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contributor authorVictor Birman
date accessioned2017-05-08T21:15:53Z
date available2017-05-08T21:15:53Z
date copyrightJanuary 1997
date issued1997
identifier other%28asce%290893-1321%281997%2910%3A1%2838%29.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44844
description abstractThe paper presents a methodology that can be employed in numerical and analytical analyses of composite plates subjected to the action of a laser beam. The problem is related both to protection of composite components of aerospace structures from hostile high-energy laser weapons as well as to drilling holes in composites using a laser. In both cases, a three-dimensional state of stresses in the vicinity of the focal spot (the contact zone where the structure-laser beam interaction takes place) has to be evaluated. In addition, if a hostile laser locks on a structure, it is necessary to estimate changes in the structural response during and after the interaction. The paper outlines the solution of the problem of local three-dimensional stresses as well as an approach to the global response analysis. Finally, a practical problem where local damage exists in the structure as a result of a limited exposure to a laser beam is discussed. Numerical examples illustrate that even a small indentation produced by a laser can noticeably affect the natural frequencies of a composite beam.
publisherAmerican Society of Civil Engineers
titleApproach to Analysis of Composite Structures Subjected to Action of High-Energy Laser Beam
typeJournal Paper
journal volume10
journal issue1
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)0893-1321(1997)10:1(38)
treeJournal of Aerospace Engineering:;1997:;Volume ( 010 ):;issue: 001
contenttypeFulltext


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