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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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