YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASME
    • Journal of Turbomachinery
    • View Item
    •   YE&T Library
    • ASME
    • Journal of Turbomachinery
    • View Item
    • All Fields
    • Source Title
    • Year
    • Publisher
    • Title
    • Subject
    • Author
    • DOI
    • ISBN
    Advanced Search
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Archive

    NASA Low-Speed Centrifugal Compressor for Three-Dimensional Viscous Code Assessment and Fundamental Flow Physics Research

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 002::page 295
    Author:
    M. D. Hathaway
    ,
    J. R. Wood
    ,
    C. A. Wasserbauer
    DOI: 10.1115/1.2929143
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A low-speed centrifugal compressor facility recently built by the NASA Lewis Research Center is described. The purpose of this facility is to obtain detailed flow field measurements for computational fluid dynamic code assessment and flow physics modeling in support of Army and NASA efforts to advance small gas turbine engine technology. The facility is heavily instrumented with pressure and temperature probes, in both the stationary and rotating frames of reference, and has provisions for flow visualization and laser velocimetry. The facility will accommodate rotational speeds to 2400 rpm and is rated at pressures to 1.25 atm. The initial compressor stage being tested is geometrically and dynamically representative of modern high-performance centrifugal compressor stages with the exception of Mach number levels. Preliminary experimental investigations of inlet and exit flow uniformity and measurement repeatability are presented. These results demonstrate the high quality of the data that may be expected from this facility. The significance of synergism between computational fluid dynamic analyses and experimentation throughout the development of the low-speed centrifugal compressor facility is demonstrated.
    keyword(s): Flow (Dynamics) , Physics , Compressors , Computational fluid dynamics , Gas turbines , Modeling , Laser velocimetry , Probes , Army , Flow visualization , Pressure , Mach number , Temperature AND Measurement ,
    • Download: (1.692Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      NASA Low-Speed Centrifugal Compressor for Three-Dimensional Viscous Code Assessment and Fundamental Flow Physics Research

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/111089
    Collections
    • Journal of Turbomachinery

    Show full item record

    contributor authorM. D. Hathaway
    contributor authorJ. R. Wood
    contributor authorC. A. Wasserbauer
    date accessioned2017-05-08T23:39:54Z
    date available2017-05-08T23:39:54Z
    date copyrightApril, 1992
    date issued1992
    identifier issn0889-504X
    identifier otherJOTUEI-28619#295_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/111089
    description abstractA low-speed centrifugal compressor facility recently built by the NASA Lewis Research Center is described. The purpose of this facility is to obtain detailed flow field measurements for computational fluid dynamic code assessment and flow physics modeling in support of Army and NASA efforts to advance small gas turbine engine technology. The facility is heavily instrumented with pressure and temperature probes, in both the stationary and rotating frames of reference, and has provisions for flow visualization and laser velocimetry. The facility will accommodate rotational speeds to 2400 rpm and is rated at pressures to 1.25 atm. The initial compressor stage being tested is geometrically and dynamically representative of modern high-performance centrifugal compressor stages with the exception of Mach number levels. Preliminary experimental investigations of inlet and exit flow uniformity and measurement repeatability are presented. These results demonstrate the high quality of the data that may be expected from this facility. The significance of synergism between computational fluid dynamic analyses and experimentation throughout the development of the low-speed centrifugal compressor facility is demonstrated.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleNASA Low-Speed Centrifugal Compressor for Three-Dimensional Viscous Code Assessment and Fundamental Flow Physics Research
    typeJournal Paper
    journal volume114
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2929143
    journal fristpage295
    journal lastpage303
    identifier eissn1528-8900
    keywordsFlow (Dynamics)
    keywordsPhysics
    keywordsCompressors
    keywordsComputational fluid dynamics
    keywordsGas turbines
    keywordsModeling
    keywordsLaser velocimetry
    keywordsProbes
    keywordsArmy
    keywordsFlow visualization
    keywordsPressure
    keywordsMach number
    keywordsTemperature AND Measurement
    treeJournal of Turbomachinery:;1992:;volume( 114 ):;issue: 002
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian