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    Longitudinal Strain Pulse Propagation in Wide Rectangular Bars: Part 2—Experimental Observations and Comparisons With Theory

    Source: Journal of Applied Mechanics:;1963:;volume( 030 ):;issue: 001::page 61
    Author:
    O. E. Jones
    ,
    A. T. Ellis
    DOI: 10.1115/1.3630106
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The plane-stress theory presented in Part 1 is shown to predict qualitatively the warping of plane sections observed in transient fringe patterns obtained using birefringent coatings and in dynamic photoelastic pictures obtained in other investigations. Measurements using conventional techniques are described in which wide rectangular bars were subjected to a longitudinal step-function pressure loading produced by a shock tube. Comparisons show that the gross features of the experimental records for the head of the pulse are qualitatively predicted by the theory. Both theory and experiment show that short-wavelength, second-mode disturbances arrive very early. Experimentally it is observed that these disturbances are accomplished by thickness-mode activity which cannot be accounted for by the plane-stress theory.
    keyword(s): Pressure , Wavelength , Coatings , Measurement , Stress , Diffraction patterns , Warping , Shock tubes AND Thickness ,
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      Longitudinal Strain Pulse Propagation in Wide Rectangular Bars: Part 2—Experimental Observations and Comparisons With Theory

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/93923
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    contributor authorO. E. Jones
    contributor authorA. T. Ellis
    date accessioned2017-05-08T23:09:58Z
    date available2017-05-08T23:09:58Z
    date copyrightMarch, 1963
    date issued1963
    identifier issn0021-8936
    identifier otherJAMCAV-25700#61_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/93923
    description abstractThe plane-stress theory presented in Part 1 is shown to predict qualitatively the warping of plane sections observed in transient fringe patterns obtained using birefringent coatings and in dynamic photoelastic pictures obtained in other investigations. Measurements using conventional techniques are described in which wide rectangular bars were subjected to a longitudinal step-function pressure loading produced by a shock tube. Comparisons show that the gross features of the experimental records for the head of the pulse are qualitatively predicted by the theory. Both theory and experiment show that short-wavelength, second-mode disturbances arrive very early. Experimentally it is observed that these disturbances are accomplished by thickness-mode activity which cannot be accounted for by the plane-stress theory.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleLongitudinal Strain Pulse Propagation in Wide Rectangular Bars: Part 2—Experimental Observations and Comparisons With Theory
    typeJournal Paper
    journal volume30
    journal issue1
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.3630106
    journal fristpage61
    journal lastpage69
    identifier eissn1528-9036
    keywordsPressure
    keywordsWavelength
    keywordsCoatings
    keywordsMeasurement
    keywordsStress
    keywordsDiffraction patterns
    keywordsWarping
    keywordsShock tubes AND Thickness
    treeJournal of Applied Mechanics:;1963:;volume( 030 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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