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    Linearized Theory of Supercavitating Hydrofoils in Subsonic Liquid Flow

    Source: Journal of Fluids Engineering:;1977:;volume( 099 ):;issue: 002::page 311
    Author:
    Tetsuo Nishiyama
    DOI: 10.1115/1.3448754
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In order to clarify the compressibility effect, the perturbed flow field of the supercavitating hydrofoil in subsonic region is examined by a linearized technique and, as a result, the general corresponding rule of the compressible flow to the incompressible one is proposed to obtain the characteristics of the supercavitating hydrofoil. The main contents are summarized as follows: (i ) Basic relations between velocity, pressure, and sound speed are shown in subsonic liquid flow within the framework of linearization. (ii ) The correspondence of the steady, characteristics of the two and three dimensional supercavitating hydrofoils in subsonic liquid flow to ones in incompressible flow is clarified. Hence we can readily calculate the characteristics by simple correction to ones in incompressible flow. (iii ) Numerical calculations are made to show the essential differences of the compressibility effect between liquid and gas flow, and also the interrelated effect between cavitation number and Mach number on the characteristics of the supercavitating hydrofoils.
    keyword(s): Flow (Dynamics) , Hydrofoil , Compressibility , Pressure , Mach number , Sound , Gas flow , Cavitation AND Compressible flow ,
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      Linearized Theory of Supercavitating Hydrofoils in Subsonic Liquid Flow

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/90050
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    • Journal of Fluids Engineering

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    contributor authorTetsuo Nishiyama
    date accessioned2017-05-08T23:03:11Z
    date available2017-05-08T23:03:11Z
    date copyrightJune, 1977
    date issued1977
    identifier issn0098-2202
    identifier otherJFEGA4-26915#311_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/90050
    description abstractIn order to clarify the compressibility effect, the perturbed flow field of the supercavitating hydrofoil in subsonic region is examined by a linearized technique and, as a result, the general corresponding rule of the compressible flow to the incompressible one is proposed to obtain the characteristics of the supercavitating hydrofoil. The main contents are summarized as follows: (i ) Basic relations between velocity, pressure, and sound speed are shown in subsonic liquid flow within the framework of linearization. (ii ) The correspondence of the steady, characteristics of the two and three dimensional supercavitating hydrofoils in subsonic liquid flow to ones in incompressible flow is clarified. Hence we can readily calculate the characteristics by simple correction to ones in incompressible flow. (iii ) Numerical calculations are made to show the essential differences of the compressibility effect between liquid and gas flow, and also the interrelated effect between cavitation number and Mach number on the characteristics of the supercavitating hydrofoils.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleLinearized Theory of Supercavitating Hydrofoils in Subsonic Liquid Flow
    typeJournal Paper
    journal volume99
    journal issue2
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.3448754
    journal fristpage311
    journal lastpage318
    identifier eissn1528-901X
    keywordsFlow (Dynamics)
    keywordsHydrofoil
    keywordsCompressibility
    keywordsPressure
    keywordsMach number
    keywordsSound
    keywordsGas flow
    keywordsCavitation AND Compressible flow
    treeJournal of Fluids Engineering:;1977:;volume( 099 ):;issue: 002
    contenttypeFulltext
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