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    A Conceptual Design Methodology for Predicting Bleed and Horsepower Requirements of Military Aircraft Engines

    Source: Journal of Engineering for Gas Turbines and Power:;1996:;volume( 118 ):;issue: 003::page 481
    Author:
    J. D. Cyrus
    DOI: 10.1115/1.2816671
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Conceptual design codes have been developed to provide conceptual design estimates of bleed and horsepower extraction requirements of advanced military aircraft. This paper describes the methodology for the computer codes. The validity of the models was assessed by generating bleed and horsepower estimates for four advanced air-craft configurations not included in the data base and comparing the model estimates to manufacturer’s estimates.
    keyword(s): Engines , Horsepower , Military aircraft , Conceptual design , Computers AND Databases ,
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      A Conceptual Design Methodology for Predicting Bleed and Horsepower Requirements of Military Aircraft Engines

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/116892
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    contributor authorJ. D. Cyrus
    date accessioned2017-05-08T23:50:01Z
    date available2017-05-08T23:50:01Z
    date copyrightJuly, 1996
    date issued1996
    identifier issn1528-8919
    identifier otherJETPEZ-26756#481_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/116892
    description abstractConceptual design codes have been developed to provide conceptual design estimates of bleed and horsepower extraction requirements of advanced military aircraft. This paper describes the methodology for the computer codes. The validity of the models was assessed by generating bleed and horsepower estimates for four advanced air-craft configurations not included in the data base and comparing the model estimates to manufacturer’s estimates.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Conceptual Design Methodology for Predicting Bleed and Horsepower Requirements of Military Aircraft Engines
    typeJournal Paper
    journal volume118
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2816671
    journal fristpage481
    journal lastpage485
    identifier eissn0742-4795
    keywordsEngines
    keywordsHorsepower
    keywordsMilitary aircraft
    keywordsConceptual design
    keywordsComputers AND Databases
    treeJournal of Engineering for Gas Turbines and Power:;1996:;volume( 118 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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