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    Discussion: “A Method for Predicting Compressor Cascade Total Pressure Losses When the Inlet Relative Mach Number Is Greater Than Unity” (Balzer, R. L., 1971, ASME J. Eng. Power, 93, pp. 119–124)

    Source: Journal of Engineering for Gas Turbines and Power:;1971:;volume( 093 ):;issue: 001::page 124
    Author:
    E. Boxer
    DOI: 10.1115/1.3445378
    Publisher: The American Society of Mechanical Engineers (ASME)
    keyword(s): Pressure , Mach number , Compressors AND Cascades (Fluid dynamics) ,
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      Discussion: “A Method for Predicting Compressor Cascade Total Pressure Losses When the Inlet Relative Mach Number Is Greater Than Unity” (Balzer, R. L., 1971, ASME J. Eng. Power, 93, pp. 119–124)

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    contributor authorE. Boxer
    date accessioned2017-05-09T00:57:18Z
    date available2017-05-09T00:57:18Z
    date copyrightJanuary, 1971
    date issued1971
    identifier issn1528-8919
    identifier otherJETPEZ-26690#124_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/151278
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDiscussion: “A Method for Predicting Compressor Cascade Total Pressure Losses When the Inlet Relative Mach Number Is Greater Than Unity” (Balzer, R. L., 1971, ASME J. Eng. Power, 93, pp. 119–124)
    typeJournal Paper
    journal volume93
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3445378
    journal fristpage124
    journal lastpage125
    identifier eissn0742-4795
    keywordsPressure
    keywordsMach number
    keywordsCompressors AND Cascades (Fluid dynamics)
    treeJournal of Engineering for Gas Turbines and Power:;1971:;volume( 093 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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