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contributor authorJi Yao Shen
contributor authorElias G. Abu‐Saba
contributor authorWilliam M. McGinley
contributor authorLonnie Sharpe, Jr.
contributor authorLawrence W. Taylor, Jr.
date accessioned2017-05-08T22:13:27Z
date available2017-05-08T22:13:27Z
date copyrightOctober 1994
date issued1994
identifier other39898345.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/74167
description abstractDistributed parameter modeling may offer a viable alternative to the finite‐element approach for modeling large flexible space structures. In addition, the introduction of the transfer matrix method to the continuum modeling process provides a very useful tool to facilitate the distributed parameter model applied to more complex configurations. This paper proposes a piecewise continuous Timoshenko beam model, which was used for the dynamic analysis of a tapered beam‐like structure. Instead of the arbitrarily assumed shape functions used in a finite‐element analysis, the closed‐form solution of the Timoshenko beam equation was used. Application of the transfer matrix method was used to relate all elements as a whole. Using the corresponding boundary conditions and compatibility equations, a characteristic equation for the global tapered beam was produced and natural frequencies derived. The results from this analysis were compared to those obtained from a conventional finite‐element analysis. While comparable results are obtained, the piecewise continuous Timoshenko beam model significantly decreased the number of modal elements required.
publisherAmerican Society of Civil Engineers
titleContinuous Dynamic Model for Tapered Beam‐Like Structures
typeJournal Paper
journal volume7
journal issue4
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)0893-1321(1994)7:4(435)
treeJournal of Aerospace Engineering:;1994:;Volume ( 007 ):;issue: 004
contenttypeFulltext


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