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    The Optimum Design of a Cavitator for High Speed Axisymmetric Bodies in Partially Cavitating Flows

    Source: Journal of Fluids Engineering:;2013:;volume( 135 ):;issue: 001::page 11301
    Author:
    Rashidi, I.
    ,
    Passandideh
    ,
    Pasandideh
    DOI: 10.1115/1.4023078
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper, the partially cavitating flow over an axisymmetric projectile is studied in order to obtain the optimum cavitator such that, at a given cavitation number, the total drag coefficient of the projectile is minimum. For this purpose, the boundary element method and numerical simulations are used. A large number of cavitator profiles are produced using a parabolic expression with three geometric parameters. The potential flow around these cavitators is then solved using the boundary element method. In order to examine the optimization results, several cavitators with a total drag coefficient close to that of the optimum cavitators are also numerically simulated. Eventually, the optimum cavitator is selected using both the boundary element method and numerical simulations. The effects of the body radius and the length of the conical section of the projectile on the shape of the optimized cavitator are also investigated. The results show that for all cavitation numbers, the cavitator that creates a cavity covering the entire conical section of the projectile with a minimum total drag coefficient is optimal. It can be seen that increasing the cavitation number causes the optimum cavitator to approach the disk cavitator. The results also show that at a fixed cavitation number, the increase in both the radius and length of the conical section causes the cavitator shape to approach that of the disk cavitator.
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      The Optimum Design of a Cavitator for High Speed Axisymmetric Bodies in Partially Cavitating Flows

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    https://yetl.yabesh.ir/yetl1/handle/yetl/151880
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    contributor authorRashidi, I.
    contributor authorPassandideh
    contributor authorPasandideh
    date accessioned2017-05-09T00:59:04Z
    date available2017-05-09T00:59:04Z
    date issued2013
    identifier issn0098-2202
    identifier otherfe_135_1_011301.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/151880
    description abstractIn this paper, the partially cavitating flow over an axisymmetric projectile is studied in order to obtain the optimum cavitator such that, at a given cavitation number, the total drag coefficient of the projectile is minimum. For this purpose, the boundary element method and numerical simulations are used. A large number of cavitator profiles are produced using a parabolic expression with three geometric parameters. The potential flow around these cavitators is then solved using the boundary element method. In order to examine the optimization results, several cavitators with a total drag coefficient close to that of the optimum cavitators are also numerically simulated. Eventually, the optimum cavitator is selected using both the boundary element method and numerical simulations. The effects of the body radius and the length of the conical section of the projectile on the shape of the optimized cavitator are also investigated. The results show that for all cavitation numbers, the cavitator that creates a cavity covering the entire conical section of the projectile with a minimum total drag coefficient is optimal. It can be seen that increasing the cavitation number causes the optimum cavitator to approach the disk cavitator. The results also show that at a fixed cavitation number, the increase in both the radius and length of the conical section causes the cavitator shape to approach that of the disk cavitator.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Optimum Design of a Cavitator for High Speed Axisymmetric Bodies in Partially Cavitating Flows
    typeJournal Paper
    journal volume135
    journal issue1
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.4023078
    journal fristpage11301
    journal lastpage11301
    identifier eissn1528-901X
    treeJournal of Fluids Engineering:;2013:;volume( 135 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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