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    Computation of Three-Dimensional Flow Fields Through Rotating Blade Rows and Comparison With Experiment

    Source: Journal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 002::page 394
    Author:
    K. P. Sarathy
    DOI: 10.1115/1.3227291
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A three-dimensional inviscid time-marching calculation solving the unsteady Euler equations in a coordinate system rotating with the blade row has been developed, based on the Denton flow solver. This calculation was used to compute the flow field through the rotor of a transonic axial compressor and compared to measurements made with an advanced laser velocimeter at DFVLR. The comparison is made at design speed at pressure ratio corresponding to peak efficiency. Comparisons of the calculated and experimentally determined Mach number contours indicate excellent agreement in the entrance region where the viscous blockage effects are small. The methodology of the analysis is also described in this paper.
    keyword(s): Flow (Dynamics) , Computation , Rotating blades , Pressure , Entrance region , Equations , Mach number , Lasers , Measurement , Compressors , Velocimeters , Design , Rotors AND Blades ,
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      Computation of Three-Dimensional Flow Fields Through Rotating Blade Rows and Comparison With Experiment

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/95803
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorK. P. Sarathy
    date accessioned2017-05-08T23:13:16Z
    date available2017-05-08T23:13:16Z
    date copyrightApril, 1982
    date issued1982
    identifier issn1528-8919
    identifier otherJETPEZ-26772#394_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/95803
    description abstractA three-dimensional inviscid time-marching calculation solving the unsteady Euler equations in a coordinate system rotating with the blade row has been developed, based on the Denton flow solver. This calculation was used to compute the flow field through the rotor of a transonic axial compressor and compared to measurements made with an advanced laser velocimeter at DFVLR. The comparison is made at design speed at pressure ratio corresponding to peak efficiency. Comparisons of the calculated and experimentally determined Mach number contours indicate excellent agreement in the entrance region where the viscous blockage effects are small. The methodology of the analysis is also described in this paper.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleComputation of Three-Dimensional Flow Fields Through Rotating Blade Rows and Comparison With Experiment
    typeJournal Paper
    journal volume104
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3227291
    journal fristpage394
    journal lastpage400
    identifier eissn0742-4795
    keywordsFlow (Dynamics)
    keywordsComputation
    keywordsRotating blades
    keywordsPressure
    keywordsEntrance region
    keywordsEquations
    keywordsMach number
    keywordsLasers
    keywordsMeasurement
    keywordsCompressors
    keywordsVelocimeters
    keywordsDesign
    keywordsRotors AND Blades
    treeJournal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 002
    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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