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    Experimental Investigation of Morel’s Method for Wind Tunnel Contractions

    Source: Journal of Fluids Engineering:;1988:;volume( 110 ):;issue: 001::page 45
    Author:
    E. G. Tulapurkara
    ,
    V. V. K. Bhalla
    DOI: 10.1115/1.3243508
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Based on a numerical study of the potential flow through contractions of chosen geometry, Morel (1975) has given a method to obtain the shape of contraction which gives small adverse pressure gradients and low nonuniformity in the velocity distribution at the exit. Two contractions with area ratios of 12 and 3.464 designed using this method are investigated experimentally. It is found that there is no separation of flow, the thickness of the boundary layer at the exit is small and the nonuniformity in velocity at the exit is smaller than the predicted value.
    keyword(s): Flow (Dynamics) , Separation (Technology) , Boundary layers , Geometry , Pressure gradient , Shapes , Thickness AND Wind tunnels ,
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      Experimental Investigation of Morel’s Method for Wind Tunnel Contractions

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    https://yetl.yabesh.ir/yetl1/handle/yetl/104078
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    • Journal of Fluids Engineering

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    contributor authorE. G. Tulapurkara
    contributor authorV. V. K. Bhalla
    date accessioned2017-05-08T23:27:30Z
    date available2017-05-08T23:27:30Z
    date copyrightMarch, 1988
    date issued1988
    identifier issn0098-2202
    identifier otherJFEGA4-27033#45_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/104078
    description abstractBased on a numerical study of the potential flow through contractions of chosen geometry, Morel (1975) has given a method to obtain the shape of contraction which gives small adverse pressure gradients and low nonuniformity in the velocity distribution at the exit. Two contractions with area ratios of 12 and 3.464 designed using this method are investigated experimentally. It is found that there is no separation of flow, the thickness of the boundary layer at the exit is small and the nonuniformity in velocity at the exit is smaller than the predicted value.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleExperimental Investigation of Morel’s Method for Wind Tunnel Contractions
    typeJournal Paper
    journal volume110
    journal issue1
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.3243508
    journal fristpage45
    journal lastpage47
    identifier eissn1528-901X
    keywordsFlow (Dynamics)
    keywordsSeparation (Technology)
    keywordsBoundary layers
    keywordsGeometry
    keywordsPressure gradient
    keywordsShapes
    keywordsThickness AND Wind tunnels
    treeJournal of Fluids Engineering:;1988:;volume( 110 ):;issue: 001
    contenttypeFulltext
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