rules for obtaining trajectories of water droplets moving around aircraft fuselages has been extended to cover the case for particles of arbitrary shape. The parameters determining the major features of the trajectories are the fuselage radius and a generalized Stokes number that can be used to calculate an equivalent water drop size for particles of arbitrary shape and density. As for water drops, the maximum width of the shadow zone for sampling the particles is about one-fifth of the fuselage radius, and it occurs for those in columns and plates of typical densities whose major dimensions are about 600 ?m and 2 mm, respectively.
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      Air Flow and Particle Trajectories around Aircraft Fuselages. Part III: Extensions to Particles of Arbitrary Shape

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4150845
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    contributor authorKing, W. D.
    date accessioned2017-06-09T14:13:48Z
    date available2017-06-09T14:13:48Z
    date copyright1985/12/01
    date issued1985
    identifier issn0739-0572
    identifier otherams-152.pdf
    identifier urihttp://onlinelibrary.yabesh.ir/handle/yetl/4150845
    description abstractEarlier work that produced generalized rules for obtaining trajectories of water droplets moving around aircraft fuselages has been extended to cover the case for particles of arbitrary shape. The parameters determining the major features of the trajectories are the fuselage radius and a generalized Stokes number that can be used to calculate an equivalent water drop size for particles of arbitrary shape and density. As for water drops, the maximum width of the shadow zone for sampling the particles is about one-fifth of the fuselage radius, and it occurs for those in columns and plates of typical densities whose major dimensions are about 600 ?m and 2 mm, respectively.
    publisherAmerican Meteorological Society
    titleAir Flow and Particle Trajectories around Aircraft Fuselages. Part III: Extensions to Particles of Arbitrary Shape
    typeJournal Paper
    journal volume2
    journal issue4
    journal titleJournal of Atmospheric and Oceanic Technology
    identifier doi10.1175/1520-0426(1985)002<0539:AFAPTA>2.0.CO;2
    journal fristpage539
    journal lastpage547
    treeJournal of Atmospheric and Oceanic Technology:;1985:;volume( 002 ):;issue: 004
    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
    yabeshDSpacePersian