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    Aerodynamic Approximations for Unsteady Supersonic Flow Through Ducts of Revolution

    Source: Journal of Manufacturing Science and Engineering:;1972:;volume( 094 ):;issue: 001::page 95
    Author:
    R. A. Skop
    ,
    R. E. Kaplan
    DOI: 10.1115/1.3428162
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Supersonic flow of a perfect, inviscid gas through a finite, flexible duct of revolution is considered. Internal equivalents to Lighthill’s piston theory and Ackeret’s strip theory are derived and compared. The comparison shows that for low reduced frequencies of the duct wall the two internal theories coincide. Using “internal strip theory”, the flutter bounds for a circular cylindrical duct are calculated. The results demonstrate that, as the effective duct aspect ratio becomes large, the flutter bounds are asymptotic to those predicted by using classical strip theory for internal flow.
    keyword(s): Approximation , Ducts , Supersonic flow , Strips , Flutter (Aerodynamics) , Internal flow , Frequency AND Pistons ,
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      Aerodynamic Approximations for Unsteady Supersonic Flow Through Ducts of Revolution

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/163196
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    • Journal of Manufacturing Science and Engineering

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    contributor authorR. A. Skop
    contributor authorR. E. Kaplan
    date accessioned2017-05-09T01:35:18Z
    date available2017-05-09T01:35:18Z
    date copyrightFebruary, 1972
    date issued1972
    identifier issn1087-1357
    identifier otherJMSEFK-27570#95_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/163196
    description abstractSupersonic flow of a perfect, inviscid gas through a finite, flexible duct of revolution is considered. Internal equivalents to Lighthill’s piston theory and Ackeret’s strip theory are derived and compared. The comparison shows that for low reduced frequencies of the duct wall the two internal theories coincide. Using “internal strip theory”, the flutter bounds for a circular cylindrical duct are calculated. The results demonstrate that, as the effective duct aspect ratio becomes large, the flutter bounds are asymptotic to those predicted by using classical strip theory for internal flow.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAerodynamic Approximations for Unsteady Supersonic Flow Through Ducts of Revolution
    typeJournal Paper
    journal volume94
    journal issue1
    journal titleJournal of Manufacturing Science and Engineering
    identifier doi10.1115/1.3428162
    journal fristpage95
    journal lastpage102
    identifier eissn1528-8935
    keywordsApproximation
    keywordsDucts
    keywordsSupersonic flow
    keywordsStrips
    keywordsFlutter (Aerodynamics)
    keywordsInternal flow
    keywordsFrequency AND Pistons
    treeJournal of Manufacturing Science and Engineering:;1972:;volume( 094 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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