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    An Approximate Analysis of the Influence of Aerodynamic Heating and Initial Twist on the Torsional Stiffness of Thin Wings

    Source: Journal of Applied Mechanics:;1960:;volume( 027 ):;issue: 002::page 332
    Author:
    Lit S. Han
    DOI: 10.1115/1.3643961
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In the present paper, approximate formulas are derived, based on the “fiber-stress” concept, for the combined influence of aerodynamic heating and initial twist on the torsional stiffness of a thin wing. Criteria are established for calculating the critical temperature difference between that of the edges and that of the mid-chord position, for preventing possible aeroelastic reversals or buckling. Formulas are valid for wings with large aspect ratios.
    keyword(s): Stiffness , Wings , Heating , Formulas , Temperature , Fibers , Stress , Chords (Trusses) AND Buckling ,
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      An Approximate Analysis of the Influence of Aerodynamic Heating and Initial Twist on the Torsional Stiffness of Thin Wings

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    http://yetl.yabesh.ir/yetl1/handle/yetl/90723
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    contributor authorLit S. Han
    date accessioned2017-05-08T23:04:17Z
    date available2017-05-08T23:04:17Z
    date copyrightJune, 1960
    date issued1960
    identifier issn0021-8936
    identifier otherJAMCAV-25541#332_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/90723
    description abstractIn the present paper, approximate formulas are derived, based on the “fiber-stress” concept, for the combined influence of aerodynamic heating and initial twist on the torsional stiffness of a thin wing. Criteria are established for calculating the critical temperature difference between that of the edges and that of the mid-chord position, for preventing possible aeroelastic reversals or buckling. Formulas are valid for wings with large aspect ratios.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAn Approximate Analysis of the Influence of Aerodynamic Heating and Initial Twist on the Torsional Stiffness of Thin Wings
    typeJournal Paper
    journal volume27
    journal issue2
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.3643961
    journal fristpage332
    journal lastpage334
    identifier eissn1528-9036
    keywordsStiffness
    keywordsWings
    keywordsHeating
    keywordsFormulas
    keywordsTemperature
    keywordsFibers
    keywordsStress
    keywordsChords (Trusses) AND Buckling
    treeJournal of Applied Mechanics:;1960:;volume( 027 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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